JPH116441A - Torizuka mechanism - Google Patents

Abstract

PROBLEM TO BE SOLVED: To layout a clearance between a housing and the vicinity of a control vane tip end in a small size in a high rotating range to an extremely high rotating range by arranging guide parts which consist of a needle bearing and the like, on a housing concentric circle part for controlling the control vane, and the tip end part of the control vane. SOLUTION: An concentric circle control vane mechanism is constituted serving a control vane 2, a spindle rolling bearing, and a tip end vane 3 as a main body. A tip end vane spring which is formed in a compact size and having a high spring constant is used in the vane tip end part. A tip end vane weight in the tip end vane spring constant is lightened. A positive displacement engine is constituted so as to seal the engine and prevent leakage of combustion gas under the rotating speed of natural frequency. On the other hand, the positive displacement type and the speed type mixed engine is constituted so as to minutely form a clearance between the control vane tip end and the housing, and prevent leakage of combustion gas, beyon the rotating speed of natural frequency. Namely, a high rotation and high torque type engine is constituted so as to carry out Torizuka cycle.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a torizuka mechanism in which a control vane of a concentric housing control vane mechanism is controlled by a concentric housing. The present invention is an expander, a compressor, which can use a multi-fuel or multi-heat source including a fission or fusion heat engine that can be used on land, at sea, or by air.
The present invention relates to a positive displacement mechanism such as a pump including a fuel injection pump or the like, a very high fuel multi-fuel internal combustion engine, and a power transmission device.

[0002]

2. Description of the Related Art As conventional internal combustion engines, a reciprocating piston type internal combustion engine, a Wankel type rotary engine and a gas turbine engine are widely known. The maximum number of revolutions that greatly affects the output due to insufficient low-speed torque or the like is about 9,000 revolutions per minute in a gasoline engine of a reciprocating piston engine. It is about 4,000 revolutions per minute for a diesel engine.
The output of a gasoline engine is about 65 to 100 horsepower per liter, and the output of a diesel engine is about 35 to 60 horsepower per liter.
For heat engines, there were small-sized, super-high-power, and speed-type gas turbines, but for automobiles and the like, low-medium-speed torque was small and fuel consumption was poor, so reciprocating piston engines of volume-type engines with good responsiveness were the mainstream. Although the response is somewhat poor in large aircraft etc., small and super-high power turbojet engines were mainstream,
I needed a long runway. The heat loss of exhaust gas in a conventional internal combustion engine was very large. The internal combustion Stirling engine could not be put to practical use because a regenerator with good thermal efficiency could not be found and a large compression ratio could not be obtained.

[0003] Even a diesel engine which is a multi-fuel engine is limited to fuels that require instantaneous completion of combustion, so that the compression ratio must be extremely high to induce self-ignition of fuel in each combustion cycle. Was. For this reason, the exhaust gas contains a very large amount of harmful exhaust gas, and for example, the exhaust gas regulation in internal combustion engines has been a very favorable nitrogen oxide concentration. The conventional vane technology does not have high rotation characteristics and is widely applied to oil pumps and the like.

The conventional gas turbine technology has almost disappeared recently except for a turbocharger in an automobile engine because of a problem in torque characteristics in a low speed range and difficulty in downsizing. Responsiveness of a conventional speed-type engine, such as a turbine, is low in the middle to low speed range, and the practical use of a positive-displacement engine is wide.
Also, the one with the car turbocharger was dangerous because afterburning, that is, afterfire was occurring during deceleration.

[0005]

SUMMARY OF THE INVENTION The thermal efficiency of a positive displacement internal combustion engine has been improved to a higher speed, a higher rotation speed and a higher torque and a higher performance.
The transmission is continuously variable, the compressor is made more sophisticated, the expander is made more sophisticated, the pump including the fuel injection pump is made more high-speed and high-performance, and the exhaust gas is harmful in the internal combustion engine. Although it was desired to reduce the composition and reduce the heat loss of the exhaust gas to a very small extent, conventional internal combustion engines and others have historically continued.

[0006]

In order to solve the above-mentioned problems, the present invention employs a positive displacement mechanism in a low and middle rotation range because of its excellent response and high middle and low speed torque. Compressor,
A vane of a positive displacement mechanism is used to constitute an expander including a heat engine that utilizes nuclear fission or fusion energy, a pump including a fuel injection pump, a multi-fuel internal combustion engine, a power transmission device, and the like. The load on the spring was reduced to have a natural frequency in the middle rotation range. In order to achieve a very high rotation type rotating at a speed of 35,000 to 45,000 per minute like a gas turbine of a speed type mechanism, a housing concentric circle control vane mechanism or a housing concentric hollow ring control vane mechanism or As the torizuka mechanism of the housing concentric hollow ring control vane mechanism, when configuring the internal combustion engine, the pressure scavenging cycle which is the torizuka cycle with the mechanical scavenging pump of the torizuka mechanism, the compression combustion expansion vane of the torizuka mechanism and the fuel injection device of the torizuka mechanism We requested a representative derivative technology capable of realizing the Torizuka cycle. In particular, in this patent, Japanese Patent Application No. 7-072
239 and Japanese Patent Application Nos. 8-179940 and 9-96
By providing a concentric portion of the housing for controlling the control vane and a guide portion made of a highly durable needle roller bearing or the like at the tip end of the control vane, the housing and the control vane are controlled from a high rotation range to an extremely high rotation range. It is possible to design a small gap with the vicinity of the tip, and it is possible to operate with extremely high thermal efficiency from a low speed range to an extremely high speed range by exhibiting an ultra-high output like a gas turbine.

