US3185386A - Packing devices comprising fixed and movable elements for rotary engines - Google Patents

Packing devices comprising fixed and movable elements for rotary engines Download PDF

Info

Publication number
US3185386A
US3185386A US133632A US13363261A US3185386A US 3185386 A US3185386 A US 3185386A US 133632 A US133632 A US 133632A US 13363261 A US13363261 A US 13363261A US 3185386 A US3185386 A US 3185386A
Authority
US
United States
Prior art keywords
rotor
sealing strips
lobes
epicyclic
stator
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.)
Expired - Lifetime
Application number
US133632A
Inventor
Peras Lucien
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.)
Renault SAS
Regie Nationale des Usines Renault
Original Assignee
Renault SAS
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 Renault SAS filed Critical Renault SAS
Application granted granted Critical
Publication of US3185386A publication Critical patent/US3185386A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • 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
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F01C19/10—Sealings for working fluids between radially and axially movable parts

Definitions

  • This invention relates to .packing devices for rotary engines of the lobar type comprising an eccentric rotor having 2N lobes and a stator having 2N +1 lobes, wherein the rotor contour is an epicycloid and the stator contour an envelope curve having its contour conjugated with the rotor epicycloid.
  • the number of contact points between the two contours equals the number of lobes of the envelope curve and it is this number (2N+l) that determines the number of working chambers in which the cycle of operation of the engine takes place.
  • 2N+1 working chambers Associated with these 2N+1 working chambers are 2N +1 combustion chambers in which the inlet and exhaust valves as well as the spark plug are mounted.
  • This invention relates more particularly but not exclusively to engines of the type defined hereinabove, wherein the combustion chambers are disposed peripherally in relation to each working chamber; therefore, these combustion chambers are formed in the stator.
  • the present invention provides packing means for sealing the joints against gas and oil leakages, in the form of fixed partitioning means disposed in the stator and of rotary partitioning means disposed in the rotor.
  • These fixed partitioning means consist of elements described in the patent application Serial No. 133,631 filed on the same date by the same applicant and entitled Packing for rotary engines, that is, strips or sections fitted in grooves or like recesses formed in the stator at the junctions of adjacent lobes, these strips or sections resiliently engaging the epicyclic contour of the rotor along one generatrix, the movable partitioning means of the present invention consisting on the one hand of lateral strips following a substantially epicyclic path, which are fitted in recesses or grooves formed in the lateral faces of the rotor so as to fit closely the epicyclic contour of the rotor, and on the other hand of circular strips disposed within said epicyclic strips and adapted to seal the engine more particularly against oil leakages through the bearing.
  • FIGURE 1 is a complete view showing the rotor and stator assembly, the upper or front flange or cover being removed to show the fixed and movable partitioning means constituting the subject-matter of this invention;
  • FIGURE 2 is a detail section showing the fixed radial partitioning means mounted in the stator and complementary strips constantly bearing on the epicyclic strip or forming a narrow gap with this section;
  • FIGURES 2a and 2b are sections taken along the lines a-a and bb of FIGURE 2 respectively;
  • FIGURE 3 is a modified embodiment of the structure shown in FIG. 2;
  • FIGURES 3a and 3b are sections taken across the lines a-a and bb of FIG. 3 respectively;
  • FIGURES 4 and 4a are diiferent embodiments of the epicyclic strip.
  • FIGURE 5 is a detail section showing an alternate embodiment of the lateral sealing member.
  • the rotary engine comprises the rotor 1 disposed in the stator 2 in which working chambers 3 as well as combustion chambers 4 are formed; these chambers receive the inlet and exhaust valves 5, 6 as well as the spark plugs 7.
  • the fixed radial strips 8 mounted on the stator and bearing on the rotor in order to seal the Working chambers from one another are complemented by an epicyclic movable strip 9 and a circular movable strip 10 both mounted on the rotor.
  • FIGURES 2, 2a and 2b illustrate in section fixed strips according to a diametral plane of the engine, according to a specific embodiment of the invention, each fixed strip 8 is fitted in a groove 12 formed in the stator, a corrugated spring blade 11 being fitted in the bottom of this groove for resiliently pressing the strip against the peripheral contour of the rotor.
  • a complementary strip 15 housed in a blind hole 14 formed in the flange or cover 13 of the stator 2 is resiliently urged by a spring 18 against the same relevant end of strip 8.
  • each strip 15 bears at the same time against the epicyclic strip 9 and these two members are adapted to slide on each other; to this end, each strip 15 may be formed at its outer portion with a rounded contour 19 or any other suitable contour and the strip 8 may also have a rounded contour 20 if desired.
  • the member 15 fits in a slot 16 formed in a member 17 force fitted in the recess 14.
  • the complementary strip 15' is disposed directly in a recess 21, a corrugated spring blade 22 causing the elastic relative engagement between the components.
  • the epicyclic strip 9 may advantageously consist of a set of resilient leaf springs 23 of moderate thickness which are urged against the flange or cover 13 by a corrugated spring blade 24 (FIG. 4).
  • corrugated spring blade 25 may be added centrally of these leaf springs, this blade corresponding substantially in shape to these springs 23 and serving the purpose of producing the sealing contact with the lateral faces of the epicyclic groove (FIG. 4a).
  • FIGURE 5 illustrates in section an alternate embodiment of the lateral sealing device wherein the bearing member 15 is replaced by a circular piston 26 guided in a recess 27 formed in the flange or cover 13. This piston is disposed astride so as to bear both on the strip 8 and on the epicyclic strip 9, and is subjected to the resilient force of a helical spring 28.
  • Packing device for a rotary engine of the lobar type comprising an eccentric rotor of substantially epicyclic contour having 2N lobes and a stator providing a chamber therein having 2nr+1 lobes and having end covers for said chamber, wherein combustion chambers are disposed around the outer periphery of the rotor in said stator, the rotor being mounted for rolling intermeshing relation of the lobes thereof with the stator lobes,
  • said packing device comprising fixed radial sealing strips disposed in the stator along the line of junction between adjacent working chambers, movable sealing strips carried by said rotor and consisting on the one hand of lateral sealing strips of substantially epicyclic contour located at a relatively short distance from the epicyclic surface of said rotor, and on the other hand of circular sealing strips disposed inside said epicyclic 10 sealing strips also on the lateral faces of the rotor, and complementary sealing strips in each stator cover end- Wise of said radial sealing strips, resiliently engaging both said radial sealing strips and the epicyclic sealing strips in order to provide the necessary lateral fluid-tightness.
  • Packing device according to claim 2, characterized in that said epicyclic strips consist of stackings of leafsprings.

