CN201354144Y

CN201354144Y - flying boat

Info

Publication number: CN201354144Y
Application number: CNU2008201789626U
Authority: CN
Inventors: 武满吉
Original assignee: Individual
Current assignee: Individual
Priority date: 2008-12-03
Filing date: 2008-12-03
Publication date: 2009-12-02
Anticipated expiration: 2018-12-03

Abstract

The utility model provides a component structure of flying boat establishes the control cabin in an gasbag below, and unit components such as propeller and power control system then are equipped with in this control cabin. The propeller is mainly composed of a power fan and a plurality of compressors arranged at the periphery of the power fan in an equiangular ring manner, the power fan can generate the power for the straight movement of the flying boat, the compressors are equally divided into a left-turning part and a right-turning part, and the left-turning direction and the right-turning direction of the flying boat can be controlled by airflow sprayed by the nozzles of the compressors at the left-turning part and the right-turning part. The power control system is composed of a plurality of solar panels, a direct current generator, a storage battery, an inverter and other components, and the solar panels are utilized to convert solar energy into direct current electric energy for supplying electric energy required by various instruments and propellers in the control room. The flying boat can utilize the characteristics of solar power generation, compressed airflow control of the flying direction and the like, so that the flying boat can fly and control conveniently and stably.

Description

HIKOUSEN

Technical field

The utility model relates to a kind of HIKOUSEN, is meant a kind of neat Berlin formula HIKOUSEN that utilizes helium or nitrogen as lifting power especially, with and the structural improvement of flying power and steering manipulation system.

Background technology

Neat Berlin formula HIKOUSEN is a kind of early stage aerocraft, and its flight lift comes from the air lift force that acts on the fuselage, has and handles and propulsion system.Derive so far, its propulsion system is to be made of the power fan system that aero-engine drives usually at present.General HIKOUSEN has a huge main gasbag, and the inside has been full of the gas that is lighter than air, as hydrogen, helium.Because very unstable burning easily of hydrogen and blast are so modern dirigible uses helium more.Two sides are provided with a balloonet in addition in the main gasbag, and air can be injected in the inside.When HIKOUSEN rises, single-piece than important lighter than air, so in passenger cabin, the air valve of balloonet is opened, helium pressure in the main gasbag can just allow the air exhaustion in the balloonet (reduction of helium density on expansion) airship float naturally gradually.Opposite, when airship descends, single-piece proportion must be heavier than air, so in passenger cabin, the air valve of balloonet is closed, and air pumping is opened, air is poured in the balloonet, also just compressed simultaneously the helium volume in the main gasbag (increase of helium pressed density), so just landing downwards gradually of HIKOUSEN.

And in the TaiWan, China patent database, another kind of HIKOUSEN is also disclosed, it is No. 115553 " a kind of hot HIKOUSEN " patent case of bulletin (hereinafter to be referred as application case formerly), as Fig. 1, shown in 2, this formerly the main formation of application case comprise: a hull is for making inflatable spindle to strengthen nylon cloth, be provided with the hat top blow off valve of a keying that stay cord is controlled at the back, afterbody then is provided with a pair of horizontal tail and a pair of normal limb, wherein the movable wing both sides of below normal limb are respectively equipped with stay cord and control and turn to, then open a hole to belly, and at the solid built-in cover body that links skeleton in length and breadth of peritreme seam.One Suspension System comprises two tension pieces, some steel wires, reaches a framework.One combustion systems comprises a flamethrower, a supply ventilating fan and a sleeve.One propulsion system comprises the passenger cabin of loading, and the stay cord of seat, engine, gas cylinder, may command movable wing and hat top blow off valve etc. is being set in the passenger cabin, and a pair of screw propeller is then established in the outer both sides of passenger cabin.Mainly utilize Suspension System to be fixed in the hull back through tension piece, and with steel wire suspention combustion systems and propulsion system, make the hull moulding by the supply ventilating fan air-supply, and the hot air that produces by flamethrower flame, make the hull buoyance lift, by controlling that the propelling of propulsion system screw propeller and movable wing turn to, hull is reached to control air objective again.

