EP0424104A1 - Moteur rotatif - Google Patents

Moteur rotatif Download PDF

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Publication number
EP0424104A1
EP0424104A1 EP90311339A EP90311339A EP0424104A1 EP 0424104 A1 EP0424104 A1 EP 0424104A1 EP 90311339 A EP90311339 A EP 90311339A EP 90311339 A EP90311339 A EP 90311339A EP 0424104 A1 EP0424104 A1 EP 0424104A1
Authority
EP
European Patent Office
Prior art keywords
rotor
rotary engine
chamber
explosion
housing
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.)
Withdrawn
Application number
EP90311339A
Other languages
German (de)
English (en)
Inventor
Kaoru Hayashitani
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
Priority claimed from JP4213290A external-priority patent/JPH0730706B2/ja
Priority claimed from JP5621090U external-priority patent/JPH0717788Y2/ja
Application filed by Individual filed Critical Individual
Publication of EP0424104A1 publication Critical patent/EP0424104A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • 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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F01C21/0809—Construction of vanes or vane holders
    • F01C21/0818—Vane tracking; control therefor
    • F01C21/0854—Vane tracking; control therefor by fluid means
    • F01C21/0863—Vane tracking; control therefor by fluid means the fluid being the working fluid
    • 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
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F01C1/3446—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface

