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WO2013184549A1 - Rotary energy transducer - Google Patents

Rotary energy transducer Download PDF

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Publication number
WO2013184549A1
WO2013184549A1 PCT/US2013/043834 US2013043834W WO2013184549A1 WO 2013184549 A1 WO2013184549 A1 WO 2013184549A1 US 2013043834 W US2013043834 W US 2013043834W WO 2013184549 A1 WO2013184549 A1 WO 2013184549A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
chambers
crankshaft
injector
energy transducer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2013/043834
Other languages
French (fr)
Inventor
Lawrence MCMILLAN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WILKINSON Cassandra L
Original Assignee
WILKINSON Cassandra L
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US13/488,998 external-priority patent/US20130239920A1/en
Application filed by WILKINSON Cassandra L filed Critical WILKINSON Cassandra L
Publication of WO2013184549A1 publication Critical patent/WO2013184549A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust

Definitions

  • This invention relates generally to an energy transducer, and more particularly, but not by way of limitation, to a hydrogen powered rotary energy transducer.
  • the invention reiates to an energy transducer comprising: a body; a crankshaft; a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft; one or more chambers located circumferentially around the rotor; an injector connected to the body such that the injector injects fuel into the one or more chambers; and an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate.
  • the fuel may be hydrogen or a mixture of hydrogen and oxygen.
  • the one or more chambers may be each angled inward toward the direction of travel of the rotor.
  • the energy transducer may further comprise a hydrogen control valve connected to the injector to control the amount of fuel injected into the one or more chambers.
  • the igniter and the hydrogen control valve may be controlled by an electronic controller, which may be controlled by a throttle.
  • the energy transducer may further comprising multiple bodies and a common crankshaft, each body with: a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft; one or more chambers located circumferentially around the rotor; an injector connected to the body such that the injector injects fuel into the one or more chambers; and an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate.
  • the igniter may be located adjacent the injector, but further along a path of rotation of the rotor.
  • the energy transducer may further comprising an exhaust port located within the body such that the exhaust port is capable of venting exhaust from the one or more chambers, and the exhaust port may be located adjacent the injector, but prior to the injector along a path of rotation of the rotor.
  • a method of transducing energy using the energy transducer may comprise: providing a body, a crankshaft, a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft, and one or more chambers located circumferentially around the rotor; injecting foe! into one of the chambers via an injector connected to the body; igniting the fuel in the chamber with an igniter, causing an explosion; and allowing the explosion to force the rotor and crankshaft to rotate.
  • the fuel may be hydrogen or a mixture of hydrogen and oxygen.
  • the method may further comprise controlling the amount of fuel injected into the one or more chambers with a hydrogen control valve, and controlling the igniter and the hydrogen control valve with an electronic controller.
  • the method may further comprise controlling the electronic controller via a throttle.
  • the method may further comprise venting exhaust from the chamber via an exhaust port. Finally, the method may further comprise repeating said injecting, igniting, and allowing steps cyclically for each of the one or more chambers.
  • Figure 1 is diagrammatic view of the energy transducer described herein;
  • Figure 2 is a diagrammatic view of the energy transducer at the beginning of a cycle:
  • Figure 3 is a diagrammatic view of the energy transducer partway through a cycle.
  • Figure 4 is a side diagrammatic view of the energy transducer.
  • the invention in general, in a first aspect, relates to a hydrogen powered rotary energy transducer.
  • the energy transducer utilizes hydrogen rather than fossil fuels, capturing the energy within the hydrogen.
  • hydrogen may refer to a mixture of hydrogen and oxygen.
  • the energy from the hydrogen is converted to power by a pump, such as a piston pump, rotary pump, thrust pump, or gear pump.
  • the energy transducer may utilize a single pump or multiple pumps in any configuration.
  • Figures 1 through 4 show a single rotary pump, comprising a body I , a rotor 2, and a crankshaft 1 1.
  • the energy transducer may comprise a body 1 housing the rotor 2 such that the rotor 2 may freely rotate within the body 1 along an axis defined by the crankshaft 1 1 .
  • One or more chambers 3 may be located circumferentially around the rotor 2. The chambers 3 may be angled inward toward the direction of travel of the rotor 2, as seen in Figures 1 through 3.
  • a direct injector 5 may be connected to the body 1 such that the direct injector 5 may inject hydrogen into the chambers 3 one at a time as the rotor 2 rotates.
  • a hydrogen control valve 7 may be connected to the direct mjector 5 to control the amount of hydrogen injected into the chambers 3.
  • a hydrogen storage tank 10 may be in fluid communication with the direct injector 5 via the hydrogen control valve 7.
  • An igniter 4 such as a spark plug, may likewise be connected to the body 1 such that the igniter 4 may ignite the hydrogen within the chamber 3.
  • the igniter 4 may be located near the injector 5, but further along the path of rotation of the rotor 2.
  • the igniter 4 may be out of phase with the injector 5, such that when a chamber 3 is aligned with the igniter 4, there is not a chamber 3 aiigned with the injector 5; likewise, when a chamber 3 is aligned with the injector 5, there is not a chamber 3 aiigned with the igniter 4.
  • An exhaust port 6 may also be located within the body 1 such that it may vent exhaust from the chambers 3 after ignition.
  • the exhaust port 6 may be located near the injector 5, but before the injector 5 along the path of rotation of the rotor 2.
  • the exhaust port 6 may also be out of phase with the injector 5, such that when a chamber 3 is aiigned with the exhaust port 6, there is not a chamber 3 aligned with the injector 5, and when a chamber 3 is aligned with the injector 5, there is not a chamber 3 aligned with the exhaust port 6.
  • An electronic controller 8 may be connected to the igniter 4 and the hydrogen control valve 7, thus controlling the overall function of the transducer, ' [ ' he electronic controller 8 may be connected to a throttle 9, such that an operator of a vehicle utilizing the transducer may control the transducer via the throttle 9.
  • the rotor 2 begins with a chamber 3 aligned with the injector 5.
  • the injector 5 injects hydrogen into one of the chambers 3.
  • the rotor 2 rotates such that the chamber 3 bearing hydrogen is aligned with the igniter 4.
  • the igniter 4 fires, causing the hydrogen in the chamber 3 to explode.
  • This explosion forces the rotor 2 to rotate, which in turn causes the crankshaft 1 1 to rotate. This movement may be seen in Figures 2 and 3.
  • exhaust is removed from the chamber 3.
  • the process is repeated cyclically for each of the chambers 3.
  • the energy/RPMs of the energy transducer may be controlled by the timing and/or size of the explosion of the hydrogen.
  • the size of the chambers 3 is not important; the size of the rotor 2 controls the amount of power it makes.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Description