The utility model that above-mentioned application case formerly can be said so neat Berlin formula HIKOUSEN and fire balloon are combined as a whole.No matter but be the neat Berlin formula HIKOUSEN of tradition or the utility model of application case formerly, power resources when flying when it rises, steering manipulation system etc. are all followed from early stage traditional technology, and not only speed is slow, unstable, and power source is not had a feature of environmental protection yet, and the necessity that is improved is arranged.

The utility model content

The technical problems to be solved in the utility model provides a kind of composition structure of HIKOUSEN, and it makes HIKOUSEN when flight lift-off, and the kinetic force of its flight has the feature of environmental protection and has more benefit, and controlling of turning to is also more exquisite, stablize.

For solving the problems of the technologies described above, embodiment of the present utility model provides technical scheme as follows:

On the one hand, provide a kind of composition structure of HIKOUSEN, constitute the main framework of HIKOUSEN by an air bag and control cabinet, appropriate location is organized members such as establishing propelling unit and power control system respectively on this air bag and control cabinet again.Wherein be filled with the gas of control HIKOUSEN lifting in this air bag, and this control cabinet is positioned at this air bag below, is made up of spaces such as control cabin, main cabin and power rooms.This power room is positioned at the control cabinet rear, can establish for the propelling unit group of forming by power fan and some compressors, the power that this power fan provides HIKOUSEN to keep straight on, and described compressor respectively has a nozzle, isogonism is located on this power fan periphery, and ring is when establishing and be divided into left-hand rotation portion and right-hand rotation portion, and then the air-flow that can spray by the compressor nozzle of left-hand rotation portion and right-hand rotation portion, controls the direction of the left and right commentaries on classics of HIKOUSEN.

This power control system comprises some solar panels, an engine controller, dynamo generator, charge controller, accumulate pond, and the member of electrically connect such as inverter.Described solar panels are located at HIKOUSEN outside appropriate location, can be direct current (DC) with solar energy converting, in order to supply the required electric energy of every instrument utensil in this control cabin.This inverter is converted to alternating current with direct current (DC), in order to supply this propelling unit required electric energy, this accumulate pond then can store the electric energy of this solar panels conversion, this charge controller is arranged between this dynamo generator and the accumulate pond, when accumulate pond current potential is inadequate, this charge controller is just opened switch, and when abundance expired rheobase, charge controller was with regard to off switch.When this accumulate pond current potential during, just open electrical generator and do generating again, and, just close electrical generator and do generating when accumulate pond current potential during less than the solar power current potential greater than the solar power current potential.

Embodiment of the present utility model has following beneficial effect:

Use by this propelling unit of supply of electrical energy and the power control system of utilizing described solar panels conversion power generation, not only meet the environmental protection demand, and inexhaustible natural resources, more realistic benefit.And the characteristics such as compressed air stream control heading of utilizing this propelling unit to produce, the convenience of also can promote HIKOUSEN flight, controlling and stability.

Description of drawings

Fig. 1 is the front plan view of HIKOUSEN in the prior art.

Fig. 2 is for commonly using the side plan view of HIKOUSEN in the prior art.

Fig. 3 is the combination view of facing of the present utility model.

Fig. 4 is a side-looking combination view of the present utility model.

Fig. 5 is the square system diagram of the utility model power control system.

Fig. 6 turns to the square system diagram of control for the utility model propelling unit.

The primary clustering nomenclature

Air bag: (10) control cabinet: (20)

Every instrument: (21) propelling unit: (30)

Power fan: (31) compressor: (32)

Blwr: (33) nozzle: (34)

Steering controller: portion is controlled on (35) left side: (351)

Portion is controlled on the right side: (352) power control system: (40)

Solar panels: (41) engine controller: (42)

Dynamo generator: (43) charge controller: (44)

Accumulate pond: (45) inverter: (46)

The specific embodiment

For technical matters, technical scheme and advantage that embodiment of the present utility model will be solved is clearer, be described in detail below in conjunction with the accompanying drawings and the specific embodiments.