[0007] The Torizuka Torizuka engine equipped with the Torizuka mechanism expander is a typical one of the representative configurations, and it has a very high thermal efficiency and an extremely high output of an extremely high rotation and maximum torque in an extremely multi-fuel engine and exhaust gas. It is a clean exhaust gas component with low heat loss.

[0008] As the working fluid, gas, vapor, liquid or the like can be used.

For example, in a heat engine such as a nuclear power plant utilizing nuclear fission or fusion, the present invention has an effect on day and night power demand fluctuations in which power demand fluctuates greatly because the torque in the low to middle speed range is higher than that of a gas turbine. Demonstrate.

When the working fluid is gas or steam, there are a compression process, a constant heat receiving process, an expansion process, and a suction / exhaust process depending on the rotation angle, and there are a torizuka mechanism torizuka engine, a torizuka mechanism torizuka type expander, a torizuka mechanism torizuka type compressor, Torizuka Torizuka pump is available.

For this reason, if a heat receiving portion such as a constant combustion chamber is formed in the housing, an adiabatic compression process, a constantly heat receiving process, and an adiabatic expansion process are performed, so that a constantly expanded work can be obtained. For this reason, the Torizuka mechanism expander can be a nuclear heat engine using an extremely large number of heat sources, a heat engine of an external combustion engine, or the Torizuka mechanism Torizuka engine can be an internal combustion engine using a very large number of fuels.

For example, if the internal combustion engine is configured as a torizuka mechanism, the torizuka engine performs combustion at every rotation in the inter-vane combustion chamber, so that the combustion gas pressure peculiar to the control vane mechanism is converted into torque with a small, extremely high thermal efficiency. Is high in conversion efficiency. This is due to the reason that the control vane mechanism performs a torizuka cycle, that is, a positive displacement regenerative constant-diffusion combustion cycle, that is, an injection period pressure increasing combustion cycle in torizuka combustion.

If the internal combustion engine is configured as a Torizuka mechanism Torizuka engine, it always passes through the diffusion combustion chamber where regeneration occurs every rotation, so unlike a diesel engine or a gasoline engine with an ignition delay, the ignition delay or explosive Torizuka combustion in which the pressure is constantly increased during the normal injection period corresponding to the extremely high rotation speed because there is no continuous combustion process and stable constant diffusion combustion.

Torizuka combustion of the volume-type regenerative continuous diffusion combustion is as follows:
A heat receiving part is formed in the Torizuka cycle, which is an approximate Carnot cycle constituted by the concentric control vane mechanism of the Torizuka mechanism.

The constant-diffusion combustion chamber provided in parallel with the sliding surface of the tip vane with the housing simply plays the role of the regenerator in the virtual internal combustion Stirling engine with a super-high thermal efficiency regenerator. Just because there is a depression in the chamber.

[0016] The combustion gas between the preceding vanes always passes through the combustion chamber due to the pressure rise and enters between the next vanes, and the diffusion combustion is always continued. A virtual ultra-high thermal efficiency regenerator that enters into the regenerator of an internal combustion Stirling engine to store heat and then immediately regenerates at 100% thermal efficiency with the same amount of combustion gas when exiting between vanes Equivalent to the existence of a mechanism.

That is, even if the experiment has not been completed yet, the space of the continuous diffusion combustion chamber is the same as that of a regenerator of an internal combustion Stirling engine with an ultrahigh thermal efficiency regenerator having a thermal efficiency of 100%. It can be seen that ultra-high output with high rotation maximum torque is possible.

Further, as shown in FIGS. 10 and 11, the combustion housing of this mechanism has a pressure-torque conversion effect peculiar to the vane mechanism having a larger torque than the reciprocating piston mechanism, and the concentric control vane mechanism of the Torizuka mechanism. By equipping the Torizuka type inflator with the Torizuka mechanism Torizuka engine, it is possible to carry out the bottoming torizuka cycle, effectively convert the combustion heat to the main shaft rotation force, and greatly reduce the heat loss due to exhaust gas. You can do it.

Therefore, as shown in FIG. 10, the change in the volume of the combustion chamber is the change of the conventional reciprocating piston mechanism as shown in FIG.
As the efficiency of converting combustion gas to torque is superior to that of, the maximum torque is obtained, so the spring constant per vane weight, which is the reciprocating weight of the spring load, is high, so that it has a natural frequency in the middle rotation range. According to the present invention, it is possible to design the gas turbine in a high speed range from a high speed range to an extremely high speed range.
High conversion efficiency with extremely high rotation of 0-45,000 rpm,
In addition, the output obtained by multiplying the rotational speed by the torque for the maximum torque having the expansion ratio ε = 15 to 25 is an extremely large output, and is a high-performance engine using a multi-fuel.

In the combustion in the space between two adjacent vanes, the regenerative constant diffusion combustion is a leading vane sliding surface having an injection nozzle tip when the combustion process ends in the preceding inter-vane combustion chamber near the end of the compression process. The fuel injected from the normal diffusion combustion chamber, which is provided in parallel with the combustion chamber, intrudes from the normal diffusion combustion chamber to the next combustion chamber together with the flame due to the increase in the pressure of the combustion gas in the preceding combustion chamber, and the flame spreads constantly through the normal diffusion combustion chamber. This is because the mechanism of the constant diffusion combustion is continued, and the constant diffusion combustion is established only by the diffusion combustion.