ROTARY ENERGY TRANSDUCER
BACKGROUND OF THE INVENTION
Field of the Invention.
[0001] This invention relates generally to an energy transducer, and more particularly, but not by way of limitation, to a hydrogen powered rotary energy transducer.
Description of the Related Art.
[0002] Internal combustion engines, such as those used in automobiles, typically run on gasoline or other fossil fuel. Such an engine consumes 75% of the energy it produces to perform its task, leaving only 25% of the energy for usable power.
[0003] It is desirable to provide an energy transducer that does not depend on fossil fuel.
[0004] It is further desirable for such an energy transducer to run on hydrogen.
[0005] It is further desirable for such an energy transducer to allow for greater utilization of the energy it creates.
SUMMARY OF THE INVENTION
[0006] In general, in a first aspect, the invention reiates to an energy transducer comprising: a body; a crankshaft; a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft; one or more chambers located circumferentially around the rotor; an injector connected to the body such that the injector injects fuel into the one or more chambers; and an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate. The fuel may be hydrogen or a mixture of hydrogen and oxygen. The one or more chambers may be each angled inward toward the direction of travel of the rotor.
[0007] The energy transducer may further comprise a hydrogen control valve connected to the injector to control the amount of fuel injected into the one or more chambers. The igniter and the hydrogen control valve may be controlled by an electronic controller, which may be controlled by a throttle.
[0008] The energy transducer may further comprising multiple bodies and a common crankshaft, each body with: a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft; one or more chambers located circumferentially around the rotor; an injector connected to the body such that the injector injects fuel into the one or more chambers; and an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate.
[0010] The igniter may be located adjacent the injector, but further along a path of rotation of the rotor. The energy transducer may further comprising an exhaust port located within the body such that the exhaust port is capable of venting exhaust from the one or more chambers, and the exhaust port may be located adjacent the injector, but prior to the injector along a path of rotation of the rotor.
[00 i 1 j A method of transducing energy using the energy transducer may comprise: providing a body, a crankshaft, a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft, and one or more chambers located circumferentially around the rotor; injecting foe! into one of the chambers via an injector connected to the body; igniting the fuel in the chamber with an igniter, causing an explosion; and allowing the explosion to force the rotor and crankshaft to rotate. The fuel may be hydrogen or a mixture of hydrogen and oxygen.
[0012] The method may further comprise controlling the amount of fuel injected into the one or more chambers with a hydrogen control valve, and controlling the igniter and the hydrogen control valve with an electronic controller. The method may further comprise controlling the electronic controller via a throttle.
[0013] The method may further comprise venting exhaust from the chamber via an exhaust port. Finally, the method may further comprise repeating said injecting, igniting, and allowing steps cyclically for each of the one or more chambers.
BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Figure 1 is diagrammatic view of the energy transducer described herein;
[0015] Figure 2 is a diagrammatic view of the energy transducer at the beginning of a cycle:
[0016] Figure 3 is a diagrammatic view of the energy transducer partway through a cycle; and
[0017] Figure 4 is a side diagrammatic view of the energy transducer.
[001 8] Other advantages and features will be apparent from the following description and from the claims.
DETAILED DESCRIPTION OF THE INVENTION
[0019] The devices and methods discussed herein are merely illustrative of specific manners in which to make and use this invention and are not to be interpreted as limiting in scope.