See also Fig. 3～shown in Figure 5, its formation of the utility model " the composition structure of HIKOUSEN " comprises: an air bag 10, control cabinet 20, propelling unit 30, and important document such as power control system 40, wherein:

This air bag 10 is the lightweight hull of general appearance cardinal principle ovalize and inboard hollow, inboard except can filling helium or nitrogen, also can as prior art two balloonet (not shown) are set, in order to the lifting of control HIKOUSEN, this is general structure of the prior art, repeats no more.

This control cabinet 20 is located at this air bag 10 belows, is provided with spaces such as control cabin, main cabin and power room in it.Be provided with in this control cabin some in order to every instrument 21 such as " air bag secret room pressure instrument ", " the azimuth compass instrument " of controlling HIKOUSEN, " longitude and latitude instrument ", and this power control system 40 members partly.And this main cabin supplies visitor's activity, and this power room then is positioned at the control cabinet rear, uses for this propelling unit to establish for 30 groups, and this also is a prior art, is not described in detail.

This propelling unit 30 is made up of a power fan 31 and some compressors 32, and respectively this compressor 32 also has a blwr 33 and nozzle 34.The power that this power fan 31 provides HIKOUSEN to keep straight on, and described compressor 32 and blwr 33 and nozzle 34 provided thereon, for isogonism is located on this power fan 31 peripheries, and ring is when establishing and be divided into left-hand rotation portion and right-hand rotation portion, and then the air-flow that can spray by compressor 32 its nozzles 34 of left-hand rotation portion and right-hand rotation portion, the direction of the left and right commentaries on classics of control HIKOUSEN.And respectively this nozzle 34 reveals to evagination, and is connected with this blwr 33, can promote the outwards atmospheric pressure of ejection of this nozzle 34 at double by this blwr 33, and then improve the effect that the air flow jetting promotion turns to.

As shown in Figure 6, what further specify is, when compressor 32 described in the utility model utilizes the air-flow of nozzle 34 ejections to control the change of heading, can be by a steering controller 35 controls, this steering controller 35 also is divided into that portion 351 is controlled on a left side and portion 352 is controlled on the right side, and compressor 32, blwr 33, nozzle 34 that portion 351 and this propelling unit 30 left-hand rotation portions numbering 1～4 are controlled in this left side electrically connect.This right side is controlled portion 352 and is then electrically connected for compressor 32, blwr 33, the nozzle 34 of numbering 5～8.And this left side is controlled portion 351 and the right side and is controlled between the nozzle (34) of portion 352 relative numbering positions (as 1 and 5,2 and 6,3 and 7,4 and 8) and establish the pipeline (not shown) that is communicated with, therefore when a left side of numbering 1.2.3.4 nozzle 34 when left-hand rotation portion is controlled portion 351 and is closed, the atmospheric pressure of described nozzle 34 equals zero, at this time the air pressure of 1 pipeline flows into 5 pipelines, the air pressure of 2 pipelines flows into 6 pipelines, the air pressure of 3 pipelines flows into 7 pipelines, and the air pressure of 4 pipelines flows into 8 pipelines.In like manner, when the right side of the nozzle 34 of right-hand rotation portion numbering 5.6.7.8 was controlled portion 352 and closed, the pressure by air pressure of described nozzle 34 equalled zero, at this time the air pressure of 5 pipelines flows into 1 pipeline, the air pressure of 6 pipelines flows into 2 pipelines, and the air pressure of 7 pipelines flows into 3 pipelines, and the air pressure of 8 pipelines flows into 4 pipelines.

This power control system 40 comprises some solar panels 41, an engine controller 42, a dynamo generator 43, a charge controller 44, an accumulate pond 45, and the member of an electrically connect such as inverter 46, wherein: described solar panels 41 are located at HIKOUSEN outside appropriate location, can be galvanic electric energy with solar energy converting, in order to supply the required electric energy of every instrument utensil in this control cabin.Simultaneously by this inverter 46 direct current (DC) is converted to alternating current again, in order to supply this propelling unit 30 required electric energy.And the energy value of changing when described solar panels 41 is higher than all required electric power of HIKOUSEN, and accumulate pond 4

Under the inadequate situation of 5 current potentials, this charge controller 44 is just opened the electric energy of switch storage by solar energy converting, and when these accumulate pond 45 chargings arrived rheobases, this charge controller 44 was with regard to off switch.

