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WO2008110059A1 - Moteur de rotor - Google Patents

Moteur de rotor Download PDF

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Publication number
WO2008110059A1
WO2008110059A1 PCT/CN2008/000394 CN2008000394W WO2008110059A1 WO 2008110059 A1 WO2008110059 A1 WO 2008110059A1 CN 2008000394 W CN2008000394 W CN 2008000394W WO 2008110059 A1 WO2008110059 A1 WO 2008110059A1
Authority
WO
WIPO (PCT)
Prior art keywords
transmission
state
chamber
rotor
gear
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/CN2008/000394
Other languages
English (en)
Chinese (zh)
Inventor
Weijia Chen
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.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Publication of WO2008110059A1 publication Critical patent/WO2008110059A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/02—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F01C1/063—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them

Definitions

  • the invention relates to a rotary engine.
  • the scissor structure has a four-stroke process
  • the force generated after ignition causes the left and right blades to move in two opposite directions.
  • the blades have a certain inertia, the two blades do not have the same direction on the same output shaft. Therefore, it is impossible for the left and right blades of the engine to maintain normal rotation in the same direction, and it is impossible to directly change the kinetic energy generated by the fuel into rotational kinetic energy.
  • the object of the present invention is to provide a rotor engine which uses the flywheel inertia to alternately counteract the forces in the opposite direction of the rear wheel, so that the two rotors can rotate in the same direction to achieve continuous operation of the rotor engine.
  • a rotary engine including a rotary engine that is driven by a transmission to have a power output device, the transmission also driving a boosting device.
  • a further technical solution of the present invention is: a rotor engine including a rotor engine, the rotor engine being driven by a transmission device having a power output device, the transmission device also driving a boosting device; the transmission device simultaneously driving the boosting device and The power output device may also respectively drive the boosting device and the power output device;
  • the transmission device has two, the two transmission devices are respectively mounted on the output shafts of the two rotors; the transmission device is a one-stage or multi-stage gear transmission mechanism
  • the boosting device is a booster flywheel, and the booster flywheel is respectively disposed on the last stage of the transmission shaft of the transmission; the gear in the transmission is a circular gear or an elliptical gear.
  • the present invention solves the fundamental problem that the scissors device cannot be continuously operated, so that the rotor engine can be realized.
  • the first stage gear is in an active state, and the corresponding booster flywheel is in a passive state, thereby assisting the flywheel to be accelerated and storing kinetic energy, when the rotor is turned
  • the corresponding booster flywheel is in an active state, and the rotor is in a passive state, thereby boosting the flywheel to release the kinetic energy required to push the rotor forward, and the two booster flywheels alternately act to keep the engine rotating.
  • the output flywheel can rotate at a constant speed, balancing torque and energy output.
  • Figure 1 is a frame diagram of the prior art
  • Embodiment 1 of the present invention is a frame diagram of Embodiment 1 of the present invention.
  • Embodiment 2 of the present invention is a frame diagram of Embodiment 2 of the present invention.
  • Embodiment 1 of the present invention is a schematic structural view of Embodiment 1 of the present invention.
  • FIG. 5 is a schematic structural diagram of Embodiment 2 of the present invention.
  • 6 to 13 are schematic views showing the state of use of the present invention.
  • a rotor engine includes a rotor engine 10, and output shafts 5 and 51 of two rotors 4 and 41 of a rotor engine are respectively mounted with a transmission device 1, and the transmission device 1 includes a driving gear 81, two driven gears 82 respectively meshing with the driving gear 81, the two driven gears 82 respectively drive the boosting device 3 and the power output device 2;
  • the boosting device 3 is a boosting flywheel 6 and 61, a boosting flywheel 6 and 61 is disposed on the passive transmission shafts 7 and 71;
  • the other two passive transmission shafts 72 and 73 of the two transmissions 1 are coaxially disposed and coaxially provided with the output flywheel 9.
  • a rotor engine includes a rotor engine 10, and output shafts 5 and 51 of two rotors 4 and 41 of a rotor engine are respectively mounted with a transmission device 1 respectively.
  • the two sets of coaxial primary gear transmission mechanisms 83 and 84 are included, and two sets of coaxial primary gear transmission mechanisms 83 and 84 drive the boosting device 3 and the power output device 2, respectively;
  • the boosting device 3 is a boosting flywheel 6 and 61.
  • the booster flywheels 6 and 61 are disposed on the corresponding passive drive shafts 7 and 71; the other two passive drive shafts 72 and 73 of the two transmissions 1 are coaxially disposed and coaxially provided with the output flywheel 9.
  • the transmission 1 described above can also be a multi-stage gear transmission, and the booster flywheels 6 and 61 are disposed on the last stage of the transmission shaft of the transmission 1.
  • the gear 8 in the transmission device 1 may be a circular gear or an elliptical gear.
  • each rotor comprises two spaced apart spacers in the same cross section, wherein the spacer E and the spacer G are one rotor, and the spacer F and the spacer H are another
  • the rotor, the movement steps of the present invention are as follows:
  • the chamber A is in the state when the work is completed; the chamber B is in the state when the exhaust is completed; the chamber C is in the state when the suction is completed; and the chamber D is in the state of being compressed to the minimum. ;
  • the ignition or nozzle device is ignited in chamber D, at which time chamber A is in an exhaust state; chamber B is in an inhaled state; chamber C is in a compressed state; chamber D is in operation Work state
  • the chamber A is in the state when the exhaust is completed; the chamber B is in the state when the suction is completed; the chamber C is in the state of being compressed to the minimum; the chamber D is in the state when the work is completed. ;
  • the ignition or nozzle device is ignited in chamber C, at which time chamber A is in an inhaled state; chamber B is in a compressed state; chamber C is in a working state; chamber D is in Exhaust state
  • the chamber A is in the state when the suction is completed; the chamber B is in the state of being compressed to the minimum; the chamber C is in the state when the work is completed; and the chamber D is in the state when the exhaust is completed. ;
  • the ignition or nozzle device is ignited in chamber B, at which time chamber A is in a compressed state; chamber B is in a working state; chamber C is in an exhaust state; chamber D is in a suction state Gas state
  • the chamber A is in a state of being compressed to a minimum; the chamber B is in a state where the work is completed; the chamber C is in a state in which the exhaust is completed; and the chamber D is at the time of completion of the intake. State
  • the ignition or nozzle device is ignited in chamber A, at which time chamber A is in a working state; chamber B is in an exhaust state; chamber C is in an inhaled state; chamber D is in Compressed state
  • the first stage drive gear 81 when one of the rotors 4 is accelerated as the front pusher, the first stage drive gear 81 is in an active state, and the corresponding booster flywheel 6 is in a passive state, so that the booster flywheel 6 is accelerated and stores kinetic energy when the rotor 4
  • the corresponding booster flywheel 6 is in an active state, and the rotor 4 is in a passive state, so that the booster flywheel 6 releases the kinetic energy required to push the rotor 4 forward, and the two booster flywheels 6 and 61 alternates to keep the engine spinning.
  • the output flywheel 9 can rotate at a constant speed to balance torque and energy output.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Supercharger (AREA)

