US1420282A - Compression-relief system for star-shaped engines - Google Patents
Compression-relief system for star-shaped engines Download PDFInfo
- Publication number
- US1420282A US1420282A US511796A US51179621A US1420282A US 1420282 A US1420282 A US 1420282A US 511796 A US511796 A US 511796A US 51179621 A US51179621 A US 51179621A US 1420282 A US1420282 A US 1420282A
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- Prior art keywords
- compression
- star
- bosses
- engines
- ring
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
- F01L13/08—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for decompression, e.g. during starting; for changing compression ratio
Definitions
- the system according to the invention permits of diminishing the filling of the cylinders and the compression by acting on the control devices of the valves, by modifying the relative periods of opening.
- ig. 1 is a cross-section on the line A-A (Fig. 2) of a compression relief system for engines of the star type, according to the invention.
- Fig. 2 is a section on the line BB (Fig. 1) with a partial axial section of a cylinder.
- Fig. 3 is a second section on the line CC (Fig. 1).
- A is the ring carrying the cams G of an ordinary valve gear, for this class of engines.
- the relief system consists of an annular member or ring E carrying as many retaining levers B- as there are pusher rods P for the control of the valves whose action is to be considered.
- the said annular member E is revoluble on a support S having as many bosses or gradients T as there are levers.
- the ring E is actuated from the exterior of the engine by a shaft I having a crank M exerting an effort in the groove of a piece N secured to the ring E.
- the ring A carrying the cams C is provided laterally with as many lateral bosses D as there are cams.
- the action takes place upon the admission valves, and the device operates as follows: For the starting, by acting upon the shaft I in the proper direction, the ring E rotates through a certain angle; the arms 0 of the retainin levers leave the bosses T, the springs 1% Specification 6f Letters'Patent. P te ted June 20,1922;
- this piston may compress the mixture remaining in the cylinder, but the effort necessary to obtain this small compression is much less than the normal effort, and is the smaller as the valve remains open the longer and as the crank brings the piston nearer to the end of the stroke.
- the starting revolutions may thus be carried out with a small effort.
- the relief device In the normal working of the engine, the relief device is thus completely at rest, without touching any or" the parts in movement, and cannot cause any hindrance to the running.
- a compression relief device for internal combustion engines having radial cylinders having radial cylinders
- compression relief device for internal combustion engines having radial cylinders, comprising a ring having cams thereon, means for rotating said ring, pusher rods adapted to be operated by the cams, valves in the engine cylinders, means for operatively connecting said valves to the pusher rods, springs tending to close said valves, an annular member, means for supporting said annular member concentrically with the cam ring, means for rotating said annular member by a certain angle, spring controlled bell crank levers pivoted on said annular member, stationary bosses on a fixed part of the device and releasing bosses on the cam ring, one arm of the said bell crank levers being adapted to engage with the stationary bosses and the other arm thereof being adapted to engage with the pusher rods and the releasing bosses.
Description
P. J. R. POSTEL-VINAY. COMPRESSION RELIEF SYSTEM FOR STAR SHAPED ENGINES.
' APPLICATION FILED OCT- 31,1921- V 1 ,420,282. Patented June 20, 1922.
2 SHEETS-SHEET 1.
P. I. R. POSTEL-VIN AY. COMPRESSION RELIEF SYSTEM FOR STAR SHAPED ENGINES.
APPLICATION FILED OCT- 31, 192i- Patented June 20, 1922. v
2 SHEETS-SHEET 2.
[71,"; fan.
{ P J. H. Rnrcl-V/my/ UNITED STATES eATENr OFFICE.
PIERRE JEAN RENE rosrnL-vINAY, or PARIS, FRANCE, ASSIGNOR r SOCIETE ,nn's
"ivro'rnuRs SALIVISON sYsTR EcAN'rON-URNE on runs, rRAivcn.
' ooiurRnssron-Rnnmr SYSTEM FOR STAR-SHAPED ENGINES.
Application filed October 31, 1921. Serial No. 511,796.
To all whom it may concern:
Be it known that I, PIERRE JEAN RENfi PosTEL-VINAY, citizen of the French Republic, residing at Paris, in the Republic of France, have invented new and useful Improvements in Compression-Relief Systems for Star-Shaped Engines, of which the following is a specification.
In order to facilitate the starting thereof, there have already been used in engines having longitudinally disposedcylinders devices for modifying the filling of the cylinders, and acting to diminish the compression. 7 g
In engines having cylinders'in star disposition, the same arrangements of parts are not available in practice;
The system according to the invention permits of diminishing the filling of the cylinders and the compression by acting on the control devices of the valves, by modifying the relative periods of opening.
It is applicable to engines of the star type having valve gear concentric with the driving shaft.
In the accompanying drawing and by wa of example:
ig. 1 is a cross-section on the line A-A (Fig. 2) of a compression relief system for engines of the star type, according to the invention.
Fig. 2 is a section on the line BB (Fig. 1) with a partial axial section of a cylinder.
Fig. 3 is a second section on the line CC (Fig. 1).
As shown in the drawing, A is the ring carrying the cams G of an ordinary valve gear, for this class of engines.
