US926641A - Explosive-engine. - Google Patents

Explosive-engine. Download PDF

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Publication number
US926641A
US926641A US39695907A US1907396959A US926641A US 926641 A US926641 A US 926641A US 39695907 A US39695907 A US 39695907A US 1907396959 A US1907396959 A US 1907396959A US 926641 A US926641 A US 926641A
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valves
piston
engine
valve
abutments
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US39695907A
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Cecil C Coffey
Tony Pfennighausen
Elvin A Robinson
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines

Definitions

  • CECIL C COFFEY, TONY PFENNIGHAUSEN, AND ELVIN A. ROBINSON, OI RIVERSIDE, CALIFORNIA.
  • This invention relates to explosive engines of the rotary t pc in which theimpulse from successive exp osions causes rotation of the rotary piston or drum of the engine, and relates more particularly to an engine of that class in which the rotatable element is provided with radial abutments which cooperate with synchronously rotated valves to compress the charges at one stage in the movement of the element and to receive the impulses from the explosions of another stage.
  • the invention has for one of its objects to improve and simplify the construction and operation of devices of this character, so as to be comparatively easy and inexpensive to manufacture, composed of few parts, and efliolent in action.
  • a further object of the invention is the provision of'an engine comprising a rotatable element having a plurality of abutments or radial projections thereon, and valves cooperating with the projections for producing the necessary functions to carr out the operation of the engine, there more sets of valves, one valve of which assists in the compression of the charges and the utilization of the ex loded gases, while the other is essential to t e exhaust and the admission of the spent gases and charges.
  • the invention comprises the various novel fea-. tures of construction and arrangement of arts which will be more fully described ereinafter nd set forth with particularity in the claim appended hereto.
  • Figure 1 is a front view of the engine.
  • Fig. 2 is a similar view with the front Specification of Letters Patent.
  • Fig. 3 is a rear view with the rear head removed.
  • Fig. 4 is a central vertical section of the engine.
  • A designates the body of the engine which is preferably a casting formed with a cylindrical casing 1 and a transverse partition 2, there being on I opposite sides of the partition, a piston chamber 3 at the front and a gear chamber 4 at the rear.
  • pockets or compartments 5 in which are housedvalves, and on the op )osite side of. the partition 2 and in line wit 1 the compartments 5 are pinion containing compartments 6.
  • openings 7 through which project valve-carrying shafts 8, and on the shafts are valves 9 and pinions 10 disposed respectively in the compartments 5 and 6, the said pinions forming drivers for the valves.
  • a rotary piston 11 that is mounted on a shaft 12, the saidshaft extending through an opening 13 in the PitItltlOIl' 2 for reeelving a gear 14 disposed in the chamber 4 and meshing at diam'etric' ally opposite points with the pinions 10, so
  • valves that all of the valves will be driven simultaneously.
  • the open sides of the chambers in the casing are closed by front and rear heads 15 and 16 and these heads are provided with bearings 17 in which the ends of the pimon shafts rotate and also with central bearings for the main shaft 12.
  • valves 9 are em loyed and are arranged on two right-angular y disposed diagonal lines, and each-valve is provided with three cavities or cups 19 arranged at one hundred and twenty degrees apart, and into these cavities engage projections or abutments 20 extending radiallyfrom the piston or drum 11 and arranged seventy-two degrees apart.
  • the piston is provided'with one more abutment than there are number of valves, when each valve is lpqrovided w1th three cavities or oekets.
  • e drum is of smaller diameter t an the chamber 3 so that the segmental spaces between each pair of adjacent abutments forms working or explosion chambers and the peripheral surfaces of the valves are adapted to contact with the peripheral surface of the piston between the abutments and the abutments engage with the circular surfaces of the pockets or cavities 19, the valves and pistons meshing after the fashion of gear wheel and pinions.
  • the flat surfaces of the valves are provided with packing members 21 that bear on the flat surfaces of the compartments 5 so that leakage of the working fluid will be revented.
  • the piston 11 is provided with pac 'ng members 22 set into the ends thereof to bear against the internal fiat walls of the chamber 3 for the purpose of preventing leakage and the projections or abutments 20 have packing strips 23 extending radially at the sides thereof and packing strips 24 as shown in Fig. 4, that extend along the crests of the said abutments so as to contact with the internal circular surface of the chamber 3. Disposed two opposite valves are admission and exhaust ports 25 and 26 respectively, which communicate with a the segmental working chambers or spaces between adjacent abutments.
  • the exhaust ports are located on the approach side of the adjacent valves, while the admission ports are located on the leaving side'of the said valves so that as an abutment approaches one of such valves, the spent gases behind the abutment will be forced out through the exhaust port until the said abutment meshes with the valve While a charge of explosive mixture will be admitted between the preceding abutmerit and valve so that as the piston rotates, the admitted charge will be compressed by the first-mentioned abutment and succeeding valve. Adjacent the leaving side of each of the other valves are s ark plugs 27 for the purpose of igniting the charges after the same have been compressed.
  • the engine may be started by hand or in any other suitable manner, and by rotating the piston, a charge of mixture will be compressed in one of the other of the valves and immediately fired so that an impulse will be given to the piston which will be sufiicient to set the engine into operation.
  • a charge of mixture is partially compressed in the space designated a, while a charge has been exploded in the space I) and the exploded gases are operating on the abutment c. This forces the piston around in a clockwise direction and the exhaust gases in the space (1 on the opposite slde of the abutment c are being discharged through the lowermost exhaust port 26.
  • the structure of the engine is such that it may be used as a compressor.
  • the ignition device is dispensed with and power applied to the shaft so as to rotate the piston, thereby drawing fluid into the casing and causing it to be delivered under pressure.