According to this mechanism, the positive displacement regeneration-type continuous diffusion combustion, that is, the torizuka combustion is a combustion system which has no ignition delay and can cope with extremely high rotation.

The positive-discharge type regenerative constant-diffusion combustion scavenging supercharged dual-, triple-, and quadruple-control vane internal combustion engine of the multi-fuel engine of the present invention and a derivative technology thereof use a mechanical scavenging pump as a control vane mechanism and concentrically control the combustion chamber. The triple and quadruple torizuka mechanism of the multi-fuel engine as the vane mechanism The effective expansion angle of the torizuka engine is larger than that of the conventional two-cycle and four-cycle internal combustion engines by configuring the expander and the fuel injection pump as concentric control vane mechanisms. Can be greatly increased, and a large air supply port and a large exhaust port can be provided as compared with the prior art, so that a mechanical scavenging pump engine having a large effective expansion angle, a very small thermal efficiency and an ultra-high output can be obtained.

Further, by using a strong tip vane spring using a leaf spring which is small and can obtain a high spring constant, the tip vane weight is reduced with respect to the tip vane spring spring constant, and the rotation speed at which the tip vane jump occurs completely seals the seal. Governs the number of revolutions that can be maintained by the displacement type in the middle rotation range.However, at the revolutions lower than the natural frequency, the combustion engine does not leak and the combustion gas does not leak. If the rotation is higher than the rotation that occurs, there will be almost no leakage due to the minute gap, so a mixture of a positive displacement engine and a speed type engine will be formed, and it will be a super high output type with a maximum torque and a maximum torque type that performs the Torizuka cycle which is the maximum torque .

The displacement of the tip vane is very small and is about 1% or less with respect to the inner diameter of the housing as shown in FIG. 12 of the numerical calculation result, which is an important aid for the extremely high rotation type. That is,
The use of the tip vane spring and the tip vane mass in the rotation above the middle rotation range where the natural frequency of the spring-mass system exists requires a technique of high-precision finishing equivalent to a gas turbine.

Torizuka Mechanism The Torizuka-type inflator equipped with a torizuka-type inflator is a genius Sadie Carnot as a torizuka cycle realization organization.
In a paper written in 824, it was later called the Carnot cycle, but it was desperate to realize an engine that approached the Carnot cycle historically around the world. It is an engine that performs approximate topping and bottoming as an engine that performs the Torizuka cycle of the per-approximate Carnot cycle realizing engine.

In the Torizuka cycle in which a regenerative displacement type constant diffusion combustion cycle is performed, the vane angle is reduced and T-Δd in FIG.
Considering the s diagram, if there is an injection, the sum of the regenerative pressure-increase combustion and the entropy change per main spindle rotation arranged in parallel per injection nozzle performs a volume-type regenerative pressure-increase combustion cycle, which is a torizuka combustion cycle. This allows the engine to be of an extremely high rotation speed, a maximum torque, a very high output, and an extremely high thermal efficiency type.

[0027] Since the genius Sadie Carnot in 1824 wrote a dissertation, the world's internal combustion engine and external combustion engine researchers have reached the goal of realizing the engine and the engine that approaches the Carnot cycle that cannot be exceeded is theoretically here. Approximately, a torizuka cycle is realized as an internal combustion engine that performs approximate topping and bottoming per injection nozzle per main spindle rotation.

Further, in this configuration, the main shaft rotation angle can be increased at a location where the gas pressure near the top dead center is large, so that the output can be increased. Also, the point that the exhaust heat becomes larger due to the positive displacement regenerative constant combustion engine when a dual exhaust, triple and quadruple control vane internal combustion engine with a mechanical exhaust turbine combined supercharged positive displacement regenerative constant combustion scavenging supercharger is used. Volumetric efficiency and thermal efficiency can be improved as a heat source for supercharging work.

Further, since the effect of improving heat efficiency and the effect of improving volumetric efficiency due to the utilization of exhaust heat are large, and operation is possible without increasing the compression ratio as much as that of a diesel engine, low pollutant emissions can be reduced because harmful components of exhaust gas can be reduced. It can also be configured as a torizuka engine, a torizuka engine of a multi-fuel engine with regenerative, positive displacement, constant diffusion combustion that uses gasoline, alcohol, light oil, heavy oil, LPG, hydrogen, etc.

In addition, because of the excellent torque-pressure conversion efficiency described above, when a Torizuka mechanism Torizuka type expander is constructed, the low-to-medium-speed torque characteristic of a positive displacement engine can be remarkably higher than that of a gas turbine. Can be obtained.

Further, the danger of afterburning, that is, afterfire, is considerably reduced because the expansion ratio is increased and the gas temperature is reduced when a Torizuka mechanism torizuka type expander is installed.

Although the thermal efficiency of the engine operation in the regenerative heat exchanger in the one-color engine that I conceived failed due to the intermediate thermal efficiency of the thermal efficiency due to the heat transfer of the regenerative regenerator, it failed. 100%
There is no need to experiment in the space that is always a depression of the combustion chamber provided parallel to the sliding surface of the tip vane, which is equivalent to the existence of an ultra-high thermal efficiency regenerator with thermal efficiency. It is a vessel.

