US1537450A - Machine with free flying piston - Google Patents
Machine with free flying piston Download PDFInfo
- Publication number
- US1537450A US1537450A US573492A US57349222A US1537450A US 1537450 A US1537450 A US 1537450A US 573492 A US573492 A US 573492A US 57349222 A US57349222 A US 57349222A US 1537450 A US1537450 A US 1537450A
- Authority
- US
- United States
- Prior art keywords
- piston
- valve
- cylinder
- duct
- admission
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B71/00—Free-piston engines; Engines without rotary main shaft
Definitions
- Thls lnventlon relates to a device for gas control m nternal combustion engines with free flying pistons and artificial atmos-" phere, as well as in devices utilizing said engines, such as engine and compressor group or the like.
- Apparatus of this type comprise no elements at the exterior of the cylinders which are in mechanical connection with the pistons, and'it appears diflicult to provide any such elements susceptible of affording good results, especially since the piston stroke has not necessarily a constant length.
- valve gear or by an auxiliary air compressor, is chiefly used to control the valve gear, and in order to provide for quick action as well as the required exactness and safety, the control of each operation is effected by the element employed to effect the preceding operation.
- Figs 5 and 6 show in sectional elevation and plan view on the line A-B of Fig. 5,
- the motor-compressor group Fig. 1 is essentially constituted as follows:
- the explosion cylinder 1 is situated above the pump cylinder 2 in the upper part f i ff ted ill? l Q l an 9m 1922. Serial No. 573,492.
- a lower or counter pressure cylinder 3 opens freely into a large-sized compressed air reservoir 4 which 1s malntalned at a constant pressure by a regulator not shown corresponding to that disclosed in the copendingapplication 574,-'
- Cylinder 3 has a slightly smaller bore than cylinder 1, and the common piston 5 will therefore comprise three'different crosssections.
- the piston 5 is at the top of the stroke. It effects the slow descent of piston 5 during the first part of the stroke by reason of the difference between cross-sections of'cylinder
- the fresh gas mixture is admitted at the pressure of reservoir 4: into cylinder1 when 1 and cylinder 8.
- The'explosion effects the descent of the pistons against the pressure, v
- the explosion cylinder 1 has an enlarged portion adapted to receivea movable concentric ring 6 which is bored to the same diameter as the cylinder and contains a'plurality of' ports 7 in helical'disposition; Said ring is-provided with a toothed flange 8 co-operating with the pinion 9 actuated by the rod with milled head 10;
- the wall of cylinder 1 and parallel to the axis is formed the bore 11 constituting a cylinder for the piston valve '12.
- a vertical duct 13 and-a horizontal duct 14 serve to connect any one of the ports 7 with the bottom of cylinder 11 when said ports are brought into coincidence with the vertical duct 13 bymeans of the pinion 9.
- the admission valve is shown at 15'.
- the gas mixturev which is compressed toabout 5 kilogrammes per square centimeter, is brought by the conduit 16 into the chamber 17 above which are disposed two cylinders of different di ameter 18,.19, the lattercylinder being closed by the cover 20.
- valve 15 has mounted thereon two differential pistons 22, 23 slidable respectively in cylinders 18, 19.
- Piston 22 has greater cross-section than the disk of the valve 15
- piston 23 has a greater cross-section than piston 22 and is provided with a shaii'k24; traversing the cover with a fluid-tight guiding fit.
- Ignition of the mixture is effected for in-- stance by the break of a primary current passing from thespring '25 to the platinum pointed screw 26 when the rod 24 lifts spring 25 by the closing of thevalve 15.
- An oblique duct 27 communicates with the top of cylinder 19.
- the annular space at the bottom of said cylinder may beclosed, 'or connected with the atmosphere by a narrow passage 28 acting as a dash-pot, orit may be fully open.
- the exhaust valve 29 is provided with the stem 30 which passes through the fluid-tight guide 31; said stem is extended by a piston valve 32 moving within the cylinder 33 and secured to a rod of smaller cross-section 34: slidable in the 1 cylinder cap 35 which is open to the air.