Definitions

  • the present invention relates to a rotary engine wherein the forms of a housing and a rotor rotating in the housing are simple, a capacity ratio of a suction chamber and a combustion chamber can be freely set, blades in blade channels which are in radial directions and which go through the center of the rotor are closely in contact with the inside surface of the housing, and the gap between a blade separating a compression chamber from an explosion chamber and the inside surface of the housing is not enlarged by explosion pressure in the explosion chamber and the explosion pressure does not leak in the compression chamber, so that explosion at an inappropriate time is prevented, stable rotation is obtained, and the fuel consumption can be substantially saved and improved.
  • a rotary engine of this kind which has been put to practical use is a Wankel-type rotary engine.
  • a Wankel-type rotary engine a triangular rotor the surface of which is made up of peritrochoid internal envelope is rotated along the inside wall of a cocoon-shaped housing made up of peritrochoidal curve, and when an internal gear disposed in the middle of the rotor is engaged with and rotates around a fixed external gear, an output axis having an eccentric rotor axis neck portion is rotated.
  • a rotor made up of peritrochoid internal envelope is rotated along the inside wall of a housing made up of peritrochoidal curve, the maximum capacity of a suction chamber and the maximum capacity of a combustion chamber is the same, fuel mixture sucked in the suction chamber is compressed and has the minimum capacity, the fuel mixture is ignited and explodes at that time, the explosion force rotates the rotor, and the fuel mixture having the minimum capacity explodes in the combustion chamber the capacity of which is the same as the maximum capacity of the suction chamber. Accordingly, part of the explosion energy is used to rotate the rotor, but the rest of the explosion energy is discharged from an exhaust hole without being used.
  • a Wankel-type rotary engine has, therefore, a fault that, since explosion energy which is available can not be effectively used and radiated without being used, the thermal efficiency is low and the cost of fuel is high.
  • a Wankel-type rotary engine also has a structural fault that one rotation of a rotor generates only one explosion of energy.
  • an apex seal as a gas seal is inserted and engaged at each of the apexes of the triangular rotor through an elastic member so that the apex seals may rise and sink freely and may be closely in contact with the inside wall of a housing.
  • the inside wall of a housing along which the rotor rotates is symmetrical. Since the maximum capacity of a suction chamber and the maximum capacity of a combustion chamber is the same, this kind of a rotary engine has the same fault as that of a conventional rotary engine.
  • gas seal for maintaining airtightness between the tip portions of blades and the inside wall of a housing is attained by pushing the blades in blade channels outward from a rotor against the inside wall of a housing by elasticity of springs or by centrifugal force acting on the blades.
  • the present invention is to enlarge part of the inside radius of a sylinder-like housing having sylinder-like inside wall, form a suction chamber and a combustion chamber, dispose a suction hole at the former end portion of the suction chamber, an ignition device at the former end portion of the combustion chamber, and an exhaust hole at the latter end portion of the combustion chamber, respectively, make the capacity of the combustion chamber large compared with the capacity of the suction chamber, insert and engage blades which can advance and retreat freely in the direction toward the inside wall of the housing in blade channels in radial directions which go through the center of a cylinder-like rotor capable of being inserted and engaged in the sylinder-like housing, and form protruding portions on the surface of the rotor in front of and at the back of the blade channels going through the center of the rotor in the rotation direction of the rotor which protruding portions are closely in contact with the circular inside surface of a connection portion of a compression chamber and the combustion chamber of the housing.
  • a first object of the present invention is to provide a rotary engine which can attain a maximum energy efficiency in which a suction chamber and a combustion chamber are formed by enlarging part of the inside radius of a cyliner-like housing having cyliner-like inside wall, and the capacity ratio of the suction chamber and the combustion chamber can be freely set and explosion energy can be effectively transformed into rotation energy.
  • a second object of the present invention is to provide an effective rotary engine with small mechanical loss wherein a rotor begins circular rotation movement directly by explosion energy and no transmission means such as a gear is necessary.
  • a third object of the present invention is to provide a rotary engine wherein a gap between a tip of a blade separating a compression chamber from an explosion chamber and the circular inside surface of a connection portion of the compression chamber and the combustion chamber of the housing which tip of a blade and inside surface of the connection portion are in close contact with each other is not enlarged by explosion pressure and compressed gas does not explode in the compression chamber, that is, does not explode at an inappropriate time and a rotor rotates with stability.
  • a fourth object of the present invention is to provide a rotary engine wherein each of suction, compression, explosion and discharge processes occurs continuously in each chamber separated from each other by blades during one rotation of a rotor, thus the rotor rotates without nonuniformity, and explosion energy can smoothly be transformed into rotation energy.