[0033]

The dual, triple and quadruple vane internal combustion engine of the present invention and its derivative technology have been pioneered as a large effective expansion angle extremely low fuel consumption small super high power internal combustion engine, and have a rotation angle of about thirty degrees more than the conventional two-cycle engine. The effective expansion is possible from 75 to 75 degrees or more, and a mechanical scavenging pump that is also a scavenging pump and a combustion chamber is formed by a tip vane with a leaf spring having a plurality of vane side seals advantageous for high rotation and low rotation Large effective expansion angle Extremely low fuel consumption The rigidity is increased by using sleeves for the combustion chamber housing and mechanical scavenging pump housing to withstand the centrifugal force of the vane in miniaturization and ultra-high output. By configuring the drive mechanism in the rotary concentric ring to achieve extremely high rotation, it is possible to achieve high durability. As a result, even a combustible fuel that does not have instantaneous completion of combustion can be configured as a positive displacement regenerative continuous diffusion combustion engine. It is possible to achieve extremely high rotation.

Since the tip vane stroke peculiar to the concentric control vane mechanism of the present housing of the Torizuka mechanism is small and the leaf spring acting on the tip vane can be designed strongly, the spring constant of the leaf spring acting on the tip vane by the weight of the tip vane is obtained. The value obtained by multiplying the square root of the value divided by the above by a constant, that is, the number of revolutions that is the natural frequency of resonance can be made extremely high, so that the limit number of revolutions is extremely high.

The extremely high rotation is a value obtained by multiplying the square root of the value of [weight of tip vane / spring constant of tip vane spring] by a constant, that is, the natural frequency of resonance (the number of revolutions at which a valve jump occurs in a poppet valve or the like). Is in the middle rotation range, and from the high rotation range to the extremely high rotation range, it can be operated like a gas turbine which is a speed type heat engine. The reason why the tip vane weight can be reduced because the tip vane stroke is small,
The reason why the leaf spring acting on the tip vane can be designed to have an extremely strong spring constant and the following reasons, it has a natural frequency in the middle rotation range, and furthermore, from the high rotation range to the extremely high rotation range, a speed type heat engine Due to the gap between the housing and the tip of the control vane, as in some gas turbines, it is possible to achieve extremely high rotational speeds of approximately 35,000 to 45,000 per minute at the same maximum rotational speed as the gas turbine.

Since the displacement of the tip vane is extremely small as shown in FIG. 12, the present engine can be established as a speed type engine.
Since the value of [tip vane weight / tip vane spring spring constant], which governs the maximum rotation speed as a positive displacement engine, can be made extremely small, the natural frequency of the spring-mass system can be taken in the middle rotation range. .

Further, since the extremely high rotational speed is the torizuka combustion of the volume-type regenerative constant-diffusion combustion, the diffusion combustion is always performed. Therefore, when the rotation speed is higher than the rotation speed having the natural frequency, the volume-type engine and the speed-type engine are used. This is a combustion method that can cope with extremely high rotations of 15,000 to 45,000 rpm or more up to the maximum rotation speed such as a turbine.

The technique related to the rotary side housing-side components shown in FIG. 8 is intended to ensure extremely high rotation.

The rotary concentric ring or the rotary concentric groove ring enhances the durability of the single-roller partial bearing, and exhibits durability sufficiently effective for use at extremely high rotation.

The maximum torque property is a characteristic of the vane mechanism. The volume of this mechanism is smaller than that of the conventional reciprocating piston mechanism as shown in FIG. Since the conversion efficiency from pressure to torque by combustion and expansion is high, and the rotation angle at the main shaft angle where the pressure is high is extremely large, torque can be obtained much more significantly than in FIG. 11 showing a conventional reciprocating piston mechanism. The reason is that the expansion ratio described below is large.

Furthermore, having an expander greatly increases the expansion ratio, which is about 15 to 25.

Since the pressure-torque conversion efficiency peculiar to the vane mechanism is high, the maximum torque is supplied, and the output obtained by multiplying the torque by the rotation speed and the constant exerts an extremely large output by the extremely high rotation speed of this configuration.

The extremely high thermal efficiency is due to the reason that the conversion efficiency is high near the near dead center where the maximum torque property is above and the expansion ratio can be extremely large.

When a speed type turbine is used and it is desired to use the rotation in the middle to low speed range more widely, it is highly effective to use a positive displacement type torizuka mechanism expander to achieve extremely high thermal efficiency.

In the case of the Torizuka engine, the variable eccentric type control vane always constitutes a fuel injection device, and thereby the inertia of the parts constituting the main moving part which prevents the extremely high rotation in the conventional internal combustion engine. Paying attention to the fact that the mass problem suppressed the upper limit of the number of revolutions, this mechanism not only made it possible to reduce the weight of the tip vane, but also made it possible to provide a strong tip vane leaf spring.

As a result, not only the control vane mechanism that does not cause the vane jump of the tip vane to extremely high rotation but also the transition to extremely high rotation is realized, but also extremely large torque, small engine size, light weight per horsepower and low fuel consumption. It is a multi-fuel engine that can use alcohol, gasoline, light oil, heavy oil, LPG, hydrogen, etc., and has a large effective expansion angle of regenerative constant diffusion combustion. Pioneered new technology. Since the output is obtained by multiplying the torque by the number of rotations, the maximum torque is multiplied by the extremely high rotation to exhibit an extremely large output.