[0020] While the devices and methods have been described with a certain degree of particularity, it is to be noted that many modifications may be made in the details of the construction and the arrangement of the devices and components without departing from the spirit and scope of this disclosure, it is understood that the devices and methods are not limited to the embodiments set forth herein for purposes of exemplification.
[0021] In general, in a first aspect, the invention relates to a hydrogen powered rotary energy transducer. The energy transducer utilizes hydrogen rather than fossil fuels, capturing the energy within the hydrogen. As used herein, hydrogen may refer to a mixture of hydrogen and oxygen. In the present invention, the energy from the hydrogen is converted to power by a pump, such as a piston pump, rotary pump, thrust pump, or gear pump. The energy transducer may utilize a single pump or multiple pumps in any configuration. Figures 1 through 4 show a single rotary pump, comprising a body I , a rotor 2, and a crankshaft 1 1.
[0022] The energy transducer may comprise a body 1 housing the rotor 2 such that the rotor 2 may freely rotate within the body 1 along an axis defined by the crankshaft 1 1 . One or more chambers 3 may be located circumferentially around the rotor 2. The chambers 3 may be angled inward toward the direction of travel of the rotor 2, as seen in Figures 1 through 3. A direct injector 5 may be connected to the body 1 such that the direct injector 5 may inject hydrogen into the chambers 3 one at a time as the rotor 2 rotates. A hydrogen control valve 7 may be connected to the direct mjector 5 to control the amount of hydrogen injected into the chambers 3. A hydrogen storage tank 10 may be in fluid communication with the direct injector 5 via the hydrogen control valve 7. [0023] An igniter 4, such as a spark plug, may likewise be connected to the body 1 such that the igniter 4 may ignite the hydrogen within the chamber 3. The igniter 4 may be located near the injector 5, but further along the path of rotation of the rotor 2. The igniter 4 may be out of phase with the injector 5, such that when a chamber 3 is aligned with the igniter 4, there is not a chamber 3 aiigned with the injector 5; likewise, when a chamber 3 is aligned with the injector 5, there is not a chamber 3 aiigned with the igniter 4. An exhaust port 6 may also be located within the body 1 such that it may vent exhaust from the chambers 3 after ignition. The exhaust port 6 may be located near the injector 5, but before the injector 5 along the path of rotation of the rotor 2. The exhaust port 6 may also be out of phase with the injector 5, such that when a chamber 3 is aiigned with the exhaust port 6, there is not a chamber 3 aligned with the injector 5, and when a chamber 3 is aligned with the injector 5, there is not a chamber 3 aligned with the exhaust port 6. An electronic controller 8 may be connected to the igniter 4 and the hydrogen control valve 7, thus controlling the overall function of the transducer, '['he electronic controller 8 may be connected to a throttle 9, such that an operator of a vehicle utilizing the transducer may control the transducer via the throttle 9.
[0024] In use, the rotor 2 begins with a chamber 3 aligned with the injector 5. The injector 5 injects hydrogen into one of the chambers 3. The rotor 2 rotates such that the chamber 3 bearing hydrogen is aligned with the igniter 4. The igniter 4 fires, causing the hydrogen in the chamber 3 to explode. This explosion forces the rotor 2 to rotate, which in turn causes the crankshaft 1 1 to rotate. This movement may be seen in Figures 2 and 3. When the chamber 3 in which the explosion occurred reaches the exhaust port 6, exhaust is removed from the chamber 3. The process is repeated cyclically for each of the chambers 3. [0025] The energy/RPMs of the energy transducer may be controlled by the timing and/or size of the explosion of the hydrogen. The size of the chambers 3 is not important; the size of the rotor 2 controls the amount of power it makes.
[0026] Whereas, the devices and methods have been described in relation to the drawings and claims, it should be understood that other and further modifications, apart from those shown or suggested herein, may be made within the spirit and scope of this invention.