- the bottom of said piston valve has formed therein. an orifice whence proceeds .a duct of'right-angled form 36 opening into the annular-groove 3710f cylinder .33 having r oponing therein the lower end offport 27 ve-mentioned, .aswell as a duct 38.
- the .duct39 also opens into cylinder 33 some- ,whatabove the bottom of the latter.
- The, piston vale 12 has two different cross-sections at 4:1 and 42 and is provided with two annular grooves 43 and 44;.
- the groove 43 cooperates with duct 39 and-duct 4.5 'commimiclating' with the compressed air reservoir 4.
- the groove 4: 1 has opening therein.
- the pressure of the mixture causes the descent of piston 5, Fig. 3 thereby enabling valve 15 to open to its full extent, and also uncovering the port 7 corresponding to the quantity of gas mixture admitted.
- the compressed mixture is thus introduced be low the piston valve 12 by ducts 13 and 14, thereby raising the latter; this movement first closes the communication between duct 39 and the compressed air reservoir and then opens duct 38 to the atmosphere through the groove 44 of valve 12 and the duct 46.
- Figs. 5 and 6 shew, arrangements of the valve gear of the air pump.
- the suction valves have a common seat upon the ring 47 Figs. 1, 5 and 6, which is mounted at the top ofthe compressor cylinder 2 and provided upon the entire circumference with orifices having the trapezoidal shape shown in Figures 5, 6.
- the radius of the bore 65 in which the said orifices 48 open is larger than the radius of cylinder 2 by somewhat more than the thickness of the clack valves 49 serving to close said orifices.
- the inner wall 65 of the ring 47 is circular so that it may be produced by machining and may be used as a common seat for the clack valves 49.
- Plates 50 also having a trapezoidal shape, as shown, are provided after casting so as to eliminate any milling and in order to guide the said valves.
- the said plates may be considered as fragments of a tube which just enter the ring 47and do not ext-end so high as the ports 48 as shown in Fig. 5.
- the valves 49 oscillate upon their base and are engaged in the rear of a flange 51, whilst the movement of the top of the valves is limited laterally by a slotted ring 52 and at the top by a lower surface of the plate 53.
- the passages 48 open at the rear into a circular passage 54 connected with the exterior by the apertures 55 formed around the entire periphery of the pump cylinder 2; said apertures are adapted to be gradually closet by a revolving shutter 56.
- the cooling water wh ch is brought by the circular passage 57 is supplied through ducts 58 into each of the passages 48.
- the discharge valves are mounted on a heavy plate 59 which is held pressed between the flanges of the explosion cylinder and the flanges of the compressor cylinder, said plate being provided around the circumference with the circular apertures 60 which are narrowed at the bottom in order to form seats for the valves.
- Said valves are preferably constituted by the balls 61 of metal, hard stone or the like which are vertically guided by a cage (32 bored to the diameter of the ball and provided with a. cross-piece 63 tor limiting the upward movement; all the HIKIUU'GS (it) open into a circular passage 64.
- Gas control system particularly. applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air constituting an artificial atmosphere, comprising an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said rod, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admission piston is submitted to 'the'pressure of the gas mixture, an-exhanst valve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exhaust piston, a duct for the communication of said exhaustcylinder with the upper face of the upper admission piston, a duct through said inner exhaust piston, an outer exhaust piston'above said inner exhaust piston, acylinder cap for said outer exhaust piston,- a piston slide valve, grooves in said piston slide valve, means for the communicationthrough one oi said grooves of above said exhaustcylinder with the compressed air reservoir, means for the com municationthrough another groove of said exhaustc lindcr with the atmos here,
- Gas control system particularly applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air constituting an artificial atmosphere
- an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said red, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admission piston is submitted to the pressure of the gas mixture, a shank provided on said upper admission piston, an electrically con nected spring lying on said shank, platinum pointed screw opposite said spring, an exhaustvalve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exliaust piston, a duct for the communication of said cylinder with the upper iace of the upper admission piston, a duct through said inner exhaust piston, an outer exhaust piston above said inner exhaust p ston, a-cyl nder cap for sa d outer exhaust piston, a piston slide valve, grooves in said piston slide valve, means for the communication through 7
- Gas control system particularly applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air. constituting an artificial atmosphere comprising an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said rod, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admisson piston is submitted to the pressure of the gas mixture, an exhaust valve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exhaust piston, a duet for the eommunicatlon of said exhaust cylinder with the upper face of the upper admission 1 piston, a duet through said inner exhaust aiston a c linder ea 9 for said outer exhaust I I I I u a a piston, a piston slide valve, grooves 1n Stud piston slide valve, means for the eommunieationthrough'one'of said grooves of above 'inder with the atmosphere, a ieylinder for said piston
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Description
May 12, 1925. 1,537,450
J. BABIN MACHINE WITH FREE FLYING PISTON I Filed July 7, 1922 2 Sheets-Sheet 1 63 v 28 I (Ag 11, L i 5s V r I r r Ii 5; 9 far/e0}?! May 12, 1925.