  • springs lie in blade channels in radial directions of a rotor.
  • a housing 1 comprises a cylinder-like body 2 having cylinder-­like inside wall 3.
  • the inside radius of two inside surface portions opposite to each other are enlarged to form portions of a concentric circle of the circle formed by the cylinder-like inside wall 3, one portion being about 30° by central angle and the other portion being about 60° by central angle. Both of the end portions of the enlarged portions smoothly lead to the cylinder-like inside wall 3 and a suction chamber 4 and a combustion chamber 5 are formed.
  • the combustion chamber 5 has larger capacity than the suction chamber 4.
  • a rotor 6 is cylinder-like and inserted and engaged in the cylinder-like inside wall 3. Blade channels 7 are radially bored so as to go through the center of the rotor 6 and to be at right angles to each other.
  • Each of blades 9 is inserted and engaged in each of the blade channels 7 divided into equal two portions.
  • an apex seal made of new ceramic (not shown) is inserted and engaged so as to maintain the airtightness and to decrease friction between itself and the inside surface of the housing 1.
  • a seal 10 for containing explosion pressure as shown in Fig. 3 is additionally provided, so as to prevent explosion pressure from leaking in the base end portion through the blade channels 7.
  • Springs 11 lie between the base ends of the blades 9 and the bottom portion 8 where the blade channels 7 cross each other.
  • the springs 11 are for pushing the tip portions of the blades 9 against the inside surface of the housing 1 mainly when the rotor 6 is not in motion and when the rotor 6 rotates at a low speed.
  • the springs When the rotor 6 rotates at a high speed, coupled with centrifugal force which acts on each of the blades 9, the springs further maintain the airtightness between each of the tips of the blades 9 and the inside surface of the housing 1.
  • the springs 11 can be omitted.
  • Air suction hole 12 is bored in the housing 1 at the former end portion of the suction chamber 4 in the rotation direction a of the rotor 6 and suck fuel mixture.
  • the air suction hole 12 may be a blowing system provided with a fuel injection equipment.
  • An ignition equipment 13 is provided in the housing 1 at the former end portion of the combustion chamber 5 in the rotation direction a of the rotor 6 and comprises a spark plug, etc (not shown).
  • the ignition equipment 13 is for igniting and exploding the fuel mixture sucked from the air suction hole 12 by compressing the fuel mixture at the former end portion of the combustion chamber 5 with blades 9 according to the rotation of the rotor 6.
  • the compressed fuel mixture is ignited and exploded at the former end portion of the combustion chamber 5, the areas of the blades 9 which are adjacent to each other and which form the explosion chamber 5a with airtightness at the former end side of the combustion chamber 5 are different, and due to the difference of the explosion pressure which acts on the blades 9, the rotor 6 is rotated.
  • An exhaust hole 14 is bored in the housing 1 at the latter end portion of the combustion chamber 5 in the rotation direction a .
  • the exhaust hole 14 is for discharging exhaust gas which is exploded and burned when the compressed fuel mixture is ignited and exploded at the side of the former end portion of the combustion chamber 5.
  • Hollows 15 the section of which is arc-like, etc. bored on the surface of the rotor 6 at the back of each of the blade channels 7 in the rotation direction of the rotor 6 adjacent to each of the blade channels 7 are for adjusting the compressibility.
  • the hollows 15 may be bored in the direction of the circumference of the surface of the rotor 6 so as to reach the adjacent blade channels 7 or the vicinity of the adjacent blade channels 7, and may additionally have the function as channels which maintain fuel mixture compressed in the compression chamber 4b at the side of the latter end of the suction chamber 4 by the blades 9 due to the rotation of the rotor 6 after being sucked in the air suction chamber 4a at the side of the former end of the suction chamber 4 and which moves the fuel mixture to the explosion chamber 5a at the former end of the combustion chamber 5.
  • the inside diameters of a lower portion of one side of the cylinder-like inside wall 3 of the housing 1 and a portion from an upper portion to a lower portion of the other side of the cylinder-like inside wall 3 facing the lower portion are enlarged to form portions of a concentric circle, one at the lower portion of the one side being about 30° by central angle and the other one from the upper portion to the lower portion of the other side being about 130° by central angle.
  • Both of the end portions of the enlarged portions smoothly lead to the cylinder-like inside wall 3 and the same kind of a suction chamber 4 and a combustion chamber 5 as the ones of the embodiment 1 are formed.
  • 6 is a rotor of the same kind as the one of the embodiment 1.
  • Three blade channels 7 of the same kind as the ones in the embodiment 1 are bored from trisecting points of the circumference of the rotor 6 toward the center of the rotor 6.
  • Blades 9 are of the same kind as the ones in the embodiment 1 and each of the blades 9 are inserted and engaged in each of the blade channels 7.
  • Explosion pressure intake holes 16 are bored from the surface of the rotor 6 at the back of each of the three blade channels 7 in the rotation direction a in parallel with each of the blade channels 7 adjacent to each of the blade channels 7 but not until the explosion intake holes 16 reach the center of the rotor 6.