Description

O. G. OOFFEY, T. PFENNIGHAUSEN & E. A. ROBINSON. EXPLOSIVE ENGINE.
APPLICATION FILED 00T.11,1907.
Patented June 29, 1909.
2 SHEETS-SHEET 1.
UNITED STATES PATENT ()FFICE.
CECIL C. COFFEY, TONY PFENNIGHAUSEN, AND ELVIN A. ROBINSON, OI RIVERSIDE, CALIFORNIA.
EXPLOSIVE-ENGINE To all whom it may concern:
Be it known that we, CECIL O. COFFEY, TONY PFENNIGHAUSEN, and ELVIN. A. Ron- INSON, citizens of the United States of America, residing at Riverside, in the county of Riverside and State of California, have invented new and useful Improvements in Explosive-Engines, of which the following is a specification.
This invention relates to explosive engines of the rotary t pc in which theimpulse from successive exp osions causes rotation of the rotary piston or drum of the engine, and relates more particularly to an engine of that class in which the rotatable element is provided with radial abutments which cooperate with synchronously rotated valves to compress the charges at one stage in the movement of the element and to receive the impulses from the explosions of another stage. The invention has for one of its objects to improve and simplify the construction and operation of devices of this character, so as to be comparatively easy and inexpensive to manufacture, composed of few parts, and efliolent in action.
A further object of the invention is the provision of'an engine comprising a rotatable element having a plurality of abutments or radial projections thereon, and valves cooperating with the projections for producing the necessary functions to carr out the operation of the engine, there more sets of valves, one valve of which assists in the compression of the charges and the utilization of the ex loded gases, while the other is essential to t e exhaust and the admission of the spent gases and charges.
With these objects in view and others, as will appear as the description proceeds, the invention comprises the various novel fea-. tures of construction and arrangement of arts which will be more fully described ereinafter nd set forth with particularity in the claim appended hereto.
In the accom anying drawings, which illustrate one of t e embodiments of the invention, Figure 1 is a front view of the engine. Fig. 2 is a similar view with the front Specification of Letters Patent.
Application filed October 11, 1907.
eing one or Patented June 29, 1909.
Serial No. 396,959.
head removed. Fig. 3 is a rear view with the rear head removed. Fig. 4 is a central vertical section of the engine.
Similar reference characters are employed to designate corresponding parts throughout the several views. a
Referring to the drawings, A designates the body of the engine which is preferably a casting formed with a cylindrical casing 1 and a transverse partition 2, there being on I opposite sides of the partition, a piston chamber 3 at the front and a gear chamber 4 at the rear. At diametrically opposite points are pockets or compartments 5 in which are housedvalves, and on the op )osite side of. the partition 2 and in line wit 1 the compartments 5 are pinion containing compartments 6. In the partition 2 are openings 7 through which project valve-carrying shafts 8, and on the shafts are valves 9 and pinions 10 disposed respectively in the compartments 5 and 6, the said pinions forming drivers for the valves. a
In the piston chamber 3 is a rotary piston 11 that is mounted on a shaft 12, the saidshaft extending through an opening 13 in the PitItltlOIl' 2 for reeelving a gear 14 disposed in the chamber 4 and meshing at diam'etric' ally opposite points with the pinions 10, so
that all of the valves will be driven simultaneously. The open sides of the chambers in the casing are closed by front and rear heads 15 and 16 and these heads are provided with bearings 17 in which the ends of the pimon shafts rotate and also with central bearings for the main shaft 12.
In the present instance, two sets or pairs of valves 9 are em loyed and are arranged on two right-angular y disposed diagonal lines, and each-valve is provided with three cavities or cups 19 arranged at one hundred and twenty degrees apart, and into these cavities engage projections or abutments 20 extending radiallyfrom the piston or drum 11 and arranged seventy-two degrees apart. In other words, the piston is provided'with one more abutment than there are number of valves, when each valve is lpqrovided w1th three cavities or oekets. e drum is of smaller diameter t an the chamber 3 so that the segmental spaces between each pair of adjacent abutments forms working or explosion chambers and the peripheral surfaces of the valves are adapted to contact with the peripheral surface of the piston between the abutments and the abutments engage with the circular surfaces of the pockets or cavities 19, the valves and pistons meshing after the fashion of gear wheel and pinions. The flat surfaces of the valves are provided with packing members 21 that bear on the flat surfaces of the compartments 5 so that leakage of the working fluid will be revented. The piston 11 is provided with pac 'ng members 22 set into the ends thereof to bear against the internal fiat walls of the chamber 3 for the purpose of preventing leakage and the projections or abutments 20 have packing strips 23 extending radially at the sides thereof and packing strips 24 as shown in Fig. 4, that extend along the crests of the said abutments so as to contact with the internal circular surface of the chamber 3. Disposed two opposite valves are admission and exhaust ports 25 and 26 respectively, which communicate with a the segmental working chambers or spaces between adjacent abutments. The exhaust ports are located on the approach side of the adjacent valves, while the admission ports are located on the leaving side'of the said valves so that as an abutment approaches one of such valves, the spent gases behind the abutment will be forced out through the exhaust port until the said abutment meshes with the valve While a charge of explosive mixture will be admitted between the preceding abutmerit and valve so that as the piston rotates, the admitted charge will be compressed by the first-mentioned abutment and succeeding valve. Adjacent the leaving side of each of the other valves are s ark plugs 27 for the purpose of igniting the charges after the same have been compressed.
