EP0240491A1 - Rotary engine. - Google Patents
Rotary engine.Info
- Publication number
- EP0240491A1 EP0240491A1 EP85905507A EP85905507A EP0240491A1 EP 0240491 A1 EP0240491 A1 EP 0240491A1 EP 85905507 A EP85905507 A EP 85905507A EP 85905507 A EP85905507 A EP 85905507A EP 0240491 A1 EP0240491 A1 EP 0240491A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- working
- expansion
- expansion space
- rotary motor
- motor
- 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.)
- Granted
Links
- 239000007789 gas Substances 0.000 claims abstract description 40
- 230000000295 complement effect Effects 0.000 claims abstract description 8
- 230000002093 peripheral effect Effects 0.000 claims description 35
- 238000007789 sealing Methods 0.000 claims description 19
- 238000013459 approach Methods 0.000 claims description 3
- 230000001154 acute effect Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 5
- 239000000567 combustion gas Substances 0.000 description 4
- 239000000446 fuel Substances 0.000 description 2
- 239000011796 hollow space material Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000036316 preload Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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
- F01C1/30—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
- F01C1/356—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 outer member
- F01C1/3566—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 outer member the inner and outer member being in contact along more than one line or surface
-
- 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
Definitions
- the invention relates to a rotary motor for converting the expansion pressure of working gases into a mechanical rotary movement.
- the expansion section in the form of a ring section corresponds to the cylinder space of a reciprocating piston engine.
- each expansion space can be sealed to the outside both in the circumferential direction and in the radial direction in order to prevent the working gases from escaping.
- This sealing takes place by means of one or more sealing rings with a corresponding preload, which can compensate for different temperature expansions of the material, or with a correspondingly small piston cross section, without any piston rings.
- EP-AS 0 080 070 A1 Zettner
- an internal combustion engine is described with a rotor with a circular cross-section and a ring-shaped stator (inner rotor) surrounding the rotor, which is designed in such a way that recesses in the form of expansion sections are present in the peripheral surface of the rotor as expansion spaces, at one end of which a combustion chamber is arranged and the other end ends in a ramp.
- Flaps are pivotally mounted on the inside of the stator, which flaps can be folded into the recesses of the rotor to absorb the forces of the expanding combustion gases and can be folded back into the stator by the ramp.
- the expansion space has a rectangular shape in an axial section in the longitudinal direction of the axis, with the result that rectangular edges which have to be sealed in the circumferential direction and in the radial direction occur on both the ramps and the flaps. The simultaneous sealing of these edges both in the circumferential direction and in the radial direction is permanently impossible.
- the invention is therefore based on the object of developing a sealing system for rotary motors which have an annular expansion space which, seen in the circumferential direction, is delimited by a fixed and a moving part, and whose wear behavior is at least comparable to the cylinder sealing system of reciprocating piston engines and that does not negatively affect the efficiency of rotary motors.
- the invention proceeds as prior art from a rotary engine for converting the expansion pressure of working gases into a mechanical rotary movement, with an engine inner part with a cylindrical outer circumferential surface, the engine inner part surrounding engine outer part with a cylinder-like inner peripheral surface, the outer peripheral surface and the inner peripheral surface lying opposite one another, bearings with which the motor inner part and the outer motor part are rotatably supported against one another, at least one working cam located on the one cylinder-like peripheral surface, which is sealed against the other cylinder-like peripheral surface and the expansion pressure Working gases to which one engine part transmits, at least one section-like recess in the same cylindrical peripheral surface following the working cam as an expansion space for the working gases, an inlet opening in each expansion space for the incoming working gases and at least one control device for at least one mounted on the other cylindrical peripheral surface, protruding into the expansion space, transferring the expansion pressure of the working gases to the other engine part and an outlet opening in each expansion space, which initially closes the working gases, the back pressure part being deflectable
- the invention consists in that the two circumferential surfaces have the shape of complementary ring surfaces, being seen in an axial section in the axial longitudinal direction through the ring surface, which has one ring surface in the form of a concave parabolic curve and the other ring surface in the form of a convex parabolic curve and both ring surfaces run with a close sliding fit parallel to each other up to their outer edges, which form two circular slots.