Description

May 25, 1965 L. PERAS 3,185,386
PACKING DEVICE-S COMPRISING FIXED AND MOVABLE ELEMENTS FOR ROTARY ENGINES 2 Sheets-Sheet 1 Filed Aug. 24, 1961 Invent-n- PERAS 3,185,386 ICES COMPRISING FIXED AND MOVABLE ELEMENTS FOR ROTARY ENGINES May 25, 1965 PACKING DEV 2 Sheets-Sheet 2 Filed Aug. 24, 1961 United States Patent 3,185,386 PACKING DEVICES COMPRISING FIXED AND MOVABLE ELEMENTS FOR ROTARY ENGINES Lucien Paras, Billancourt, France, assignor to Regie Nationale des Usines Renault, Billancourt, France Filed Aug. 24, 1961, Ser. No. 133,632 Claims priority, application France, Sept. 20, 1960, 839,013, Patent 1,277,311 3 Claims. (Cl. 230-145) This invention relates to .packing devices for rotary engines of the lobar type comprising an eccentric rotor having 2N lobes and a stator having 2N +1 lobes, wherein the rotor contour is an epicycloid and the stator contour an envelope curve having its contour conjugated with the rotor epicycloid.
The number of contact points between the two contours equals the number of lobes of the envelope curve and it is this number (2N+l) that determines the number of working chambers in which the cycle of operation of the engine takes place. Associated with these 2N+1 working chambers are 2N +1 combustion chambers in which the inlet and exhaust valves as well as the spark plug are mounted.
This invention relates more particularly but not exclusively to engines of the type defined hereinabove, wherein the combustion chambers are disposed peripherally in relation to each working chamber; therefore, these combustion chambers are formed in the stator.
In an engine of this type the present invention provides packing means for sealing the joints against gas and oil leakages, in the form of fixed partitioning means disposed in the stator and of rotary partitioning means disposed in the rotor.
These fixed partitioning means consist of elements described in the patent application Serial No. 133,631 filed on the same date by the same applicant and entitled Packing for rotary engines, that is, strips or sections fitted in grooves or like recesses formed in the stator at the junctions of adjacent lobes, these strips or sections resiliently engaging the epicyclic contour of the rotor along one generatrix, the movable partitioning means of the present invention consisting on the one hand of lateral strips following a substantially epicyclic path, which are fitted in recesses or grooves formed in the lateral faces of the rotor so as to fit closely the epicyclic contour of the rotor, and on the other hand of circular strips disposed within said epicyclic strips and adapted to seal the engine more particularly against oil leakages through the bearing.
With the foregoing and other objects in view, the invention resides in the novel arrangement and combination of par-ts and in the details of construction hereafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed may be made within the scope of what is claimed without departing from the spirit of the invention.
Other objects and advantages will become apparent from the following description taken in conjunction with the accompanying drawing in which:
FIGURE 1 is a complete view showing the rotor and stator assembly, the upper or front flange or cover being removed to show the fixed and movable partitioning means constituting the subject-matter of this invention;
FIGURE 2 is a detail section showing the fixed radial partitioning means mounted in the stator and complementary strips constantly bearing on the epicyclic strip or forming a narrow gap with this section;
FIGURES 2a and 2b are sections taken along the lines a-a and bb of FIGURE 2 respectively;
ice
FIGURE 3 is a modified embodiment of the structure shown in FIG. 2;
FIGURES 3a and 3b are sections taken across the lines a-a and bb of FIG. 3 respectively;
FIGURES 4 and 4a are diiferent embodiments of the epicyclic strip, and
FIGURE 5 is a detail section showing an alternate embodiment of the lateral sealing member.
In the form of embodiment illustrated in FIG. 1, the rotary engine comprises the rotor 1 disposed in the stator 2 in which working chambers 3 as well as combustion chambers 4 are formed; these chambers receive the inlet and exhaust valves 5, 6 as well as the spark plugs 7.