In practice, the engine may be started by hand or in any other suitable manner, and by rotating the piston, a charge of mixture will be compressed in one of the other of the valves and immediately fired so that an impulse will be given to the piston which will be sufiicient to set the engine into operation. As shown in Fig. 2, a charge of mixture is partially compressed in the space designated a, while a charge has been exploded in the space I) and the exploded gases are operating on the abutment c. This forces the piston around in a clockwise direction and the exhaust gases in the space (1 on the opposite slde of the abutment c are being discharged through the lowermost exhaust port 26. In the space e, a charge has been admitted and the compression thereof begun, while in the pocket f of the left hand valve, a charge is ully compressed and one of the abutments eaaeai of the piston meshing in the said pocket'so as to hold the charge compressed, and as soon as the piston moves sufficiently to throw the said abutment out of the pocket, explosion is produced by the s arking plug 27 so as to impart another impu se to the piston and the spent gases in the space g will be forced out through the uppermost exhaust port 26. In this manner, two impulses are given to each abutment during one revolution, making thereby ten impulses to the piston which insures an even and steady torque. The engine has the advantage of simplicity of construction and a minimum number of parts and effectiveness of operation.
The structure of the engine is such that it may be used as a compressor. The ignition device is dispensed with and power applied to the shaft so as to rotate the piston, thereby drawing fluid into the casing and causing it to be delivered under pressure.
From the foregoing description, taken in connection with the accompanying drawings, the advantages of the construction and of the method of operation will be readily apparent to those skilled in the art to which the invention appertains, and while I have described the principle of operation of the invention, together with the apparatus which I now consider to be the best embodiment thereof, I desire to have it understood that the ap aratus shown is merely illustrative and t at such changes may be made when desired as are within the scope of the claims.
Having thus described the invention, what I claim is In an engine, the combination of a casing, heads therefor, a single partition between the heads and provided with a central bearing opening and additional bearing openings spaced around the central one, there being bearing openings in the heads alining with those of the partition, said partition dividing the easing into a piston compartment and a gearing compartment, a shaft mounted in the central bearing openings, a rotary piston secured to the shaft and provided with radial tooth-shaped abutments, a plurality of valve chambers formed in the casing and equally spaced around and communicating with the piston chamber, rotary valves in the valve chambers each valve being provided with a plurality of approximately semi circular pockets into which the tooth-shaped abutments of the piston are adapted to enter, admission and exhaust ports arranged in one of the heads and located at opposite sides of a line passing through the center of the iston and the valves disposed at diametricall opposite points whereby the valves and abutments cooperate to discharge the products of combustion through the exhaust port and draw in a mixture charge through the admiss1on port, an ignition device'located imme-= diately adjacent and on the leaving side of the other valve for firing the compressed charge between such valve and the approximate piston abutment, shafts secured to the valve and extending through the bearing openings of the partition, pinions on the valve shafts, and a gear wheel on the central shaft meshing with the pinions for positively rotating the said valves.
In testimony whereof We affix our signa- 10 tures in presence of two Witnesses.
CECIL C. COFFEY. TONY PFENNIGHAUSEN. ELVIN A. ROBINSON.
Witnesses:
ARTHUR C. ALLEN, TED F. MALTBRO.
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742882A (en) * 1951-02-27 1956-04-24 Leo F Porter Rotary-turbine-explosion type engine
US2856120A (en) * 1954-10-16 1958-10-14 Fawzi Mohamed Ibrahim Rotary piston machine, especially for use as a compressor
US2920814A (en) * 1956-12-28 1960-01-12 Inst Francais Du Petrole Rotary compressor system
US3096745A (en) * 1956-07-09 1963-07-09 Standish F Thompson Rotary engine
US3203406A (en) * 1960-11-28 1965-08-31 Dettwiler Georges Rotary engine
US3498271A (en) * 1968-03-18 1970-03-03 Dale F Marean Rotary engine
US3852001A (en) * 1973-04-26 1974-12-03 Pollard R Fluid translator
DE2710301A1 (en) * 1976-03-11 1977-09-15 Cherng Yi Su COMBUSTION ENGINE
WO2003095799A1 (en) * 2002-05-06 2003-11-20 Lurtz Jerome R Non-eccentric devices
WO2004067916A1 (en) * 2003-01-31 2004-08-12 Julian Zhen Chuan Kang Rotary machine with major and satellite rotors
US20070172375A1 (en) * 2002-05-06 2007-07-26 Lurtz Jerome R Non-eccentric devices
US20090229787A1 (en) * 2002-05-06 2009-09-17 Jerome Lurtz Generator using gravitational and geothermal energy
CN104100302A (en) * 2013-04-11 2014-10-15 刘千省 Rotor steam turbine
CN106812552A (en) * 2015-11-30 2017-06-09 熵零股份有限公司 Angular momentum engine