When the mechanical scavenging pump supplies fresh air charged during the suction period of about 160 to 170 ° to the vane compression combustion expansion chamber, it is a very large air supply passage which is extremely advantageous at extremely high revolutions, and the charging efficiency is sufficient. High.

The total expansion angle of the Torizuka mechanism equipped with the concentric circular control vane expander is about 1 times that of the vane expander.
The 60-170 ° expansion period adds to the approximately 145-165 ° expansion period of the vane compression combustion expansion chamber, for a total expansion period of approximately 305-335 °. That is, since the reciprocating piston mechanism has an effective expansion angle of about 155 to 170 [deg.] Excluding the overlap of the intake and exhaust valves, which is much larger than that of the air, the number of molecules of the combustion gas is larger than that of air. When applied to an internal combustion engine or the like that can obtain expansion work, it is possible to significantly reduce the calorific value of exhaust gas loss.

The torizuka mechanism torizuka engine equipped with the torizuka mechanism expander has an expansion ratio of about 15 to 25, and is configured to take advantage of supercharging. It is an effective cost performance improvement measure to improve the torque per unit weight and the output by utilizing the supercharging of the mechanism Torizuka engine, etc., and to reduce the size and weight.

Conventionally, automobiles and the like equipped with an exhaust turbine supercharger have been subjected to afterfire during deceleration or the like. However, a Torizuka Torizuka engine equipped with a Torizuka Torizuka type expander uses an expander. The risk of afterfire occurring due to the exhaust gas being exhausted through is small.

Claims 2 and 6 can be applied not only to land use but also to power transmission devices for aircraft, ships, etc., and therefore have a very wide application range.

The present invention relates to a positive-displacement regenerative constant-diffusion combustion supercharged vane internal combustion engine with a mechanical supercharger or a composite turbocharger, and as a derivative technology, a large effective expansion angle, extremely low fuel consumption, a small super-high-power prime mover, and a derivative aerial. And a land-based jet propulsion engine, which constitutes a prime mover and a propulsion method that achieve a very high rotation type, increase output, improve volumetric efficiency, improve thermal efficiency, and improve propulsion efficiency.

In particular, when a triple or quadruple control vane internal combustion engine or a mechanical exhaust turbine combined supercharging is used, the heat loss of the internal combustion engine is determined by the volume regeneration type constant diffusion combustion supercharging in the space between the vanes, thereby utilizing the exhaust heat loss. Therefore, the achievement of the extremely high rotation type, the increase of the output, the improvement of the volumetric efficiency, the improvement of the thermal efficiency and the improvement of the propulsion efficiency are remarkably large.

According to a ninth aspect of the present invention, there is provided a turbine utilizing a momentum in a mass flow rate of air without discharging high-pressure air as it is by a combined compressor of a torizuka mechanism compressor of an axial flow compressor and a concentric groove control vane compressor. By compensating the horsepower loss by turning the air compressor, an extremely large capacity air compressor is constituted, so that even a large aircraft can perform vertical takeoff and landing.

Even if a Torizuka mechanism compressor or a Torizuka mechanism oil feed pump is used coaxially with the turbine, there is no problem in high rotation characteristics.

According to the thirteenth aspect of the present invention, since the single roller partial bearing is used, the single roller per one side groove for vane control is supported by the roller support having a high strength, and withstands the centrifugal force at the time of high rotation. It is characterized by the following. An extremely small bearing that can withstand extremely high rotation can be configured as compared with the case where a needle roller bearing is used.

According to a thirteenth aspect of the present invention, the portion supported by the single roller supporting portion has the same lubrication as the slide bearing, and the portion whose position is controlled by the concentric circle of the housing is the rolling bearing. Is the same as

By forming a single roller partial bearing at the end of the vane on the center side of the rotor as shown in FIG. 7, it is small and durable. When the internal combustion engine is configured, the characteristic of the maximum torque that rotates to the extremely high rotation causes the pressure of the vane mechanism to decrease.
Since the torque conversion efficiency is extremely high, an output obtained by multiplying the two and multiplying by a constant can obtain an extremely large output.

[0059]

[Brief description of the drawings]

FIG. 1 is an external view of a control vane and a tip vane in a torizuka mechanism of the present invention, that is, a concentric control vane mechanism.

FIG. 2 is a front view of an assembly drawing of a torizuka mechanism of the present invention, that is, a concentric control vane mechanism. 1 and 2 show a torizuka mechanism of the present invention using a needle roller bearing. Rotary side housing-related component technology improves lubrication and durability at extremely high speeds even with single roller partial bearings.

FIG. 3 is a side view in a conceptual view of a four-vane internal combustion engine using a torizuka mechanism of the present invention, that is, a concentric control vane mechanism.

FIG. 4 is a side view of a turbojet engine with a multi-stage compression injector according to the present invention.

FIG. 5 is a front view of the downward injection type jet propulsion aircraft for vertical takeoff and landing of a torizuka mechanism driven multi-stage compressor supercharged quadruple control vane internal combustion turbojet composite injection rotational force composite propulsion of the present invention. It has a concentric control vane mechanism Torizuka engine inside the fuselage of the fuselage. A multi-stage compression injector is driven by a concentric control vane mechanism Torizuka engine to operate a turbojet engine.

FIG. 6 is a sectional view of a single-roller partial bearing of a rotor center side bearing type in a control vane. A single roller partial bearing is provided at the vane base.