To seal this engine against gas and oil leakages the fixed radial strips 8 mounted on the stator and bearing on the rotor in order to seal the Working chambers from one another are complemented by an epicyclic movable strip 9 and a circular movable strip 10 both mounted on the rotor.
FIGURES 2, 2a and 2b illustrate in section fixed strips according to a diametral plane of the engine, according to a specific embodiment of the invention, each fixed strip 8 is fitted in a groove 12 formed in the stator, a corrugated spring blade 11 being fitted in the bottom of this groove for resiliently pressing the strip against the peripheral contour of the rotor. To seal the ends of this strip a complementary strip 15 housed in a blind hole 14 formed in the flange or cover 13 of the stator 2 is resiliently urged by a spring 18 against the same relevant end of strip 8.
The end strip 15 bears at the same time against the epicyclic strip 9 and these two members are adapted to slide on each other; to this end, each strip 15 may be formed at its outer portion with a rounded contour 19 or any other suitable contour and the strip 8 may also have a rounded contour 20 if desired.
More particularly, the member 15 fits in a slot 16 formed in a member 17 force fitted in the recess 14. In an alternate embodiment illustrated in FIGURES 3, 3a and 3b, the complementary strip 15' is disposed directly in a recess 21, a corrugated spring blade 22 causing the elastic relative engagement between the components.
Finally, the epicyclic strip 9 may advantageously consist of a set of resilient leaf springs 23 of moderate thickness which are urged against the flange or cover 13 by a corrugated spring blade 24 (FIG. 4).
If desired, another corrugated spring blade 25 may be added centrally of these leaf springs, this blade corresponding substantially in shape to these springs 23 and serving the purpose of producing the sealing contact with the lateral faces of the epicyclic groove (FIG. 4a).
FIGURE 5 illustrates in section an alternate embodiment of the lateral sealing device wherein the bearing member 15 is replaced by a circular piston 26 guided in a recess 27 formed in the flange or cover 13. This piston is disposed astride so as to bear both on the strip 8 and on the epicyclic strip 9, and is subjected to the resilient force of a helical spring 28.
Of course, other modifications and alterations could be brought to the packing means described and illustrated herein, without departing from the spirit and scope of the invention.
I claim:
1. Packing device for a rotary engine of the lobar type comprising an eccentric rotor of substantially epicyclic contour having 2N lobes and a stator providing a chamber therein having 2nr+1 lobes and having end covers for said chamber, wherein combustion chambers are disposed around the outer periphery of the rotor in said stator, the rotor being mounted for rolling intermeshing relation of the lobes thereof with the stator lobes,
said rotor lobes and stator lobes thereby forming expansible and contractible fluid working chambers therebetween, said packing device comprising fixed radial sealing strips disposed in the stator along the line of junction between adjacent working chambers, movable sealing strips carried by said rotor and consisting on the one hand of lateral sealing strips of substantially epicyclic contour located at a relatively short distance from the epicyclic surface of said rotor, and on the other hand of circular sealing strips disposed inside said epicyclic 10 sealing strips also on the lateral faces of the rotor, and complementary sealing strips in each stator cover end- Wise of said radial sealing strips, resiliently engaging both said radial sealing strips and the epicyclic sealing strips in order to provide the necessary lateral fluid-tightness.
2. Packing device according to claim 1, characterized in that said sealing strips consist of strips urged by spring means to their sealing position.
4 3. Packing device according to claim 2, characterized in that said epicyclic strips consist of stackings of leafsprings.
References Cited by the Examiner UNITED STATES PATENTS 748,348 12/03 Cooley. 1,310,157 7/19 De Campo 9156 3,033,180 5/62 Bentele l238 FOREIGN PATENTS 1,057,613 5/59 Germany.
24,559 1908 Great Britain.
15 KARL J. ALBRECHT, Primary Examiner.
WILLIAM FELDMAN, JOSEPH H. BRANSON, JR.,
Examiners.

