US1828228A - Gas engine - Google Patents

Gas engine Download PDF

Info

Publication number
US1828228A
US1828228A US1828228DA US1828228A US 1828228 A US1828228 A US 1828228A US 1828228D A US1828228D A US 1828228DA US 1828228 A US1828228 A US 1828228A
Authority
US
United States
Prior art keywords
rotor
piston
casing
gas
cam
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
Publication date
Application granted granted Critical
Publication of US1828228A publication Critical patent/US1828228A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2730/00Internal combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01Internal combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • F02B2730/011Internal combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the housing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • This invention relates to internalcombustion engines of the rotary type.
  • One of the objects of-this invention is to v assure a continuous functioning in the different steps during the rotating of a gas-engine including intake, compression, explosion and exhaust.
  • Another object is to provide a rotor which may be acted upon on its periphery by which 1 the rotor can be caused to rotate.
  • Another object is to provide a compressor, cylinder and piston in radial relation to the rotor, including means by which compressed gas can be transferred to the periphery of the rotor where it may be caused to set the rotor in motion.
  • Another object is to provide a rotor with a spiral cam, whereby the gas-compressing mechanism may be operated.
  • FIG. 1 is a fragmentary cross section through a cylinder enclosing a rotor and a compressing mechanism in radial relation to the rotor, the compressing piston being shown in the innermost position in"the rotor cam, in which position gas may be brought to explodeto act upon the cam of the rotor between the cam and the piston.
  • Fig. 2 is a similar view as Fig. 1, in whic the piston is shown in its compressing position within the compressing cylinder, the cam of the rotor being below the piston and the overfiow and communicating. channel connecting a space above the piston with a space below and sidewise of the piston, by which compressed gasis partly transferred from the space abo e to the space below and sidewise of the piston, poaratory to being discharged upon the cam of the 1 tor.
  • Fig. 3 is a similar illustration as Figs. 1 and 2 with the compressingrpiston ust forced into the cam of the rotor to the point of shutting off the overflow channel at which moment explosion may occur in the space below and sidewise of the piston to act upon'the cam of the rotor.
  • FIG. 4 is a fragmentary side elevation of a complete rotary motor, illustrating the feature of having several rotors within a single housing with a common manifold for the gas intake of the several rotors and another common manifold for the exhaust of the several rotors.
  • Fig. 5 is a diagrammatic end elevation to illustrate the difierent positions of rotor cams in relation to one another in the manner of which the intake and outlet manifolds of a motor can be arranged straight across several rotors in a common housing in the manner illustrated in Fig. 4 and whereby a successive operation of several motors may be accomplished.
  • Fig. 6 is a slightly modified form of a gas control forthe rotor including a valve controlled gas supply, whereby gas compressed by a separate'machinery,not shown in the drawings, can be injected into the housing to act upon the rotor instead of having indiclose enough to the point of explosion in relation to the rotor.
  • the rotor 7 is mounted in a housing 8. 8
  • a compression cylinder 9 is arranged in radial relation to the rotor 7.
  • a piston 10 is shiftable within the compres-' further illustration that means of various forms are known, in which cams can be made to positively move a cooperating member back and forth, so that in this case the compression piston 10 may be engaged with the cam in any well-known manner. No particular means is claimed or illustrated for this reason, but merely the spring 34 to make it known that the piston can be broughtdown.
  • a circular casing a compression chamber extending radially from said casing and having a valve control-led gas inlet in its outer end, the walls of the compression chamber having a gas passage formed therein with its ends opening into the inner and outer end portions of the chamber, a rotor rotatably mounted in said casing and formed with a substantially radially extending face and having its edge face constituting a cam surface intersecting the ends of the radially extending face, a piston slidable in said compression chamber and extending into said casing and resting upon the edge face of said rotor, said piston having a recess in its lower end moved into and out of communication with the lower end of said gas passage during reciprocation of the piston and disposed opposite the radial face of the rotor when the piston is in a lowered position, and spark forming means to explode a charge of gas between the piston and radial face of the rotor.
  • a casing a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a. rotor in 'said casing having a circumferentially extending cam surface and a shoulder joining ends of the cam surface, a piston slidable longitudinally in said cylinder into and out of said casing and at its inner end bearing against the cam surface of said rotor, the cylinder having a fuel passage opening into its outer and inner ends, said piston having movement across the inner end of the fuel passage and formed to define a.
  • a casing a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a'rotor in said casing having a circumferentially extending cam surface and a shoulder joining ends of the cam surface, a piston slid-able longitudinally in said cylinder into and out of said casing, and at its inner end bearing against the cam surface of said rotor, the cylinder having a fuel passage opening into its outer and inner ends, said piston having movement across the inner end of the fuel passage and formed to define a pocket to be filled with compressed fuel forced through the passage by the piston when the inner end of the fuel passage is uncovered as the piston moves outwardly, and means to explode fuel carried into the casing with the piston, a
  • a casing In an internal combustion engine, a casing, a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a rotor in passage and formed to define a pocket to be CLARENCE w. KEMPTON.