- the configuration of the circumferential surfaces as parabolic ring surfaces avoids all edges inside the motor to be sealed both in the circumferential direction and in the radial direction and the associated sealing problems in the motor described above. Exemplary embodiments of the invention are shown in the drawings. Show it :
- 1A is a partial section through a counter pressure part with scraper edge
- 1B is a partial section through a counter pressure part with a scraper edge on a seal
- FIG. 6 shows a central section perpendicular to the motor axis along the half center line VI-VI of FIG. 7 through a second embodiment of the rotary motor
- FIG. 1 shows a central section perpendicular to the motor axis along the half center line I - I of FIG. 2 by a rotary motor 1.
- the rotary motor 1 is a first embodiment of this motor type, which is described in more detail below.
- the rotary motor 1 consists of an inner motor part 101 with a cylindrical outer circumferential surface 102 and an outer motor part 123 surrounding the inner motor part 101 with a cylindrical inner circumferential surface 124, the outer circumferential surface 102 and the inner circumferential surface 124 being close to one another as can be seen in FIG.
- section-shaped recesses are provided as expansion spaces 107, 108, 109 for the working gases driving the rotary motor 1. Between two section-shaped recesses, for example between the recesses 107, 108, part of the cylindrical peripheral surface forms the working cam 104. In the example shown in FIG.
- the rotary motor 1 has three expansion spaces 107, 108, 109 and thus three working cams 104, 105, 106.
- the expansion space 107 is sealed off from the cylinder-like inner circumferential surface 124 in the circumferential direction by a seal 116. This makes it possible for the working cam 104 to transmit the expansion pressure of the working gases as torque to the engine inner part 101.
- the expansion spaces 108, 109 are sealed in the same way by seals 117, 118.
- An inlet opening 110 for the working gases driving the rotary motor 1 opens into the expansion space 107. The same applies to the other expansion rooms 108, 109.
- Compressed air, water vapor, organic vapors and also exhaust gases can be used as working gases, which are fed directly to the inlet openings 110, 111, 112.
- liquid or gaseous fuels can be placed in an external combustion chamber with an oxidizer, e.g. Atmospheric oxygen, burned and the combustion gases are introduced through the inlet openings into the expansion rooms.
- an oxidizer e.g. Atmospheric oxygen
- spark plugs can be arranged, for example, in the direction of rotation in the rear of the working cams 104, 105, 106.
- the counter-pressure part 126 also prevents the working gases from leaving the expansion space 107 from the outlet opening 113 until the relative rotation of the two motor parts 101, 123 caused by the expansion of the working gases against one another via a control causes the counter-pressure part 126 to evade the working cam 106 and the Release outlet 113. This can be done in such a way that the working cam 106 is pressed back into a recess 136 against the pressure of a spring 132, 133, 134, 135 by the ramp 120, 121, 122 or the like shown in FIG.
- Figure 1A gives the relative to each other
- 1B shows a second possibility, which consists in providing the scraper edge 141 on the seal 137 of the counterpressure part 126.
- FIG. 2 shows a first axial section in the longitudinal direction of the axis through the rotary motor 1 along the line II-II of FIG. 1. It can be seen from the section through the two circumferential surfaces 102, 124 that they have the shape of complementary ring surfaces, one ring surface 102 having the shape of a concave parabolic curve and the other ring surface 124 having the shape of a convex parabolic curve .
- the term "parabola-like curve” means the parabola, the parabola-like curve described in FIG. 2A and the hyperbola.
- the ring surfaces 102, 124 receives one by rotating one of these parabolic curves around the axis of rotation of the motor 1, the axis of symmetry of the parabolic curve being able to be at any angle on the axis of rotation.
- the two ring surfaces 102, 124 run with a close sliding fit parallel to each other up to their outer edges 103, 125, which form two circular slots 14-8, 14-9.
- the term "sliding fit”, which is generally known in the art, is to be understood to mean that the distance d between the edges 103, 125 corresponds at least to the largest of the following three values: twice the mean roughness depth of the annular surface material or the round and plane Impact of the annular surfaces 102, 124 or the differences in the thermal expansion coefficients of the annular surfaces 102, 124 that are effective during operation.
- the radial sealing of the slots 148, 149 from the outside is additionally carried out in each case by the labyrinth seals 150, 151, since they already curve the branches of the parabolic curve corresponding ring surface parts act as labyrinth seals.
- the labyrinth seals 150, 151 consist of a seal with a single deflection of the outflow path for the working gases by 180 °.
- the labyrinth seal can be seen in an axial section in the longitudinal direction of the axis, at any angle to the motor axis.