Claims (1)

1. PACKING DEVICE FOR A ROTARY ENGINE OF THE LOBAR TYPE COMPRISING AN ECCENTRIC ROTOR OF SUBSTANTIALLY EPICYCLIC CONTOUR HAVING 2N LOBES AND A STATOR PROVIDING A CHAMBER THEREIN HAVING 2N+1 LOBES AND HAVING END COVERS FOR SAID CHAMBER, WHEREIN COMBUSTION CHAMBERS ARE DISPOSED AROUND THE OUTER PERIPHERY OF THE ROTOR IN SAID STATOR, THE ROTOR BEING MOUNTED FOR ROLLING INTERMESHING RELATION OF THE LOBES THEREOF WITH THE STATOR LOBES, SAID ROTOR LOBES AND STATOR LOBES THEREBY FORMING EXPANSIBLE AND CONTRACTIBLE FLUID WORKING CHAMBERS THEREBETWEEN, SAID PACKING DEVICE COMPRISING FIXED RADIAL SEALING STRIPS DISPOSED IN THE STATOR ALONG THE LINE OF JUNCTION BETWEEN ADJACENT WORKING CHAMBERS, MOVABLE SEALING STRIPS CARRIED BY SAID ROTOR AND CONSISTING ON THE ONE HAND OF LATERAL SEALING STRIPS OF SUBSTANTIALLY EPICYCLIC CONTOUR LOCATED AT A RELATIVELY SHORT DISTANCE FROM THE EPICYCLIC SURFACE OF SAID ROTOR, AND ON THE OTHER HAND OF CIRCULAR SEALING STIPS DIPOSED INSIDE SAID EPICYCLIC SEALING STRIPS ALSO ON THE LATERAL FACES OF THE ROTOR, AND COMPLEMENTARY SEALING STRIPS, RESILIENTLY ENGAGING BOTH WISE OF SAID RADIAL SEALING STRIPS, RESILIENTLY ENGAGING BOTH SAID RADIAL SEALING STRIPS AND THE EPICYCLIC SEALING STRIPS IN ORDER TO PROVIDE THE NECESSARY LATERAL FLUID-TIGHTNESS.
US133632A 1960-09-20 1961-08-24 Packing devices comprising fixed and movable elements for rotary engines Expired - Lifetime US3185386A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR839013A FR1277311A (en) 1960-09-20 1960-09-20 Sealing system with fixed and movable elements for rotary engine