. J. BABIN MACHINEWITH FREE FLYING PISTON- 2 Sheets-Sheet 2 July 7, 1922 Patented May 12, 1925.
UNITED STATES JULES'BABIN, 0F PARIS, FRANCE.
PATENT 0mm.
MACHINE WITH FREE FLYING PISTON.
Application filed. July 7,
To all whom it may concern:
Be it known that 1, Johns BABIN, citizen of the French Republic, residing 25 Boulevard Malesherbes, Paris, France, have invented certain and useful Improvements in ll lachines with Free Flying Pistons, of
which the following is a specification.
Thls lnventlon relates to a device for gas control m nternal combustion engines with free flying pistons and artificial atmos-" phere, as well as in devices utilizing said engines, such as engine and compressor group or the like.
Apparatus of this type comprise no elements at the exterior of the cylinders which are in mechanical connection with the pistons, and'it appears diflicult to provide any such elements susceptible of affording good results, especially since the piston stroke has not necessarily a constant length.
According to my invention, the compressed air produced by the apparatus itself,
or by an auxiliary air compressor, is chiefly used to control the valve gear, and in order to provide for quick action as well as the required exactness and safety, the control of each operation is effected by the element employed to effect the preceding operation.
By reason of the ig Piston Speed employed' Fig. 2 in the various stagesof operation.
Figs 5 and 6 show in sectional elevation and plan view on the line A-B of Fig. 5,
the suction and delivery valve devices as ap plied to the air pump of a motor-compressor. r 1
The motor-compressor group Fig. 1 is essentially constituted as follows:
The explosion cylinder 1 is situated above the pump cylinder 2 in the upper part f i ff ted ill? l Q l an 9m 1922. Serial No. 573,492.
pression of air, the lower 'part being open to the atmosphere' A lower or counter pressure cylinder 3 opens freely into a large-sized compressed air reservoir 4 which 1s malntalned at a constant pressure by a regulator not shown corresponding to that disclosed in the copendingapplication 574,-'
113. Cylinder 3 has a slightly smaller bore than cylinder 1, and the common piston 5 will therefore comprise three'different crosssections.
the piston 5 is at the top of the stroke. It effects the slow descent of piston 5 during the first part of the stroke by reason of the difference between cross-sections of'cylinder The fresh gas mixture is admitted at the pressure of reservoir 4: into cylinder1 when 1 and cylinder 8. The'explosion effects the descent of the pistons against the pressure, v
in tank 4. Upon the completion of the down stroke of the piston, the same is driven-upwardly by the pressure of the compressed air of the reservoir4; the burnt gas is'thus discharged from cylinder 1 into the atmos phere, and the series of operations recom mences.