In addition, this engine controller 42 and dynamo generator 43 are electrically connected at these solar panels 41 and accumulate pond 45.When accumulate pond 45 current potentials during, just open electrical generator 43 and do generating, otherwise, just close electrical generator 43 and do generating when accumulate pond 45 current potentials during less than the solar power current potential greater than the solar power current potential.

In view of the above, form, utilize described solar panels 41 converting electrical energies to supply this propelling unit 30, power control system 40 by above-mentioned member, and every electric system of HIKOUSEN is used, not only meet the environmental protection demand, and inexhaustible natural resources, more realistic benefit.And the characteristics such as compressed air stream control heading of utilizing this propelling unit 30 to produce, the convenience of also can promote HIKOUSEN flight, controlling and stability.Compared to the composition structure of traditional HIKOUSEN, the utility model has the characteristics of innovation, practicality and functional promotion really.Utilize solar electrical energy generation, and compressed air stream is controlled characteristics such as heading, the convenience of can promote HIKOUSEN flight, controlling and stability.

The above is a preferred implementation of the present utility model; should be understood that; for those skilled in the art; under the prerequisite that does not break away from principle described in the utility model; can also make some improvements and modifications, these improvements and modifications also should be considered as protection domain of the present utility model.

Claims

1. HIKOUSEN, its formation comprises an air bag, control cabinet, propelling unit, and a power control system, wherein be filled with the gas of control HIKOUSEN lifting in this air bag, and this control cabinet is positioned at this air bag below, has control cabin, main cabin and power room, it is characterized in that:

This propelling unit is located at the power room place at this control cabinet rear, the compressor that is located on this power fan periphery by a power fan and at least one isogonism is formed, the power that this power fan provides HIKOUSEN to keep straight on, and described compressor respectively has a nozzle, described compressor is divided into left-hand rotation and turns right two ones, and control the direction of the left and right commentaries on classics of HIKOUSEN respectively by the air-flow of left-hand rotation portion and the nozzle ejection of right-hand rotation portion;

This power control system comprises at least one solar panels, accumulate pond and inverter at least, and described solar panels are located at HIKOUSEN outside appropriate location, are direct current (DC) with solar energy converting, in order to supply the required electric energy of every instrument utensil in this control cabin; This inverter is converted to alternating current with direct current (DC), and in order to supply this propelling unit required electric energy, this accumulate pond then can store the electric energy of this solar panels conversion.

2. HIKOUSEN according to claim 1 is characterized in that respectively the nozzle of this compressor is equipped with a blwr in addition, and in order to the lifting atmospheric pressure, and then the raising air flow jetting promotes to turn to.

3. HIKOUSEN according to claim 1 and 2, it is characterized in that, when described compressor utilizes the change of nozzle control heading, utilize steering controller control, this steering controller also is divided into that portion is controlled on a left side and portion is controlled on the right side, described compressor, blwr, nozzle that portion and this propelling unit left-hand rotation portion are controlled in this left side electrically connect, and described compressor, blwr, the nozzle electric connection of portion and this propelling unit right-hand rotation portion are controlled in this right side.

4. HIKOUSEN according to claim 1, it is characterized in that, this power control system also comprises an engine controller and dynamo generator, this engine controller is electrically connected at these solar panels, dynamo generator, and the accumulate pond, when accumulate pond current potential during, just open electrical generator and do generating greater than the solar power current potential, and, just close electrical generator and do generating when accumulate pond current potential during less than the solar power current potential.

5. according to claim 1 or 4 described HIKOUSENs, it is characterized in that, this power control system also comprises a charge controller, this charge controller is arranged between this dynamo generator and the accumulate pond, when cell potential is inadequate, this charge controller is just opened switch, and when abundance expired rheobase, charge controller was with regard to off switch.