- the recess 119 in the motor outer part 123 serves to receive a suspension of the counter-pressure parts and / or to cool the motor.
- FIG. 2A shows the "parabola-like curve" 144 mentioned above.
- the parabola-like curve 144 consists of a circular arc 145, to which two straight lines 146, 147 adjoin. If the straight lines 146, 147 are extended beyond the circular arc 145, the straight lines 146, 147 enclose an angle ⁇ . The angle ⁇ is always less than 180 °.
- FIG. 3 shows a second axial section in the longitudinal direction of the axis through the rotary motor 1 along the line III-III of FIG. 1.
- This section shows how a seal 117 is arranged in the outer circumferential surface 102 of the inner motor part 101, which, viewed in the circumferential direction, seals the outer circumferential surface 102 against the inner circumferential surface 124 of the outer motor part 123.
- the expansion space 107 in the region of the working cam 104 is thereby sealed.
- a special property of the seal 117 which can be readily understood from FIG. 3, is to be practically wear-free after the initial running-in process, since the motor outer part 123 and the motor inner part 101 can rotate relative to one another with any desired accuracy without play due to the bearings 141, 142.
- FIG. 4 shows a third axial section in the longitudinal axis direction through the rotary motor 1 along the line IV-IV from FIG. 1.
- Figure 4 is thus a section through the expansion space 108 for the working gases.
- the expansion space 108 also has the concave shape of a parabola, a parabola-like curve described in FIG. 2A or a hyperbola.
- the wall of the expansion space 108 merges continuously into the outer peripheral surface 102.
- At one end of the expansion space 108 is the inlet opening 111 for those flowing into the expansion space 108 Working gases and at the other end the outlet opening 114 for the expanded working gases.
- FIG. 5 shows an axial section in the longitudinal axis direction along the line V - V of FIG. 1.
- Section shows the counter pressure part 126 in the expansion space 107.
- the counter pressure part 126 has a shape complementary to the wall of the expansion space 107 and is sealed against the wall of the expansion space 107 by a seal 137. It can also be seen here that there are no edges to be sealed in the circumferential direction between the counterpressure part 126 and the expansion space 107.
- the arrangement of the seals 116, 117, 118 in the annular surface 102 and the seal 137 in the counter pressure part 126, the seal 138 in the counter pressure part 127, etc. shows that the ring surface 102 and the complementary ring surface portion of the counter pressure parts 126, 127, 128, 129 can have on average only the shape of the parabolic curve described above.
- the spring 132 is part of the control device.
- the head 131 of the counter pressure part 132 rests with four approximately conical surfaces on the surfaces of a recess 136 in the motor outer part 123
- the inner motor part 101 can be the stator and the outer motor part 123 can be the rotor. However, it is also possible vice versa, namely that the inner motor part 101 is the rotor and the outer motor part 123 is the stator.
- FIG. 6 shows a section perpendicular to the central axis along the half center line VI-VI of FIG. 7 through a rotary motor 2.
- the rotary motor 2 consists of a motor inner part 201 with an outer circumferential surface 202 and a motor outer part 204 which is ideal for surrounding the motor inner part 201 with an inner circumferential surface 206, the outer circumferential surface 202 and the inner circumferential surface 206 as can be seen from FIG opposite.
- Part of the inner peripheral surface 206 has been left as working cams 207, 208, 209 between two section-shaped expansion spaces.
- the working cam 207 is sealed off from the annular outer circumferential surface 202 by a seal 213. This makes it possible for the working cam 207 to transmit the expansion pressure of the working gases as torque to the motor outer part 205.
- An inlet opening 211 for the working gases opens into the expansion space 210.
- a counterpressure part 203 which projects into the expansion space 210 and transmits the expansion pressure of the working gases to the motor inner part 201, is mounted on the ring-shaped outer circumferential surface 202 of the motor inner part 201.
- the counter pressure part 203 is sealed off from the inner circumferential surface 206 by a parabolic seal 213.
- the counter-pressure part 203 covers an outlet opening 212 for the expanding working gases until the relative rotation of the two motor parts 201, 205 caused by the expansion relative to one another via a control, for example a ramp 219, causes the counter-pressure part 203 to evade the working cam 207.
- Each counter pressure part 203 is pressed by the pressure of a spring 204 against the inner surface 206, or the wall of the expansion space 210, the seal in
- the seal 214 has the same shape as the seal 137.