Abstract

L'invention concerne un moteur (10) de rotor comprenant un dispositif d'entraînement (1) et un dispositif de sortie de puissance (2). Le moteur (10) de rotor entraîne le dispositif de sûreté de puissance (2) à l'aide du dispositif d'entraînement (1), qui entraîne, à son tour, le dispositif auxiliaire d'entraînement (3) de sorte que les pistons circulaires tournent dans la même direction, assurant ainsi un fonctionnement continu du moteur de rotor (10).
PCT/CN2008/000394 2007-03-15 2008-02-25 Moteur de rotor Ceased WO2008110059A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN200710020286.X 2007-03-15
CNA200710020286XA CN101046156A (zh) 2007-03-15 2007-03-15 带助推飞轮的转子发动机

Publications (1)

Publication Number Publication Date
WO2008110059A1 true WO2008110059A1 (fr) 2008-09-18

Family

ID=38771040

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2008/000394 Ceased WO2008110059A1 (fr) 2007-03-15 2008-02-25 Moteur de rotor

Country Status (2)

Country Link
CN (1) CN101046156A (fr)
WO (1) WO2008110059A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102168747B (zh) * 2011-03-24 2013-10-02 中国人民解放军国防科学技术大学 定轴轮系与非匀速传动机构组合的功率传输装置

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2106224U (zh) * 1990-11-15 1992-06-03 牟均福 全循环旋转活塞式内燃机
US5429085A (en) * 1993-11-16 1995-07-04 Stauffer; John E. Timing mechanism for rotary engines
CN1180136A (zh) * 1997-01-14 1998-04-29 伏伟 平面四杆机构控制的全密封组合转子发动机
JPH1162605A (ja) * 1997-08-13 1999-03-05 Chota Yanagi 回転式内燃機関
US6305345B1 (en) * 2000-03-11 2001-10-23 Igor V. Bakhtine High-output robust rotary engine with a symmetrical drive and improved combustion efficiency having a low manufacturing cost
CN1490495A (zh) * 2002-10-16 2004-04-21 姚乃刚 转子发动机
CN1564906A (zh) * 2002-07-01 2005-01-12 方骏兴 轮步旋转活塞式发动机

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2106224U (zh) * 1990-11-15 1992-06-03 牟均福 全循环旋转活塞式内燃机
US5429085A (en) * 1993-11-16 1995-07-04 Stauffer; John E. Timing mechanism for rotary engines
CN1180136A (zh) * 1997-01-14 1998-04-29 伏伟 平面四杆机构控制的全密封组合转子发动机
JPH1162605A (ja) * 1997-08-13 1999-03-05 Chota Yanagi 回転式内燃機関
US6305345B1 (en) * 2000-03-11 2001-10-23 Igor V. Bakhtine High-output robust rotary engine with a symmetrical drive and improved combustion efficiency having a low manufacturing cost
CN1564906A (zh) * 2002-07-01 2005-01-12 方骏兴 轮步旋转活塞式发动机
CN1490495A (zh) * 2002-10-16 2004-04-21 姚乃刚 转子发动机

Also Published As

Publication number Publication date
CN101046156A (zh) 2007-10-03

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