Publications (1)

Publication Number Publication Date
US3185386A true US3185386A (en) 1965-05-25

Family

ID=8739310

Family Applications (1)

Application Number Title Priority Date Filing Date
US133632A Expired - Lifetime US3185386A (en) 1960-09-20 1961-08-24 Packing devices comprising fixed and movable elements for rotary engines

Country Status (6)

Country Link
US (1) US3185386A (en)
DE (1) DE1426047A1 (en)
ES (1) ES270531A1 (en)
FR (1) FR1277311A (en)
GB (1) GB995248A (en)
OA (1) OA01636A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282496A (en) * 1962-11-08 1966-11-01 Radziwill Maciej Sealing means for a power driven machine with a rotary piston
US3366317A (en) * 1966-04-30 1968-01-30 Kloeckner Humboldt Deutz Ag Rotary piston internal combustion engine, especially circular piston internal combustion engine
US3369739A (en) * 1966-04-30 1968-02-20 Kloeckner Humboldt Deutz Ag Rotary piston internal combustion engine, especially circular piston internal combustion engine
US3827838A (en) * 1973-01-05 1974-08-06 Ramsey Corp Oil seal for rotary piston engines
US3869229A (en) * 1973-03-26 1975-03-04 Toyo Kogyo Co Sealing device for use in rotary piston engine
US3910733A (en) * 1969-09-18 1975-10-07 Leslie H Grove Rotary mechanism having at least two camming elements
US3998572A (en) * 1974-11-29 1976-12-21 Sealed Power Corporation Spacer-spring for rotary piston engines
US4018548A (en) * 1975-12-08 1977-04-19 Curtiss-Wright Corporation Rotary trochoidal compressor
US4334830A (en) * 1980-03-24 1982-06-15 The Nash Engineering Company Two-stage liquid ring pump with improved intrastage and interstage sealing means
US4411605A (en) * 1981-10-29 1983-10-25 The Trane Company Involute and laminated tip seal of labyrinth type for use in a scroll machine
US4813858A (en) * 1986-05-20 1989-03-21 Mannesmann Rexroth Gmbh Gerotor pump with pressure valve and suction opening for each pressure chamber
US5295814A (en) * 1989-10-04 1994-03-22 Archimedes Associates Inc. Trochoidal rotary piston machine with piston follow-up mechanism
US5538409A (en) * 1993-05-19 1996-07-23 Scalzo Automotive Research Limited Trochoidal piston side seal
US5836181A (en) * 1994-04-18 1998-11-17 Kvaerner Pulping Ab Diffuser
US20030202896A1 (en) * 2002-04-24 2003-10-30 Dong Xingen Jeffrey Hydraulic motor with a separate spool valve

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1366863A (en) * 1963-05-30 1964-07-17 Renault Side sealing rings for rotary engines
US4415317A (en) * 1981-02-09 1983-11-15 The Trane Company Wrap element and tip seal for use in fluid apparatus of the scroll type
KR920703965A (en) * 1989-10-04 1992-12-18 크리스토퍼 에이취. 맥래플린 Rotary piston mechanism seal

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US748348A (en) * 1902-06-16 1903-12-29 Cooley Epicycloidal Engine Dev Company Rotary fluid-engine.
GB190824559A (en) * 1908-11-16 1909-11-04 Fred Umpleby Improvements in and relating to Rotary Internal Combustion Engines.
US1310157A (en) * 1919-07-15 Planoorapii co
DE1057613B (en) * 1957-11-18 1959-05-21 Nsu Werke Ag In-axis rotary piston machine
US3033180A (en) * 1960-01-29 1962-05-08 Curtiss Wright Corp Rotating combustion engine seal construction

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1310157A (en) * 1919-07-15 Planoorapii co
US748348A (en) * 1902-06-16 1903-12-29 Cooley Epicycloidal Engine Dev Company Rotary fluid-engine.
GB190824559A (en) * 1908-11-16 1909-11-04 Fred Umpleby Improvements in and relating to Rotary Internal Combustion Engines.
DE1057613B (en) * 1957-11-18 1959-05-21 Nsu Werke Ag In-axis rotary piston machine
US3033180A (en) * 1960-01-29 1962-05-08 Curtiss Wright Corp Rotating combustion engine seal construction