FIG. 7 is an assembly drawing of a torizuka mechanism of a housing concentric control vane mechanism equipped with a single roller partial bearing. Reference numeral 18 denotes a rolling surface of a bearing such as a single roller partial bearing in a concentric groove of the housing. The emphasis was placed on the durability of the Torizuka engine at extremely high speeds. Further, reference numeral 8 denotes an air supply passage, which is an extremely high-rotation type and has a significantly large passage cross-sectional area. FIG. 18 is an assembly drawing of a torizuka mechanism of a housing concentric control vane mechanism equipped with a single roller partial bearing, in which a rolling surface of a rotary housing concentric ring indicated by a dotted line 18 is rotated at a rotation speed close to the rotation speed of the rotor. With sufficient lubrication and durability.

FIG. 8 shows a drive mechanism for a concentric rotating wheel of a rotary housing. It is a block diagram of the drive mechanism in a rotary housing concentric ring. The durability at extremely high rotations has been secured.

FIG. 9 is a T-∫ds diagram of a torizuka mechanism of the present invention, that is, a torizuka engine using a concentric control vane mechanism. FIG. 4 is a TS diagram of the Torizuka engine and shows an approximate Carnot cycle, and performs a torizuka cycle, which is an approximate Carnot cycle, per rotation of the spindle per injection nozzle.

FIG. 10 shows the volume change with respect to the main shaft rotation angle in the combustion chamber for the torizuka mechanism of the present invention, that is, the concentric control vane mechanism. An extremely large torque can be obtained as compared with the conventional volume change. It is a figure of a numerical calculation result. The concentric control vane mechanism has a larger main shaft rotation angle than the reciprocating piston mechanism in a place where the gas pressure near the near dead center has a large ability to convert the torque while the gas pressure is high, which means that an extremely large torque can be obtained.

FIG. 11 shows a volume change with respect to a main shaft rotation angle in a combustion chamber for a conventional reciprocating piston mechanism. Compared to FIG. 10 for the concentric control vane mechanism of the present invention, it can be seen that the conventional reciprocating piston mechanism has a low ability to convert the expansion force of the combustion gas into torque and is extremely disadvantageous in obtaining a large torque. . It is a figure of a numerical calculation result. The gas pressure drop near the top dead center is more rapid than at the Torizuka engine.

FIG. 12 is a view showing displacement of a tip vane in a torizuka mechanism of the present invention, that is, a concentric control vane mechanism, with respect to a main shaft rotation angle. In order to obtain extremely high rotational speed, the displacement is small enough, and the tip vane spring weight can be made very light with respect to the spring constant of the tip vane. it can. FIG. 4 shows displacement of a tip vane in a torizuka mechanism of the present invention, that is, a concentric control vane mechanism, with respect to a main shaft rotation angle. In order to obtain extremely high rotation, the amount of displacement is sufficiently small, and the weight of the tip vane with respect to the spring constant of the tip vane spring can be extremely reduced. Therefore, the rotation speed at which the tip vane continues to sink can be designed in the middle rotation range. It is a figure of a numerical calculation result. This is a calculation result in the case where a guide portion such as a needle roller bearing is provided at the base of the concentric control vane of the housing. In the first aspect, when the control vane has a guide portion at the tip end portion, it is qualitatively the same, but the displacement amount is sufficiently small.

[Explanation of symbols]

REFERENCE SIGNS LIST 1 needle roller bearing 2 control vane 3 tip vane 4 rotor 5 vane compression combustion expansion chamber housing 6 compression combustion expansion chamber control vane with leaf spring with side seal 8 air supply passage 9 passage to expander 10 injection nozzle or ignition Plug 11 Housing concentric ring 12 Expander 13 Exhaust passage 14 Multistage compressor 15 Hydraulic driven turbojet engine 16 Roller 17 Roller support 18 Rolling surface of bearing in control vane 20 Driven concentric control vane mechanism Oil pump 21 Variable eccentric concentric control vane mechanism Torizuka type constant fuel injection device 22 Main shaft of Torizuka mechanism 25 Rotary housing concentric ring constant speed increasing gear 26 Rotary housing concentric ring

Claims (14)