The relief system consists of an annular member or ring E carrying as many retaining levers B- as there are pusher rods P for the control of the valves whose action is to be considered.
The said annular member E is revoluble on a support S having as many bosses or gradients T as there are levers.
The ring E is actuated from the exterior of the engine by a shaft I having a crank M exerting an effort in the groove of a piece N secured to the ring E.
The ring A carrying the cams C is provided laterally with as many lateral bosses D as there are cams.
In the example described, the action takes place upon the admission valves, and the device operates as follows: For the starting, by acting upon the shaft I in the proper direction, the ring E rotates through a certain angle; the arms 0 of the retainin levers leave the bosses T, the springs 1% Specification 6f Letters'Patent. P te ted June 20,1922;
cause the levers to rise in the plane of the pusher rods. As the action continues, these levers B gradually raise by their ends the pusher rods by acertain height which is considered suflicient, but which-is only a portion of the ordinary lift produced by the cams C. All the pusher rods forjthe admission, except those already raised by the cams C, are raised. All the cylinders are thus in communication with the admission" manifold. The couple of rotation,
necessary for the beginning of the'engine starting is therefore extremely small.
' By continuing to exert this effort of roe tation' to obtain the starting, it happens that: the cams C move in co-ordinated time under the rollers of the pusher rods, raising the latter as if to effect a normal admission, but during the descent for the closing, the
pusher rod P is retained by the lever B.
It is only when the bosses D of the cam ring have driven back the lever B, that the pusher rod is released and that the admission valve falls again on its seat.
The angular distance of these bosses D with reference to the cams is regulated in such manner that, by means of the valve which has remained open, the piston when rising again for compression in its cylinder may drive without difficulty a considerable part of the cylinder contents into the admission manifold.
When the valve has again fallen, this piston may compress the mixture remaining in the cylinder, but the effort necessary to obtain this small compression is much less than the normal effort, and is the smaller as the valve remains open the longer and as the crank brings the piston nearer to the end of the stroke.
The starting revolutions may thus be carried out with a small effort.
The cycles with low compression follow each other regularly, for when once the bosses D have passed by, the lever B is returned against the pusher rod by its spring R, but it occupies its retaining position only when the cam is commencing the admission at the normal point, has raised the pusher rod in order to permit the spring R to effect the complete return of the lever to itsrstraight position.
When the engine has started, and when a sufficient speed is acquired Which is able to stand the normal compressions, the shaft I is no longer actuated; by the eliect of the control devices or of a spring V, the ring E is returned, drawing with it the retaining levers B which are released from the pusher rods in their plane. The small arms 0 of the levers then rise upon the bosses T, thereby tilting to the rear the arms B which will thus clear the bosses D.
In the normal working of the engine, the relief device is thus completely at rest, without touching any or" the parts in movement, and cannot cause any hindrance to the running.
Having now described my invention, what 1 claim as new and'desire to secure by Letters Patent is: V
1. A compression relief device for internal combustion engines having radial cylinders,
comprising a ring having cams thereon,-
means for rotating said ring, pusher rods adapted to be operated by the cams, valves in the engine cylinders, means for operatively connecting said valves to the pusher rods, springs tending to close said valves, an annular member, means for supporting said annular member concentrically with the cam ring, means "for rotating said annular memher by a certain angle, spring controlled levers pivoted on said annular member and adapted to engage with the pusher rods for preventing the valves from closing, stationary bosses adapted to act on said levers and releasing bosses on the cam ring adapted to act u on the levers.
2. compression relief device for internal combustion engines having radial cylinders, comprising a ring having cams thereon, means for rotating said ring, pusher rods adapted to be operated by the cams, valves in the engine cylinders, means for operatively connecting said valves to the pusher rods, springs tending to close said valves, an annular member, means for supporting said annular member concentrically with the cam ring, means for rotating said annular member by a certain angle, spring controlled bell crank levers pivoted on said annular member, stationary bosses on a fixed part of the device and releasing bosses on the cam ring, one arm of the said bell crank levers being adapted to engage with the stationary bosses and the other arm thereof being adapted to engage with the pusher rods and the releasing bosses.
In testimony whereof I have signed my name to this specification.
PIERRE JEAN RENE POSTEL-VINAY.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US511796A US1420282A (en) | 1921-10-31 | 1921-10-31 | Compression-relief system for star-shaped engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US511796A US1420282A (en) | 1921-10-31 | 1921-10-31 | Compression-relief system for star-shaped engines |
Publications (1)
Publication Number | Publication Date |
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US1420282A true US1420282A (en) | 1922-06-20 |
Family
ID=24036484
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US511796A Expired - Lifetime US1420282A (en) | 1921-10-31 | 1921-10-31 | Compression-relief system for star-shaped engines |
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US (1) | US1420282A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619948A (en) * | 1948-12-14 | 1952-12-02 | Ricardo & Co Engineers | Decompression mechanism for reciprocating internal-combustion engines |
-
1921
- 1921-10-31 US US511796A patent/US1420282A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2619948A (en) * | 1948-12-14 | 1952-12-02 | Ricardo & Co Engineers | Decompression mechanism for reciprocating internal-combustion engines |
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