- FIG. 7 shows a first axial section in the longitudinal direction of the axis through the rotary motor 2 along the line VII-VII of FIG. 6. From this section, it can be seen that the outer peripheral surface 202 and the inner peripheral surface 206 have the shape of complementary ring surfaces, the outer peripheral surface 202 having the convex shape and the inner peripheral surface 206 having the concave shape of the parabolic curves described above.
- the convex and concave ring surfaces 202, 206 corresponding to the curves run, as has also been described above, with a sliding fit up to their outer edges, which appear as two circular slots 215, 216.
- FIG. 8 shows a second axial section in the longitudinal direction of the axis through the rotary motor 2 along the line VIII-VIII of FIG. 6. This figure shows a section through a section-shaped expansion space 210 and corresponds to FIG. 4.
- FIG. 9 shows a third axial section in the longitudinal direction of the axis through the rotary motor 2 along the line IX-IX of FIG. 6. From this section it can be seen that the counter-pressure part 202 moves into the expansion space 210 and is held there by the spring 204. The counter pressure part 202 is sealed in the circumferential direction against the wall of the expansion space 210 by the seal 214, which is visible in cross section in FIG. 6. This seal 214 corresponds to the seal 137 from FIG. 5 and is described there in detail. The deflection of the counterpressure part 203 when the inner motor part 201 rotates relative to the outer motor part 205 when the working cam 207 approaches is effected by a ramp 219.
- Shape and the inner peripheral surface 124 has the convex shape, while in the rotary motor 2, the outer peripheral surface 202 has the convex shape and the inner peripheral surface 206 has the concave shape.
- FIG. 10 shows the Schroeder motor 30 with the expansion space 31, the working cam 32 and the counter pressure part 33.
- FIG. 11 shows the Walter motor 40 with the expansion space 41, the working cam 42, the counter pressure part 43 and the valve-controlled outlet opening 44 for the working gases.
- FIG. 12 shows the Brown motor 50 with the expansion space 51, the working cam 52 and the counter pressure part 53.
- FIG. 13 shows the Thomas motor 60 with the expansion space 61, the working cam 62 and the counter pressure part 63.
- FIG. 14 A shows the first embodiment of the Wenzel motor 70 with the expansion space 71, the working cam 72 and the counter pressure part 73.
- This first embodiment corresponds to the motor principle shown in FIGS. 1 to 5.
- FIG. 14B shows the second embodiment of the Wenzel motor 80, in which the counterpressure part 83 is fastened to the inner part, the working cam to the outer part and which corresponds to the motor principle shown in FIGS. 6 to 9.
- the rotary motor 80 has the expansion space that can only be specified in cross section 81, the working cam 82 and the like Back pressure part 83.
- the working gases enter the expansion space through the slot 84 from the engine inner part.
- the expansion space can therefore only be specified in a cross-sectional line 81, since it is located in the motor outer part cut away in FIG. 14B.
- the labyrinth seal 85 is fixedly attached to the motor outer part 86 in this case.
- FIG. 15 shows the Zettner motor 90 with the expansion space 91, the working cam 92, the counterpressure part 93 and the inlet opening 94 for the working gases into the expansion space 91.