  • Each of spaces for confining explosion pressure 17 which leads to each of the blade channels 7 are bored from the side in the center of the rotor 6.
  • Interconnecting holes 18 which connects each of the explosion pressure intake holes 16 with the space for confining explosion pressure 17 are bored from the periphery of the rotor 6, have nonreturn valves 19 built in them, and are embedded, etc. so as to be just in front of the explosion pressure intake holes 16 and are blocked. A part of the explosion pressure is taken in the space for confining explosion pressure 17 through the nonreturn valves 19 of the interconnecting holes 18 from the explosion intake holes 16, thereby blades 9 in each of the blade channels 7 are pushed strongly against the inside surface of the housing 1 and the airtightness between the tip of each of the blades 9 and the inside surface of the housing 1 is raised.
  • a round-bar-like divider portion 20 is attached to a portion of the housing 1 between the air suction hole 12 and the exhaust hole 14.
  • the divider portion 20 is provided to raise the airtightness between the suction chamber 4 and the combustion chamber 5 when, as in the present embodiment, the suction chamber 4 and the combustion chamber 5 are adjacent to each other, and the divider portion 20 can be attached so as to rotate together with the rotor 6.
  • the rotation of the rotor 6 is, as in the embodiment 1, caused by the difference in the explosion pressure acting on the blades 9 which are exposed to an explosion chamber 5a on the former end side of the combustion chamber 5 and are adjacent to each other.
  • the present embodiment is shown in Fig. 5, in which the explosion pressure in the space for confining explosion pressure 17 of the embodiment 2 is utilized only for maintaining the airtightness between the inside surface of the housing 1 and the blade 9 which separates the compression chamber 4b on the latter end side of the suction chamber and the explosion chamber 5a on the former end side of the combustion chamber 5.
  • the Bulkhead 21 as shown in Fig. 5, divides the inside of the space for confining explosion pressure 17 of Fig. 4.
  • the bulkhead 21 comprises three blades radially formed each of the blades connecting the side nearer to the rotor 6 of each of the interconnecting holes 18 in each of the spaces for confining 17 which interconnecting holes 18 connects the explosion pressure intake holes 16 with the spaces for confining 17 with the center of the rotor 6.
  • the bulkhead 21 makes each of the explosion pressure intake holes 16 connect with a base portion of each of the blade channels 7 adjacent to each of the explosion pressure intake holes 16 in the opposite direction to the rotation direction a of the rotor 6.
  • the bulkhead 21 utilizes explosion pressure only for pushing a blade 9 which is adjacent to the explosion chamber in the opposite direction to the rotation direction of the rotor 6 against the cylinder-like inside wall 3 of the housing 1.
  • the bulkhead 21 prevents explosion pressure from leaking in the suction chamber 4, and at the same time, makes the force pushing the tip of a blade 9 in the combustion chamber 5 and in the normal direction of the rotation of the rotor 6 against the inside wall of the housing 1 reduced, except when it is appropriate to push the blade 9 against the inside wall of the housing 1, and makes the friction decreased between the tip of the blade 9 and the inside wall of the housing 1 to rotate the rotor 6 with ease.
  • Holes 22 are provided on the bulkhead 21 and part of explosion pressure is utilized also to maintain the airtightness between the tip portion of a blade 9 in the combustion chamber 5 and the inside surface of the housing 1.
  • the holes numbered as 22 are bored in the three blades of the bulkhead 21, respectively. By boring said holes 22, explosion pressure which is continuously caused and which acts only on a blade 9 in the opposite direction to the rotation direction of the rotor due to the bulkhead 21 provided as in the embodiment 3 is controlled and utilized so as to act on each of the blades 9 equally, without intermission, and effectively.
  • the present embodiment is shown in Fig. 7.
  • Devices for adjusting the degree of aperture 23 are additionally provided at the holes 22 of the bulkhead 21 of the embodiment 4.
  • the degree of the airtightness between the tip of each of the blades 9 in the combustion chamber 5 and the inside surface of the housing 1 is adjusted by remote control of the devices for adjusting the degree of aperture 23.
  • the devices for adjusting the degree of aperture 23 utilize aperture diaphragms as in a camera, etc. and adjust the degree of aperture of the holes 22 according to the friction between the inside wall of the housing 1 and the tips of the blades 9, which friction depends on the nature, for example, viscosity, of the fuel. When great friction acts, the degree of aperture is made small and the rotation of the blades 9 in the suction chamber 4 and the combustion chamber 5 is made easy.
  • the present embodiment is shown in Figs. 8 and 9.
  • the same kind of a housing 1 and a rotor 6 as in the embodiment 1 is used and explosion pressure in the explosion chamber 5a on the former end side of the combustion chamber 5 is prevented from leaking in the compression chamber 4b on the latter end side of the suction chamber 4.
  • Cicular inside surface 24 is a part of the cylinder-like inside wall 3 and connects the compression chamber 4b on the latter end side in the rotation direction a of the rotor 6 of the suction chamber 4 with the explosion chamber 5a of the former end side in the rotation direction a of the rotor 6 of the combustion chamber 5.