Claims

WHAT IS CLAIMED !S:
1. An energy transducer comprising:
a body;
a crankshaft;
a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft;
one or more chambers located circumferentiaiiy around the rotor;
an injector connected to the body such that the injector injects fuel into the one or more chambers; and
an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate. 2. The energy transducer of Claim 1 where the fuel is hydrogen or a mixture of hydrogen and oxygen. 3. The energy transducer of Claim 1 where the one or more chambers are each angied inward toward a direction of travel of the rotor. 4. The energy transducer of Claim 1 further comprising a hydrogen control valve connected to the injector to control the amount of fuel injected into the one or more chambers. 5. The energy transducer of Claim 4 where the igniter and the hydrogen control valve are controlled by an electronic controller.
6. The energy transducer of Claim 5 where the electronic controller is controlled by a throttle. 7. The energy transducer of Claim 1 further comprising multiple bodies and a common crankshaft, each body with:
a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft;
one or more chambers located circumferentia!ly around the rotor;
an injector connected to the body such that the injector injects fuel into the one or more chambers; and
an igniter connected to the body such that the igniter ignites the fuel in the one or more chambers, which causes the rotor to rotate. 8. The energy transducer of Claim 1 where the igniter is located adjacent the injector. but further along a path of rotation of the rotor. 9. The energy transducer of Claim 1 further comprising an exhaust port located within the body such that the exhaust port is capable of venting exhaust from the one or more chambers. 10. The energy transducer of Claim 9 where the exhaust port is located adjacent the injector, but prior to the injector along a path of rotation of the rotor. 1 1. A method of transducing energy, the method comprisin
providing: a body;
a crankshaft;
a rotor mounted to the crankshaft and housed within the body such that the rotor may rotate within the body along an axis defined by the crankshaft; and
more chambers located circumferentially around the rotor; injecting fuel into one of the chambers via an injector connected to the body; igniting the fuel in the chamber with an igniter, causing an explosion; and allowing the explosion to force the rotor and crankshaft to rotate.
32. The method of Claim 1 1 where the fuel is hydrogen or a mixture of hydrogen and oxygen.
13. The method of Claim 1 1 where the method further comprises controlling amount of fuel injected into the one or more chambers with a hydrogen control valve.
14. The method of Claim 13 further comprising controlling the igniter and the hydrogen control valve with an electronic controller.
15. The method of Claim 14 further comprising controlling the eiectronic controller via a throttle.
16. The method of Claim 11 further comprising venting exhaust from the chamber via an exhaust port.
17. The method of Claim I I further comprising repealing said injecting, igniting, and allowing steps cyclically for each of the one or more chambers.
PCT/US2013/043834 2012-06-05 2013-06-03 Rotary energy transducer Ceased WO2013184549A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/488,998 2012-06-05
US13/488,998 US20130239920A1 (en) 2011-05-06 2012-06-05 Rotary energy transducer

Publications (1)

Publication Number Publication Date
WO2013184549A1 true WO2013184549A1 (en) 2013-12-12

Family

ID=49712522

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/043834 Ceased WO2013184549A1 (en) 2012-06-05 2013-06-03 Rotary energy transducer

Country Status (1)

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WO (1) WO2013184549A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11807645B2 (en) 2015-05-14 2023-11-07 Eni S.P.A. Polymers containing indacen-4-one derivatives

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005273505A (en) * 2004-03-24 2005-10-06 Omunitekku:Kk Multi-air space type rotary engine
WO2006088289A1 (en) * 2005-02-17 2006-08-24 Woo Gyoon Kim Free piston rotary engine
US20070068481A1 (en) * 2004-07-14 2007-03-29 Campbell Robert L Concentric internal combustion rotary engine
US20090194065A1 (en) * 2006-05-09 2009-08-06 Okamura Yugen Kaisha Rotary Piston Type Internal Combustion Engine
US20110083637A1 (en) * 2009-10-08 2011-04-14 Blount David H Rotary double engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005273505A (en) * 2004-03-24 2005-10-06 Omunitekku:Kk Multi-air space type rotary engine
US20070068481A1 (en) * 2004-07-14 2007-03-29 Campbell Robert L Concentric internal combustion rotary engine
WO2006088289A1 (en) * 2005-02-17 2006-08-24 Woo Gyoon Kim Free piston rotary engine
US20090194065A1 (en) * 2006-05-09 2009-08-06 Okamura Yugen Kaisha Rotary Piston Type Internal Combustion Engine
US20110083637A1 (en) * 2009-10-08 2011-04-14 Blount David H Rotary double engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11807645B2 (en) 2015-05-14 2023-11-07 Eni S.P.A. Polymers containing indacen-4-one derivatives

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