[Claims] In a rotary volume change mechanism, a side housing having a concentric cylindrical portion of a housing, or a rotary side housing side hollow ring having a rotary housing concentric hollow groove ring or a rotary housing concentric hollow ring is provided. Controlled vane and side housing with concentric hollow groove ring to control control vane, or rotary housing to control control vane concentric hollow ring or rotary housing concentric hollow groove ring and cylindrical housing Needle roller bearings and needle roller bearing support parts eccentric from the center of the roller, or single roller and single roller partial bearing support parts, or bearings for controlling the position of control vanes having curved surface bearings and their rings The guide part is a concentric hollow circle of the housing and the concentric hollow circle inside the housing or the rotary side housing. The control vane automatically moves from the center of the rotor with the rotation of the rotor by entering the groove portion of the wheel and the inside thereof or the concentric ring of the housing on the rotary side housing side and the inside thereof. The rotational speed of the concentric hollow groove ring of the type housing is a torizuka mechanism in which the control vane is automatically position-controlled and moved with the rotation of the rotor in the vicinity of the rotational speed of the rotor, that is, the housing concentric control vane mechanism, At the tip of the control vane, which is close to the concentric control vane housing, has a guide part with a concentric part of the housing and a needle roller bearing for position control of the control vane. The number is about 35,000-45,000
The torizuka mechanism is characterized by the fact that it is a mixed type of volume type and speed type, achieves miniaturization, and exhibits ultra-high output with extremely high rotation and maximum torque. 2. A torizuka mechanism, that is, a housing concentric control vane mechanism, a compressor, an expander including an expander such as a nuclear fission or fusion nuclear heat engine, a pump including a fuel injection pump, a multi-fuel internal combustion engine, A control vane and a leaf spring having a concentric circular side housing side guide portion with a side seal having a tip vane and a leaf spring acting on the tip vane, which are used in a volumetric mechanism requiring airtightness such as a transmission device and an angle adjusting mechanism. When mechanical scavenging including supercharging is performed using the shaft of a rotor having a side seal with a mechanism as the main shaft, the tip vane and the housing with a leaf spring acting on the tip vane are concentrically rotated by a mechanical scavenging pump having a side housing side guide control vane. To perform scavenging or scavenging by a mechanical scavenging pump configured to perform mechanical scavenging or scavenging supercharging. A concentric housing with a side seal having a leaf spring acting on the tip vane and the tip vane or a rotary housing with a side housing side guide control vane or a side seal having a leaf spring and a housing having a concentric ring and a rotor side seal. In a combustion chamber that performs continuous diffusion combustion separated by two vanes adjacent to the rotor that is eccentric to the rotor, a new gas is exchanged by a mechanical scavenging pump that has an air supply port and an exhaust port near the rotor dead center. If the air is compressed and the fresh air is air, the Torizuka mechanism always configures a fuel injection device, etc., so that the same inter-vane compression combustion expansion chamber performs combustion at every revolution and the compression combustion expansion housing has a positive displacement regenerative normal diffusion combustion. Combustion named Torizuka combustion due to its novelty, and from a constant diffusion combustion chamber installed parallel to the tip vane sliding surface Positive fuel can be used for the injected fuel.Positive displacement regenerative continuous diffusion combustion of internal combustion engine.Torizuka engine. Compression ignition Torizuka mechanism Torizuka engine, or multi-fuel engine positive displacement regenerative constant diffusion combustion spark ignition compression ignition hybrid Torizuka mechanism Torizuka engine, or when fresh air was premixed, it was vaporized by the ignition device. The fuel is ignited by spark ignition to burn near the rotor's near-dead center, and by using a positive displacement regenerative constant-diffusion combustion spark ignition Torizuka mechanism Torizuka engine, the expansion work performed by working gas by burning near the rotor's near-dead center is achieved. Specific to the vane mechanism, in which the rotation angle around the near dead center of the main shaft of the engine due to the rotation of the rotor is small and the rotation angle at the place where the pressure is high and the pressure is high is larger than that of the conventional internal combustion engine The leaf spring acts on the tip vane and the housing concentric side housing control vane and the reaction force causes the tip vane to act on the housing, and the compression combustion expansion chamber housing Using a ferrous metal sleeve as a light alloy, and using a metal sleeve or metal plating as a mechanical scavenging pump housing, and a variable air supply type variable scavenging pump with variable eccentricity A concentric control vane internal combustion engine, a side housing fluid mechanical scavenging pump and side housing fluid scavenging holes, and a central housing that rotates in synchronization with the engine speed by a timer. Perform the Torizuka cycle of the positive displacement regenerative continuous combustion cycle The Tokazuka Torizuka Engine is a multi-fuel engine that can use gasoline, light oil, heavy oil, LPG, hydrogen, etc. It is a high-response, medium-to-low-speed, high-volume, regenerative, constant-diffusion combustion engine. Torizuka mechanism of variable eccentricity control vane mechanism As a triple control vane system of the constant fuel injection device and the torizuka mechanism compression combustion expansion chamber control vane mechanism, the heat receiving process part of the pressure increase cycle during the injection period in positive displacement type regenerative constant diffusion combustion, that is, the injection nozzle An internal combustion engine that performs intake, compression, and heat receiving process portions and expansion in a Torizuka cycle of an approximate Carnot cycle per main spindle rotation, wherein the Torizuka mechanism according to claim 1, 3, and 4, and this claim. The torizuka mechanism according to claim 1, wherein a torizuka cycle utilizing exhaust gas loss is completely performed. 