  • a blade 9a is the one among the blades 9 which is in contact with the circular inside surface 24 separating the compression chamber 4b from the explosion chamber 5a.
  • Protrusions 25 are provided on the surface of the rotor 6 in front of and at the back of the cross-shaped blade channels 7 in the rotation direction of the rotor 6. The protrusions 25 are in contact with the circular inside surface 24 connecting the compression chamber 4b with the explosion chamber 5a.
  • channels 26 in parallel with each of the blade channels 2 are bored in the rotor 6 in front of and at the back of each of the blade channels 2 in the rotating direction a of the rotor 6.
  • Cylinder-like enlarged portions 26a are formed at the base portions of the channels 26.
  • Protruding boards 27 to be inserted and engaged in the channels 26 have cylinder-like enlarged portions 27a formed at the base portions of the protruding boards 27 to be inserted and engaged in the cylinder-like enlarged portions 26a.
  • the cylinder like enlarged portions 27a at the base portions are inserted and enoaged from the side in the cylinder like enlarged portions 26a of the channels 26 so that the tip portions of the protruding boards 27 are in contact with the circular inside surface 24 of the housing 1 connecting the compression chamber 4b with the explosion chamber 5a.
  • the present embodiment is shown in Fig. 10. Protrusions as the protruding portions 25 of the embodiment 6 are screwed to the surface of the rotor 6.
  • Attaching portions 28 are shaped and bored on the surface of the rotor 6 in front of and at the back of each of the blade channels 7 in the rotation direction a of the rotor 6 so as to be in parallel with the blade channels 7.
  • Washer based protruding portions 29 have washers 29a, respectively, which are fit in the attaching portions 28.
  • Protruding pieces 29b are formed which protrude from the washers 29a, respectively, in a reversed T shape, in an L shape, etc.
  • Each of the washers 29a is fixed by screwing to each of the portions of the rotor 6 at each of the attaching portions 28.
  • the tip portion of each of the protruding pieces 29b is in contact with the circular inside surface 24 connecting the compression chamber 4b with the explosion chamber 5a of the housing 1.
  • a reversed-T-shaped washer based protruding portion 29 and an L-shaped washer based protruding portion may be mixedly used as shown in Fig. 10, or, only one of them may be used.
  • the present embodiment is shown in Fig. 11.
  • the protruding portions 25 of the embodiment 6 are directly formed at the rotor 6.
  • Protrusions 31 are formed on the surface of the rotor 6 in front of and at the back of each of the blade channels 7 in the rotation direction a of the rotor 6 so as to be in parallel with each of the blade channels 7.
  • the tip portions of the protrusions 31 are in contact with the circular inside surface 24 which connects the compression chamber 4b with the explosion chamber 5a and are made to be protruding portions 25.
  • an output axis is not rotated by the engagement of an internal gear and an external gear like a conventional Wankel-type rotary engine but an output axis is directly connected with the rotor 6, explosion energy can be directly transformed into circular rotation movement of an output axis through the rotor 6, thereby energy loss in this part is small and, as a whole, the fuel consumption is smaller than in a conventional Wankel-type rotary engine.
  • the present invention has the abovementioned structure.
  • the maximum capacity of the combustion chamber enclosed with the inside wall of the housing of peritrochoidal curve and the rotor of peritrochoid internal envelope is not fixed to be equal to the maximum capacity of the suction chamber like a conventional Wankel-type rotary engine.
  • the ratio of the maximum capacity of the suction chamber and the maximum capacity of the combustion chamber can be freely set by adjusting the size of the portions where the radius of the cylinder-like inside wall is enlarged.
  • the combustion chamber 5 can be enlarged enough compared with the suction chamber 4 and explosion energy which was conventionally radiated from the exhaust hole 14 without being used can be effectively used in the circular rotation.
  • explosion energy can be directly transformed into rotation movement of the output axis (not shown) through the rotor 6, energy is not lost, heat efficiency is raised, and fuel consumption can be substantially improved.
  • the weak points of a conventional Wankel-type rotary engine wherein a rotor rotates in the housing while moving vertically, which is a quasi-reciprocating movement, can be thus resolved.
  • protruding portions 25 which are in contact with the circular inside surface 24 connecting the compression chamber 4b and the explosion chamber 5a of the housing 1 are provided on the surface of the rotor 6 in front of and at the back of each of the blade channels 7 which go through the center of the rotor 6 in the rotation direction a of the rotor 6, three points, that is, the blade 9a, a protruding portion 25 in front of the blade 9a, and a protruding portion 25 at the back of the blade 9a are in contact with the circular inside wall 24 connecting the compression chamber 4b with the explosion chamber 5a.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
EP90311339A 1989-10-18 1990-10-16 Moteur rotatif Withdrawn EP0424104A1 (fr)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
JP27248489 1989-10-18
JP272484/89 1989-10-18
JP42132/90 1990-02-22
JP4213290A JPH0730706B2 (ja) 1989-10-18 1990-02-22 ロータリーエンジン
JP5621090U JPH0717788Y2 (ja) 1990-05-28 1990-05-28 ロータリーエンジンの圧縮室への爆発圧漏洩防止装置
JP56210/90 1990-05-28