The fluid control devices are shewn in detail in Fig. 2. At the upper part, the explosion cylinder 1 has an enlarged portion adapted to receivea movable concentric ring 6 which is bored to the same diameter as the cylinder and contains a'plurality of' ports 7 in helical'disposition; Said ring is-provided with a toothed flange 8 co-operating with the pinion 9 actuated by the rod with milled head 10; In, the wall of cylinder 1 and parallel to the axis is formed the bore 11 constituting a cylinder for the piston valve '12., A vertical duct 13 and-a horizontal duct 14 serve to connect any one of the ports 7 with the bottom of cylinder 11 when said ports are brought into coincidence with the vertical duct 13 bymeans of the pinion 9. c U
The admission valve is shown at 15'. The gas mixturev which is compressed toabout 5 kilogrammes per square centimeter, is brought by the conduit 16 into the chamber 17 above which are disposed two cylinders of different di ameter 18,.19, the lattercylinder being closed by the cover 20. The
Ignition of the mixture is effected for in-- stance by the break of a primary current passing from thespring '25 to the platinum pointed screw 26 when the rod 24 lifts spring 25 by the closing of thevalve 15.
An oblique duct 27 communicates with the top of cylinder 19. The annular space at the bottom of said cylinder may beclosed, 'or connected with the atmosphere by a narrow passage 28 acting as a dash-pot, orit may be fully open. The exhaust valve 29 is provided with the stem 30 which passes through the fluid-tight guide 31; said stem is extended by a piston valve 32 moving within the cylinder 33 and secured to a rod of smaller cross-section 34: slidable in the 1 cylinder cap 35 which is open to the air.
, The bottom of said piston valve has formed therein. an orifice whence proceeds .a duct of'right-angled form 36 opening into the annular-groove 3710f cylinder .33 having r oponing therein the lower end offport 27 ve-mentioned, .aswell as a duct 38. The .duct39 also opens into cylinder 33 some- ,whatabove the bottom of the latter. The
' duct t0 communicates, with the upper an V nularfportion of cflinder. 33 and with the reservoir of .air .un er pressure. 9
The, piston vale 12 has two different cross-sections at 4:1 and 42 and is provided with two annular grooves 43 and 44;. The groove 43 cooperates with duct 39 and-duct 4.5 'commimiclating' with the compressed air reservoir 4. The groove 4: 1 has opening therein. ion one side the duct 38 and on the other the duct 4L6 opening to the .Saliddeviceis operated in the following manner Having previously determined the volume of the charge of gas mixture,- the ring :6 is rotated by means of pinion .9 so asto bring into coincidence with duct 18 the given orifice twhich the piston 5 will uncover when "forth hereunder; the piston valve 12 is at the bottom of the stroke; v When the" disc of va lve 29 comes very near its seat, the
lower .edge of piston valve 32 will {uncover duct 39; "the compressed air which enters through passage t'5,'groove 43 of the valve 1.2 will suddenly enter the lower part of cyl' inder 33 and the duct 39 raising the piston sition for commencing a new valve 32 and thus completing the closing action of valve 29; this compressed air pro- 7 ceeds through duct 36, groove 37 and duct 27, into the space above piston 23, thus open ing the valve 15 which is at once caused to bear upon the top of piston 5.
The pressure of the mixture causes the descent of piston 5, Fig. 3 thereby enabling valve 15 to open to its full extent, and also uncovering the port 7 corresponding to the quantity of gas mixture admitted. The compressed mixture is thus introduced be low the piston valve 12 by ducts 13 and 14, thereby raising the latter; this movement first closes the communication between duct 39 and the compressed air reservoir and then opens duct 38 to the atmosphere through the groove 44 of valve 12 and the duct 46. I
The compressed air which exerted'pres, sure uponthe top of piston 23 of admission valve 15 will now be discharged through duct 27, groove 37, ducts 36 and 38, groove 44 and duct 46, and the valve 15 will he closed by the pressure of the gas mixture, which enters through conduit 16 and alone acts upon the bottom of piston 22. When rising, the shank 24; lifts the contact spring 25 and breaks the current, thereby igniting the charge of gas. At the same time, the pressure in the lower part of cylinder '33 will have diminished and hecome equal to atmospheric pressure, the exhaust'valve 29 will, however, remain closedunder the effect of the pressure exerted thereupon in the first place by the mixture in the cylinder and subsequently by the gas of the explosion.