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2742882A (en) * 1951-02-27 1956-04-24 Leo F Porter Rotary-turbine-explosion type engine
US2856120A (en) * 1954-10-16 1958-10-14 Fawzi Mohamed Ibrahim Rotary piston machine, especially for use as a compressor
US3096745A (en) * 1956-07-09 1963-07-09 Standish F Thompson Rotary engine
US2920814A (en) * 1956-12-28 1960-01-12 Inst Francais Du Petrole Rotary compressor system
US3203406A (en) * 1960-11-28 1965-08-31 Dettwiler Georges Rotary engine
US3498271A (en) * 1968-03-18 1970-03-03 Dale F Marean Rotary engine
US3852001A (en) * 1973-04-26 1974-12-03 Pollard R Fluid translator
DE2710301A1 (en) * 1976-03-11 1977-09-15 Cherng Yi Su COMBUSTION ENGINE
US4057035A (en) * 1976-03-11 1977-11-08 Cherng Yi Su Internal combustion engines
US20030215346A1 (en) * 2002-05-06 2003-11-20 Lurtz Jerome R. Non-eccentric devices
WO2003095799A1 (en) * 2002-05-06 2003-11-20 Lurtz Jerome R Non-eccentric devices
US20060120910A1 (en) * 2002-05-06 2006-06-08 Lurtz Jerome R Non-eccentric devices
US20070172375A1 (en) * 2002-05-06 2007-07-26 Lurtz Jerome R Non-eccentric devices
US20090229787A1 (en) * 2002-05-06 2009-09-17 Jerome Lurtz Generator using gravitational and geothermal energy
US7841082B2 (en) 2002-05-06 2010-11-30 Lurtz Jerome R Non-eccentric devices
US8291722B2 (en) 2002-05-06 2012-10-23 Lurtz Jerome R Generator using gravitational and geothermal energy
WO2004067916A1 (en) * 2003-01-31 2004-08-12 Julian Zhen Chuan Kang Rotary machine with major and satellite rotors
US20070119408A1 (en) * 2003-01-31 2007-05-31 Kang Julian Z C Rotary machine with major and satellite rotors
CN104100302A (en) * 2013-04-11 2014-10-15 刘千省 Rotor steam turbine
CN104100302B (en) * 2013-04-11 2016-12-07 刘千省 Turbine
CN106812552A (en) * 2015-11-30 2017-06-09 熵零股份有限公司 Angular momentum engine

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