Description

' Patented Oct; 20,1931
UNITED STATES CLARENCE W. KEMPTON, OF LOS ANGIE-LES, CALIFORNIA GAS ENGINE Application filed August 8, 1927, Serial No. 211,514. Renewed March 18, 1981.
This invention relates to internalcombustion engines of the rotary type.
One of the objects of-this invention is to v assure a continuous functioning in the different steps during the rotating of a gas-engine including intake, compression, explosion and exhaust. I
Another object is to provide a rotor which may be acted upon on its periphery by which 1 the rotor can be caused to rotate.
Another object is to provide a compressor, cylinder and piston in radial relation to the rotor, including means by which compressed gas can be transferred to the periphery of the rotor where it may be caused to set the rotor in motion.
Another object is to provide a rotor with a spiral cam, whereby the gas-compressing mechanism may be operated.
Other objects will appear from the following description and appended claims as well as from the accompanying drawings, in which Fig. 1 is a fragmentary cross section through a cylinder enclosing a rotor and a compressing mechanism in radial relation to the rotor, the compressing piston being shown in the innermost position in"the rotor cam, in which position gas may be brought to explodeto act upon the cam of the rotor between the cam and the piston.
Fig. 2 is a similar view as Fig. 1, in whic the piston is shown in its compressing position within the compressing cylinder, the cam of the rotor being below the piston and the overfiow and communicating. channel connecting a space above the piston with a space below and sidewise of the piston, by which compressed gasis partly transferred from the space abo e to the space below and sidewise of the piston, poaratory to being discharged upon the cam of the 1 tor.
Fig. 3 is a similar illustration as Figs. 1 and 2 with the compressingrpiston ust forced into the cam of the rotor to the point of shutting off the overflow channel at which moment explosion may occur in the space below and sidewise of the piston to act upon'the cam of the rotor.
50 Fig. 4 is a fragmentary side elevation of a complete rotary motor, illustrating the feature of having several rotors within a single housing with a common manifold for the gas intake of the several rotors and another common manifold for the exhaust of the several rotors. v
Fig. 5 is a diagrammatic end elevation to illustrate the difierent positions of rotor cams in relation to one another in the manner of which the intake and outlet manifolds of a motor can be arranged straight across several rotors in a common housing in the manner illustrated in Fig. 4 and whereby a successive operation of several motors may be accomplished. Fig. 6 is a slightly modified form of a gas control forthe rotor including a valve controlled gas supply, whereby gas compressed by a separate'machinery,not shown in the drawings, can be injected into the housing to act upon the rotor instead of having indiclose enough to the point of explosion in relation to the rotor.
As illustrated in Fig. 1 of the drawings, the rotor 7 is mounted in a housing 8. 8 A compression cylinder 9 is arranged in radial relation to the rotor 7.
" A piston 10 is shiftable within the compres-' further illustration that means of various forms are known, in which cams can be made to positively move a cooperating member back and forth, so that in this case the compression piston 10 may be engaged with the cam in any well-known manner. No particular means is claimed or illustrated for this reason, but merely the spring 34 to make it known that the piston can be broughtdown.
Having thus described my invention, I claim:
1. In an internal combustion engine, a circular casing, a compression chamber extending radially from said casing and having a valve control-led gas inlet in its outer end, the walls of the compression chamber having a gas passage formed therein with its ends opening into the inner and outer end portions of the chamber, a rotor rotatably mounted in said casing and formed with a substantially radially extending face and having its edge face constituting a cam surface intersecting the ends of the radially extending face, a piston slidable in said compression chamber and extending into said casing and resting upon the edge face of said rotor, said piston having a recess in its lower end moved into and out of communication with the lower end of said gas passage during reciprocation of the piston and disposed opposite the radial face of the rotor when the piston is in a lowered position, and spark forming means to explode a charge of gas between the piston and radial face of the rotor.
2. In an internal combustion engine, a casing, a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a. rotor in 'said casing having a circumferentially extending cam surface and a shoulder joining ends of the cam surface, a piston slidable longitudinally in said cylinder into and out of said casing and at its inner end bearing against the cam surface of said rotor, the cylinder having a fuel passage opening into its outer and inner ends, said piston having movement across the inner end of the fuel passage and formed to define a. pocket to be filled with compressed fuel forced through the passage by the piston when the inner end of the fuel passage is uncovered as the piston moves outwardly, and means to explode fuel carried into the casing with the piston whereby the fuel will expand between the piston and shoulder of the rotor and impart rotary motion to the rotor.
3. In an internal combustion engine, a casing, a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a'rotor in said casing having a circumferentially extending cam surface and a shoulder joining ends of the cam surface, a piston slid-able longitudinally in said cylinder into and out of said casing, and at its inner end bearing against the cam surface of said rotor, the cylinder having a fuel passage opening into its outer and inner ends, said piston having movement across the inner end of the fuel passage and formed to define a pocket to be filled with compressed fuel forced through the passage by the piston when the inner end of the fuel passage is uncovered as the piston moves outwardly, and means to explode fuel carried into the casing with the piston, a
link extending transversely of the piston with one end pivoted to the piston and its other end pivoted to the casing, and resilient means acting upon said link to urge the piston toward the rotor.
4. In an internal combustion engine, a casing, a cylinder having a valve controlled fuel inlet and having its inner end open and communicating with said casing, a rotor in passage and formed to define a pocket to be CLARENCE w. KEMPTON.
Oct. 20, 1931. G. c. MARSH 1,828,229
FEEDING MOLTEN GLASS Filed July 18, 1928 2 Sheets-Sheet 1 INVENTOR Wow BY W
US1828228D Gas engine Expired - Lifetime US1828228A (en)