'VVhen piston 5 under the effect of the explosion is near the bottom of the stroke, Fig. 4, the pressure .of the burnt gas will be reduced .to such degree that its action upon the valve 29 becomes less than thepre'ssure of the compressed air upon the annular surface at the top of the valve 32, and therefore the valve :QQKVl l'l open to permit the escape of the hurnt gas to the atmosphere. .At the same time, andfby reason of the; pressure of the compressed air upon the differential sections of the groove 44, valve 12 will return to the lower position. When this takes place, the whole device is in the proper pocycle of operations above set forth.
dVi-th said arrangement, itis observed that each operation, at the exact moment when it is completed, controls the immediately following. operation. By reason of ,what'may "be termed a pneumatic interlock-ing action,
the failure of any one element'will not give rise to any accident, but will only cause the stopping of theapparatus. f 7
Figs. 5 and 6 shew, arrangements of the valve gear of the air pump.
By reason of the high piston speed resulting from theoperation of the motor, it is The suction valves have a common seat upon the ring 47 Figs. 1, 5 and 6, which is mounted at the top ofthe compressor cylinder 2 and provided upon the entire circumference with orifices having the trapezoidal shape shown in Figures 5, 6. The radius of the bore 65 in which the said orifices 48 open is larger than the radius of cylinder 2 by somewhat more than the thickness of the clack valves 49 serving to close said orifices. The inner wall 65 of the ring 47 is circular so that it may be produced by machining and may be used as a common seat for the clack valves 49. Plates 50 also having a trapezoidal shape, as shown, are provided after casting so as to eliminate any milling and in order to guide the said valves. The said plates may be considered as fragments of a tube which just enter the ring 47and do not ext-end so high as the ports 48 as shown in Fig. 5. The valves 49 oscillate upon their base and are engaged in the rear of a flange 51, whilst the movement of the top of the valves is limited laterally by a slotted ring 52 and at the top by a lower surface of the plate 53.
The passages 48 open at the rear into a circular passage 54 connected with the exterior by the apertures 55 formed around the entire periphery of the pump cylinder 2; said apertures are adapted to be gradually closet by a revolving shutter 56. The cooling water wh ch is brought by the circular passage 57 is supplied through ducts 58 into each of the passages 48. V
The discharge valves are mounted on a heavy plate 59 which is held pressed between the flanges of the explosion cylinder and the flanges of the compressor cylinder, said plate being provided around the circumference with the circular apertures 60 which are narrowed at the bottom in order to form seats for the valves. Said valves are preferably constituted by the balls 61 of metal, hard stone or the like which are vertically guided by a cage (32 bored to the diameter of the ball and provided with a. cross-piece 63 tor limiting the upward movement; all the HIKIUU'GS (it) open into a circular passage 64.
ll hat I claim is: V
1. Gas control system particularly. applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air constituting an artificial atmosphere, comprising an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said rod, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admission piston is submitted to 'the'pressure of the gas mixture, an-exhanst valve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exhaust piston, a duct for the communication of said exhaustcylinder with the upper face of the upper admission piston, a duct through said inner exhaust piston, an outer exhaust piston'above said inner exhaust piston, acylinder cap for said outer exhaust piston,- a piston slide valve, grooves in said piston slide valve, means for the communicationthrough one oi said grooves of above said exhaustcylinder with the compressed air reservoir, means for the com municationthrough another groove of said exhaustc lindcr with the atmos here, a c ly P y inder for said p'ston slide valve and means for the communication of the bottom of said cylinder with the upper part of the power cylinder.