- the rotary motor 90 works, for example, as an external rotor.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
- Valve Device For Special Equipments (AREA)
- Hydraulic Motors (AREA)
- Supercharger (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Power Steering Mechanism (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
- Permanent Magnet Type Synchronous Machine (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
- Sealing Devices (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
Abstract
Un moteur à cylindres rotatifs (1) utilisé pour convertir la force d'expansion de gaz de travail en un mouvement mécanique de rotation comprend une partie intérieure de moteur (101) ayant une circonférence extérieure cylindrique (102) et une partie extérieure de moteur (123) qui entoure la partie intérieure de moteur (101) et a une circconférence intérieure cylindrique (124). Les deux circonférences (102, 124) sont agencées l'une en face de l'autre. Sur une des circonférences cylindriques (102) est agencé au moins un ergot de travail (104, 105, 106) qui transfère la force d'expansion des gaz de travail à la partie de moteur (101) et au moins une chambre d'expansion (107, 108, 109). Sur l'autre circonférence cylindrique (124) est montée une pièce de contre-pression (126, 127, 128, 129) qui fait saillie dans la chambre d'expansion (107, 108, 109) et qui transfère la force d'expansion des gaz de travail à l'autre partie de moteur (123). Les deux circonférences (102, 104) ont la forme de surfaces annulaires complémentaires. Une coupe axiale dans le sens de l'axe longitudinal des surfaces annnnulaires (102, 104) révèle qu'une des surfaces annulaires (102) a la forme d'une courbe parabolique concave et que l'autre surface annulaire (124) a la forme d'une courbe parabolique convexe. Les deux surfaces annulaires (102, 124) sont étroitement ajustées l'une à l'autre de manière à glisser l'une sur l'autre et s'étendent parallèlement l'une à l'autre jusqu'à leurs bords extérieurs.A rotary cylinder engine (1) used to convert the expanding force of working gas into a mechanical rotational movement includes an inner engine portion (101) having a cylindrical outer circumference (102) and an outer engine portion ( 123) which surrounds the inner engine part (101) and has a cylindrical inner circumference (124). The two circumferences (102, 124) are arranged one opposite the other. On one of the cylindrical circumferences (102) is arranged at least one working lug (104, 105, 106) which transfers the expansion force of the working gases to the engine part (101) and at least one expansion chamber (107, 108, 109). On the other cylindrical circumference (124) is mounted a backpressure piece (126, 127, 128, 129) which projects into the expansion chamber (107, 108, 109) and which transfers the expansion force working gases to the other engine part (123). The two circumferences (102, 104) have the form of complementary annular surfaces. An axial section along the longitudinal axis of the annular surfaces (102, 104) reveals that one of the annular surfaces (102) has the shape of a concave parabolic curve and that the other annular surface (124) has the shape of a convex parabolic curve. The two annular surfaces (102, 124) are tightly adjusted to each other so as to slide over one another and extend parallel to each other as far as their outer edges.
Description
Claims
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/EP1985/000513 WO1987002096A1 (en) | 1985-10-02 | 1985-10-02 | Rotary engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0240491A1 true EP0240491A1 (en) | 1987-10-14 |
EP0240491B1 EP0240491B1 (en) | 1990-03-07 |
Family
ID=8165063
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP85905507A Expired - Lifetime EP0240491B1 (en) | 1985-10-02 | 1985-10-02 | Rotary engine |
Country Status (11)
Country | Link |
---|---|
US (1) | US4890990A (en) |
EP (1) | EP0240491B1 (en) |
JP (1) | JPS62502205A (en) |
AT (1) | ATE50822T1 (en) |
AU (1) | AU577422B2 (en) |
BR (1) | BR8507295A (en) |
DE (1) | DE3576381D1 (en) |
IL (1) | IL80159A (en) |
RU (1) | RU1789036C (en) |
WO (1) | WO1987002096A1 (en) |
ZA (1) | ZA867452B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7015348B2 (en) | 2002-07-30 | 2006-03-21 | Takasago International Corporation | Method for producing an optically active β-amino acid |
EP2581552A4 (en) * | 2010-06-10 | 2017-03-08 | Beijing Rostar Technology Co. Ltd | Spiraster-type fluid motor or engine and compressor or pump |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