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3282496A (en) * 1962-11-08 1966-11-01 Radziwill Maciej Sealing means for a power driven machine with a rotary piston
US3366317A (en) * 1966-04-30 1968-01-30 Kloeckner Humboldt Deutz Ag Rotary piston internal combustion engine, especially circular piston internal combustion engine
US3369739A (en) * 1966-04-30 1968-02-20 Kloeckner Humboldt Deutz Ag Rotary piston internal combustion engine, especially circular piston internal combustion engine
US3910733A (en) * 1969-09-18 1975-10-07 Leslie H Grove Rotary mechanism having at least two camming elements
US3827838A (en) * 1973-01-05 1974-08-06 Ramsey Corp Oil seal for rotary piston engines
US3869229A (en) * 1973-03-26 1975-03-04 Toyo Kogyo Co Sealing device for use in rotary piston engine
US3998572A (en) * 1974-11-29 1976-12-21 Sealed Power Corporation Spacer-spring for rotary piston engines
US4018548A (en) * 1975-12-08 1977-04-19 Curtiss-Wright Corporation Rotary trochoidal compressor
US4334830A (en) * 1980-03-24 1982-06-15 The Nash Engineering Company Two-stage liquid ring pump with improved intrastage and interstage sealing means
US4411605A (en) * 1981-10-29 1983-10-25 The Trane Company Involute and laminated tip seal of labyrinth type for use in a scroll machine
US4813858A (en) * 1986-05-20 1989-03-21 Mannesmann Rexroth Gmbh Gerotor pump with pressure valve and suction opening for each pressure chamber
US5295814A (en) * 1989-10-04 1994-03-22 Archimedes Associates Inc. Trochoidal rotary piston machine with piston follow-up mechanism
US5538409A (en) * 1993-05-19 1996-07-23 Scalzo Automotive Research Limited Trochoidal piston side seal
US5836181A (en) * 1994-04-18 1998-11-17 Kvaerner Pulping Ab Diffuser
US20030202896A1 (en) * 2002-04-24 2003-10-30 Dong Xingen Jeffrey Hydraulic motor with a separate spool valve
US6783339B2 (en) * 2002-04-24 2004-08-31 Parker Hannifin Corporation Hydraulic motor with a separate spool valve

Also Published As

Publication number Publication date
DE1426047A1 (en) 1969-04-03
FR1277311A (en) 1961-12-01
OA01636A (en) 1969-09-20
ES270531A1 (en) 1961-12-16
GB995248A (en) 1965-06-16

Similar Documents

Publication Publication Date Title
US3185386A (en) Packing devices comprising fixed and movable elements for rotary engines
US3171590A (en) Oil seal construction for rotary combustion engines
US3193186A (en) Packings for rotary engines
US3251541A (en) Sealing construction for rotary mechanisms
US3506275A (en) Seal construction for rotary combustion engine
US3193188A (en) Rotor and seal construction for rotary mechanisms
US3102518A (en) Seal construction for rotary combustion engine
US3142440A (en) Multi-part apex seal
US3196849A (en) Apex seal construction for rotary combustion engine
US2979042A (en) Seal vent arrangement for rotating combustion engines
US3400691A (en) Seal construction for rotary combustion engines
GB993864A (en) Improvements in or relating to rotary internal combustion engines or the like
US3081745A (en) Gas seal for rotary mechanisms
US3261542A (en) Rotor and seal construction for rotary mechanisms
GB1001247A (en) Radial seals for rotary piston engines
US20130028775A1 (en) Apex seal arrangement for rotary internal combustion engine
US3180560A (en) Sealing system for rotary mechanisms
CA2782794C (en) Apex seal for rotary internal combustion engine
US4060352A (en) Sealing grid system for rotary piston mechanism of the Wankel type
US4219315A (en) Sealing member for orbital or rotary motors
US3193189A (en) Seal means for rotary mechanisms
US3932075A (en) Rotor and sealing grid for rotary engines
US3142439A (en) Sealing means for rotary engine
US3139072A (en) Trochoid compensation for rotary engine
US3277873A (en) Sealing structure