2. Gas control system particularly applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air constituting an artificial atmosphere comprising .an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said red, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admission piston is submitted to the pressure of the gas mixture, a shank provided on said upper admission piston, an electrically con nected spring lying on said shank, platinum pointed screw opposite said spring, an exhaustvalve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exliaust piston, a duct for the communication of said cylinder with the upper iace of the upper admission piston, a duct through said inner exhaust piston, an outer exhaust piston above said inner exhaust p ston, a-cyl nder cap for sa d outer exhaust piston, a piston slide valve, grooves in said piston slide valve, means for the communication through 7 one of said grooves of above'said exhaust cylinder with the compressed air reservoir, means for the communication through another groove of said exhaust cylinder with the atmosphere, a cylinder for said piston slide valve and means for the communication of the bottom of said cylinder with the upper part of the power cylinder. Y
3. Gas control system particularly applicable to motor compressor apparatus of the internal combustion type with free flying piston and reservoir of compressed air. constituting an artificial atmosphere comprising an admission valve for previously compressed explosive mixture, a rod for said valve, two admission pistons mounted on said rod, the cross section of the upper admission piston being greater than the cross section of the lower admission piston, means whereby the lower face of the lower admisson piston is submitted to the pressure of the gas mixture, an exhaust valve for burnt gas, a rod for said valve, an inner exhaust piston on said rod, an exhaust cylinder for said inner exhaust piston, a duet for the eommunicatlon of said exhaust cylinder with the upper face of the upper admission 1 piston, a duet through said inner exhaust aiston a c linder ea 9 for said outer exhaust I I I u a a piston, a piston slide valve, grooves 1n Stud piston slide valve, means for the eommunieationthrough'one'of said grooves of above 'inder with the atmosphere, a ieylinder for said piston slide valve, a revoluble ring .oon-
.stituting the upper part of the power eylin- ,der, a' plurality of orifices, which are situated atv different heights provided in said ring, and means for the .coinmunlcatlon of the bottom of the cylinder of the piston slide valve with the power cylinder through-one of said orifices.
In witness whereofl have hereunto set my hand.
,JULES BABIN. I Y
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US573492A US1537450A (en) | 1922-07-07 | 1922-07-07 | Machine with free flying piston |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US573492A US1537450A (en) | 1922-07-07 | 1922-07-07 | Machine with free flying piston |
Publications (1)
Publication Number | Publication Date |
---|---|
US1537450A true US1537450A (en) | 1925-05-12 |
Family
ID=24292202
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US573492A Expired - Lifetime US1537450A (en) | 1922-07-07 | 1922-07-07 | Machine with free flying piston |
Country Status (1)
Country | Link |
---|---|
US (1) | US1537450A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2936743A (en) * | 1956-11-19 | 1960-05-17 | Stirling A Colgate | Internal combustion apparatus |
-
1922
- 1922-07-07 US US573492A patent/US1537450A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2936743A (en) * | 1956-11-19 | 1960-05-17 | Stirling A Colgate | Internal combustion apparatus |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2035203A (en) | Method of and apparatus for feeding fuel | |
US1036288A (en) | Gaseous-power generator. | |
US1537450A (en) | Machine with free flying piston | |
US2065025A (en) | Internal combustion engine of the liquid fuel injection compression ignition type | |
US2030732A (en) | Internal combustion engine | |
US1113456A (en) | Gas-engine. | |
US2041081A (en) | Rocket engine | |
US2072474A (en) | Internal combustion engine | |
US2920444A (en) | Pulse reaction combustion engine | |
US1077150A (en) | Internal-combustion engine. | |
US1621936A (en) | Constant-pressure internal-combustion engine | |
US2068311A (en) | Method and apparatus for introducing explosive charges into internal combustion engines | |
US1671271A (en) | Sleeve-valve engine | |
US1971013A (en) | Valve | |
US2272171A (en) | Internal combustion engine | |
US1027841A (en) | Fluid-compressor. | |
US2062621A (en) | Oil engine | |
DE657765C (en) | Compound internal combustion engine | |
DE477402C (en) | Control of the exhaust valve of four-stroke internal combustion engines by the explosion gas pressure | |
US1251043A (en) | Method and apparatus for burning fuel. | |
Spanogle et al. | A Description and Test Results of a Spark-ignition and a Compression-ignition 2-stroke-cycle Engine | |
US458073A (en) | Motoren-pabrik-deutz | |
US1091963A (en) | Two-cycle engine. | |
US2354778A (en) | Fuel conserving device for internal-combustion motors | |
US1849220A (en) | Monocycle internal combustion engine |