Publications (1)

Publication Number Publication Date
EP0424104A1 true EP0424104A1 (fr) 1991-04-24

Family

ID=27291075

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90311339A Withdrawn EP0424104A1 (fr) 1989-10-18 1990-10-16 Moteur rotatif

Country Status (5)

Country Link
EP (1) EP0424104A1 (fr)
KR (1) KR910008255A (fr)
AU (1) AU6360090A (fr)
CA (1) CA2027843A1 (fr)
CS (1) CS507590A3 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995035227A1 (fr) * 1994-06-22 1995-12-28 Foehl Artur Dispositif d'entrainement pour organe de retraction de ceinture de securite
ES2111422A1 (es) * 1994-02-02 1998-03-01 Garcia Fernandez Manuel Turbina en accion, de palas oscilantes.
FR2809453A1 (fr) * 2000-05-26 2001-11-30 Jean Claude Orgeval Moteur rotatif a palettes fonctionnant selon les memes cycles que les moteurs dits alternatifs
WO2004068001A1 (fr) * 2003-01-27 2004-08-12 Chuting Liu Mecanisme d'entrainement de liquide, a feuilles dommageables, exempt de force centrifuge

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB205904A (en) * 1922-07-28 1923-10-29 Harry Clarence Phillips Improvements in and relating to rotary prime movers, motors, compressors, pumps and the like
US2752893A (en) * 1953-06-10 1956-07-03 Oleskow Mathew Fluid motor
DE1914222A1 (de) * 1969-03-20 1970-10-01 Langen & Co Drehkolbenpumpe
DE2855567A1 (de) * 1978-12-22 1980-06-26 Duesterloh Gmbh Nachstelleinrichtung fuer eine sperrfluegel- oder zahnradmaschine
GB1573552A (en) * 1978-02-28 1980-08-28 Rae W L S Rotary internal combustion engine
GB2094890A (en) * 1981-03-18 1982-09-22 Collier Philip Harry Rotary positive-displacement fluid-machines

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB205904A (en) * 1922-07-28 1923-10-29 Harry Clarence Phillips Improvements in and relating to rotary prime movers, motors, compressors, pumps and the like
US2752893A (en) * 1953-06-10 1956-07-03 Oleskow Mathew Fluid motor
DE1914222A1 (de) * 1969-03-20 1970-10-01 Langen & Co Drehkolbenpumpe
GB1573552A (en) * 1978-02-28 1980-08-28 Rae W L S Rotary internal combustion engine
DE2855567A1 (de) * 1978-12-22 1980-06-26 Duesterloh Gmbh Nachstelleinrichtung fuer eine sperrfluegel- oder zahnradmaschine
GB2094890A (en) * 1981-03-18 1982-09-22 Collier Philip Harry Rotary positive-displacement fluid-machines

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2111422A1 (es) * 1994-02-02 1998-03-01 Garcia Fernandez Manuel Turbina en accion, de palas oscilantes.
WO1995035227A1 (fr) * 1994-06-22 1995-12-28 Foehl Artur Dispositif d'entrainement pour organe de retraction de ceinture de securite
US5653398A (en) * 1994-06-22 1997-08-05 Foehl; Artur Drive device for a belt pretensioner
FR2809453A1 (fr) * 2000-05-26 2001-11-30 Jean Claude Orgeval Moteur rotatif a palettes fonctionnant selon les memes cycles que les moteurs dits alternatifs
WO2004068001A1 (fr) * 2003-01-27 2004-08-12 Chuting Liu Mecanisme d'entrainement de liquide, a feuilles dommageables, exempt de force centrifuge

Also Published As

Publication number Publication date
KR910008255A (ko) 1991-05-30
CA2027843A1 (fr) 1991-04-19
AU6360090A (en) 1991-08-01
CS507590A3 (en) 1992-02-19

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