3. A torizuka mechanism, that is, a concentric control vane mechanism, a control vane mechanism of a compression combustion expansion chamber and a control vane mechanism of a mechanical scavenging pump, a positive-displacement regeneration type continuous diffusion combustion dual control vane mechanism or compression combustion expansion. The control vane mechanism of the chamber, the control vane mechanism of the mechanical scavenging pump, and the control vane mechanism of the fuel injection pump are of the positive displacement type. Torizuka mechanism housing concentric control vane mechanism characterized by having an expander, torizuka mechanism control vane mechanism Variable displacement eccentric control of a positive displacement, constant combustion triple control vane mechanism with a fuel injection device or a torizuka mechanism Vane mechanism A continuous regenerative, constant-diffusion combustion quadruple control vessel equipped with a concentric control vane mechanism expander for the housing of the Torizuka mechanism in the constant fuel injector. As a torizuka mechanism of the torizuka mechanism, a bottoming operation to perform the heat radiation process part of the torizuka cycle is performed, and the torizuka mechanism completes the torizuka cycle utilizing the exhaust loss according to the first, second, fourth, and fourth aspects. The torizuka mechanism according to claim 1, wherein the mechanism is configured. 4. A positive-displacement, constant-diffusion, dual-diffusion control vane engine with a torizuka mechanism, a concentric control vane mechanism, and a torizuka-mechanical scavenging pump equipped with a torizuka mechanism positive-displacement control vane constant-diffusion combustion chamber housing. Or a torizuka mechanism control vane mechanical scavenging pump equipped with a torizuka mechanism control vane combustion chamber and a torizuka mechanism expander A torizuka mechanism positive displacement regenerative triple control vane Torizuka engine with a variable eccentric injection amount adjustment housing concentric control vane mechanism A torizuka mechanism volume-type regenerative constant-diffusion combustion triple control vane with a torizuka mechanism always-fuel-injection device, which constitutes a torizuka-type fuel injection device of a fuel injection device and achieves positive-displacement-type constant-diffusion combustion. Bottoming as a torizuka engine or a torizuka mechanism with a torizuka mechanism expander, a positive displacement, regenerative, constant-diffusion combustion quadruple control vane mound engine. Claim 1 and claims 2 and 3
The torizuka mechanism according to claim 1, wherein the torizuka mechanism is configured to completely perform the torizuka cycle utilizing the exhaust loss by the torizuka mechanism. 5. A torizuka mechanism, that is, a concentric control vane mechanism, wherein a flow path is provided using a housing and a side housing near a near dead center, and a flow path is provided using a housing and a side housing near a far dead center. The variable eccentric torizuka mechanism according to claim 1, characterized in that the transmission ratio is steplessly changed by changing the amount of eccentricity using a fluid. 6. A toroidal mechanism, i.e., a concentric control vane mechanism, in which a fluid pressure sent from a torizuka mechanism continuously variable transmission is sent back to a driven vane pump of a driving section. The torizuka mechanism according to claim 1, further comprising: 7. The torizuka mechanism, that is, the concentric control vane mechanism itself has a high maximum rotation speed and a large amount of exhaust gas per volume. Extremely high thermal efficiency and extremely light weight achieved by equipping an exhaust turbine supercharger with a mechanical displacement type regenerative continuous diffusion combustion triple control vane tokazuka engine or a Torizuka mechanism volume regenerative constant diffusion combustion quadruple control vane torizuka engine. Positive displacement regenerative continuous diffusion combustion dual control vane mechanism type torizuka engine with exhaust turbine supercharger or positive displacement regenerative continuous diffusion combustion triple control vane mechanism torizuka engine with exhaust turbine supercharger to achieve engine weight or Extremely high combustion gas of internal combustion engine at extremely high speed as a positive displacement regenerative constant diffusion combustion quadruple control vane mechanism type torizuka engine with exhaust turbine supercharger Possessed mechanism according to claim 1, wherein the utilizing output from Rukoto other than shaft power. 8. An air compression injector or an air jet injector having a vertical wing and a horizontal wing at a fuselage head, a fuselage upper part, and a fuselage tail and having a head wing and a tail wing attached to a horizontal wing in an aircraft. The torizuka mechanism according to claim 1, wherein the overhead tail wing aircraft is characterized in that the aircraft angle can be changed and the jet propulsion flight can be performed in vertical takeoff and landing and aerial stationary by changing the injection angle of the turbojet engine with the air compression injector. 9. The torizuka mechanism according to claim 1, wherein said torizuka mechanism is a concentric control vane having a flat H-shaped cross section. 10. In the case of a four-wheeled vehicle, the hydraulic pressure sent from the continuously variable transmission of the torizuka mechanism, that is, the concentric control vane mechanism, is directly sent to the drive wheels so that four-wheel drive four-wheel steering can be selected. 2. The torizuka mechanism according to claim 1, wherein the drive direction changing method is characterized in that a small turn with a fast limit speed is effective. 11. A torizuka mechanism, that is, a concentric circle control vane mechanism, having a plurality of variable vertical injection ports for steering vertical takeoff and landing of downward injection and backward injection propulsion from the upper front to the rear upper of the fuselage. 2. The torizuka mechanism according to claim 1, wherein the jet propulsion aircraft is capable of performing a flight with a large lift. 12. A torizuka mechanism, that is, a concentric control vane mechanism, wherein a plurality of steering screws are provided from a lower front part to a lower rear part of a hull to achieve high speed navigation with a small turning radius. The torizuka mechanism according to claim 1, wherein the tail steering propulsion vessel is used. 13. A torizuka mechanism, that is, a concentric control vane mechanism for controlling a housing concentric control vane, wherein a single vane is supported by a roller supporting portion per one side groove for a single vane, The torizuka mechanism according to claim 1, wherein the control vane is controlled by a concentric circle of the housing of the side part of the side housing or the rotary side housing side part. 14. A torizuka mechanism, that is, a concentric control vane mechanism, wherein the vane has a tip vane at a vane tip portion near the inner wall of the housing of the housing concentric control vane, and a tip of a tip vane guide portion sliding with the tip vane is connected to the housing concentric control vane. The front end of the control vane is characterized by having an entrance and exit from the constant combustion chamber, which is the tip of the control vane, which is formed with a slope extending from the tip of the tip vane sliding portion to the width of the portion that houses the tip vane spring. The torizuka mechanism according to claim 1.