Publications (1)

Publication Number Publication Date
US1828228A true US1828228A (en) 1931-10-20

Family

ID=3422733

Family Applications (1)

Application Number Title Priority Date Filing Date
US1828228D Expired - Lifetime US1828228A (en) Gas engine

Country Status (1)

Country Link
US (1) US1828228A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938505A (en) * 1958-04-30 1960-05-31 Harry C Quartier Annularly spaced oscillating piston engine
US3118432A (en) * 1960-08-05 1964-01-21 Horace Tomasello Rotary internal combustion engine
US3204616A (en) * 1963-01-10 1965-09-07 Harold G Eastman Rotor engine
US4715338A (en) * 1986-12-30 1987-12-29 Pasquan Raymond F Rotary engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938505A (en) * 1958-04-30 1960-05-31 Harry C Quartier Annularly spaced oscillating piston engine
US3118432A (en) * 1960-08-05 1964-01-21 Horace Tomasello Rotary internal combustion engine
US3204616A (en) * 1963-01-10 1965-09-07 Harold G Eastman Rotor engine
US4715338A (en) * 1986-12-30 1987-12-29 Pasquan Raymond F Rotary engine

Similar Documents

Publication Publication Date Title
US2158532A (en) Complementary rotary engine
US2966898A (en) Rotary piston internal combustion engine
US3244153A (en) Rotary combustion engine
US1828228A (en) Gas engine
US2766737A (en) Injection valve for rotary type internal combustion engine
US2062753A (en) Rotary gasoline engine
US3220388A (en) Rotary internal combustion engine
US3692002A (en) Rotary internal combustion engine
US3056391A (en) Rotary internal combustion engine
US3251348A (en) Rotary piston engine
US5946903A (en) Internal combustion engine having a separate rotary combustion chamber
US3882827A (en) Four-phase cycle planetating piston internal combustion engine
US2812748A (en) Rotary internal combustion engine
US2473785A (en) Rotary combustion motor
US1369070A (en) Rotary internal-combustion engine
US3823694A (en) Rotary piston engine having alternately used external combustion chambers
US20140190446A1 (en) Fixed vane rotary abutment engine
US2280742A (en) Rotary internal combustion engine
US2127016A (en) Internal combustion engine
US2215232A (en) Rotary internal combustion engine
US1184114A (en) Rotary engine.
US3176664A (en) Internal combustion rotary engine
US4337741A (en) Rotary internal combustion engine
US2904019A (en) Rotary internal combustion engine
US3848575A (en) Sliding vane rotary combustion engine