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GB2254888B (en) * | 1991-03-05 | 1995-04-05 | Ian Alexander Giles | Rotary positive-displacement pump and engine |
DE29513194U1 (en) * | 1995-08-17 | 1995-11-23 | Heidenescher, Ferdinand, 49143 Bissendorf | Rotary piston internal combustion engine |
BE1010391A3 (en) * | 1996-06-27 | 1998-07-07 | Orphanidis Michalis | Rotary piston volumetric effect machine and engine derived from such a machine |
US7793635B2 (en) * | 2006-05-09 | 2010-09-14 | Okamura Yugen Kaisha | Rotary piston type internal combustion engine |
JP5147134B2 (en) * | 2006-05-09 | 2013-02-20 | オカムラ有限会社 | Rotary fluid machine |
IL216439A (en) | 2011-11-17 | 2014-02-27 | Zettner Michael | Rotary engine and process |
ITBL20120010A1 (en) | 2012-11-30 | 2014-05-31 | Ruggero Libralato | ROTARY ENDOTHERMAL ENGINE WITH DOUBLE ROTATION CENTER, PERFECTED WITH WALL-RETAINING WALLS AND DIFFERENTIAL EXHAUSTS |
US9291095B2 (en) * | 2013-03-15 | 2016-03-22 | Randy Koch | Rotary internal combustion engine |
US9464566B2 (en) | 2013-07-24 | 2016-10-11 | Ned M Ahdoot | Plural blade rotary engine |
CN110005606A (en) * | 2019-03-28 | 2019-07-12 | 云大信 | A kind of card slot pump installation and flow rate adjusting method |
WO2024142064A1 (en) | 2022-12-29 | 2024-07-04 | Coool.Energy Ltd | Rotary compressor and expander |
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US1442198A (en) * | 1914-06-24 | 1923-01-16 | Arthur Kitson | Rotary pump, engine, or meter |
GB113697A (en) * | 1917-03-27 | 1918-03-07 | Nikolai Demianovitch Shelikof | An Improved Rotary Engine. |
US1625233A (en) * | 1922-08-23 | 1927-04-19 | Cheever J Cameron | Rotary engine |
US1770141A (en) * | 1927-05-31 | 1930-07-08 | Albert J Meyer | Pump |
US1859618A (en) * | 1929-09-18 | 1932-05-24 | Ward W Cleland | Rotary internal combustion engine |
US2796030A (en) * | 1953-05-29 | 1957-06-18 | Nebel Franz Philip | Rotary pump for handling viscous materials |
US3249096A (en) * | 1962-10-12 | 1966-05-03 | Franceschini Enrico | Rotating internal combustion engine |
US3181512A (en) * | 1963-04-22 | 1965-05-04 | Fred J Hapeman | Rotary internal combustion engine |
GB1349521A (en) * | 1970-01-01 | 1974-04-03 | Oppenheim H | Rotary-piston machines |
JPS4711874A (en) * | 1970-11-05 | 1972-06-14 | ||
AR212382A1 (en) * | 1977-11-16 | 1978-06-30 | Quiroga P | ROTARY ENGINE WITH SIDE ACTING PISTONS |
US4561834A (en) * | 1983-07-13 | 1985-12-31 | Poss Design Limited | Rotary vaned pumps with fixed length and shearing knife-edged vanes |
-
1985
- 1985-10-02 WO PCT/EP1985/000513 patent/WO1987002096A1/en active IP Right Grant
- 1985-10-02 DE DE8585905507T patent/DE3576381D1/en not_active Expired - Lifetime
- 1985-10-02 JP JP60504873A patent/JPS62502205A/en active Granted
- 1985-10-02 AT AT85905507T patent/ATE50822T1/en not_active IP Right Cessation
- 1985-10-02 AU AU50131/85A patent/AU577422B2/en not_active Ceased
- 1985-10-02 EP EP85905507A patent/EP0240491B1/en not_active Expired - Lifetime
- 1985-10-02 BR BR8507295A patent/BR8507295A/en not_active IP Right Cessation
-
1986
- 1986-09-26 IL IL80159A patent/IL80159A/en active IP Right Revival
- 1986-09-30 ZA ZA867452A patent/ZA867452B/en unknown
-
1987
- 1987-05-27 RU SU874202624A patent/RU1789036C/en active
-
1988
- 1988-04-14 US US07/181,356 patent/US4890990A/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
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See references of WO8702096A1 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7015348B2 (en) | 2002-07-30 | 2006-03-21 | Takasago International Corporation | Method for producing an optically active β-amino acid |
US7893296B2 (en) | 2002-07-30 | 2011-02-22 | Takasago International Corporation | Method for producing an optically active β-amino acid |
EP2581552A4 (en) * | 2010-06-10 | 2017-03-08 | Beijing Rostar Technology Co. Ltd | Spiraster-type fluid motor or engine and compressor or pump |
Also Published As
Publication number | Publication date |
---|---|
ZA867452B (en) | 1987-05-27 |
IL80159A0 (en) | 1986-12-31 |
JPH0229841B2 (en) | 1990-07-03 |
AU5013185A (en) | 1987-04-24 |
ATE50822T1 (en) | 1990-03-15 |
EP0240491B1 (en) | 1990-03-07 |
JPS62502205A (en) | 1987-08-27 |
US4890990A (en) | 1990-01-02 |
IL80159A (en) | 1992-07-15 |
BR8507295A (en) | 1987-11-03 |
AU577422B2 (en) | 1988-09-22 |
RU1789036C (en) | 1993-01-15 |
WO1987002096A1 (en) | 1987-04-09 |
DE3576381D1 (en) | 1990-04-12 |
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