Nothing Special   »   [go: up one dir, main page]

US1482628A - Rotary engine - Google Patents

Rotary engine Download PDF

Info

Publication number
US1482628A
US1482628A US278880A US27888019A US1482628A US 1482628 A US1482628 A US 1482628A US 278880 A US278880 A US 278880A US 27888019 A US27888019 A US 27888019A US 1482628 A US1482628 A US 1482628A
Authority
US
United States
Prior art keywords
piston
pistons
casing
gear
gears
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
US278880A
Inventor
Frank A Bullington
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US278880A priority Critical patent/US1482628A/en
Application granted granted Critical
Publication of US1482628A publication Critical patent/US1482628A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/02Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F01C1/063Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them
    • F01C1/077Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them having toothed-gearing type drive

Definitions

  • y invention relates to rotary engines 10 of the general type shown and described in my pending application, filed June 17, 1918,
  • the present invention has as its principal object to improve and simplify the engine casing, the form of to piston, the operating connections between the pistons, the ignition means, and the pressure sealing means.
  • the to pistons have a continuous rotary motion within the piston casing, as distinguished from engines in which the pistons have an intermittent stopping functon just preceding or simultaneously with the explosions.
  • Figure 1 is a vertical longitudinal sectional view through an engine embodying my improvements, taken on line 1-1 of F1 5.
  • igure 2 is a vertical sectional view through the piston casing, taken on line 2-2 of Fig. 1, with pistons shown in side elevation; v
  • Figure 3 is a horizontal longitudinal sectional view taken on line 3-3 of 1* igs. and d;
  • Figure 1 is a. vertical sectional view taken on line 1- 3: of Figs. 1 and 3;
  • Figure 5 is a diagrammatic view showing the pistons in the positions indicated in Fig. 2 and also showing the relative positions of the operative connecting gears, shown in Fig. d;
  • igure 6 is a similar view showing the pistons and the operating connecting gears in an advanced position
  • Figures 7 and 8 show the operating connecting gears in difierent positions when the difiere-nt pistons of the group occupy the same positions as shown in Figs. 5 and 6, respectively 2 or passageways 1.
  • Figure 8 is a detail view showing a modified construction of mechanism illustrated in Fig. 4;
  • Figure 9 is a detail view of one pair of pistons, one piston being shown in section, and the other in side elevation;
  • Figure 10 is a detail section through one piston on line 1010 of Fig. 9;
  • Figure 11 is a detail sectional view through one of the pistons on line 1111 of Fig. 9, showing my improved sealing means in position;
  • Figure 12 is a fragmentary bottom plan view of the piston shown in Fig. 11;
  • Figure 13 is a fragmentary side elevation of the end of the piston shown in Fig. 11;
  • Figure 14 is a side elevation of my improved sealing means between the casing and the sides of the piston lips.
  • myinvention as here shown for purposes of description, comprises a piston casing 1, shown in two parts, designated 1 and 1", the parts of which are connected by meansof suitable bolts 2, and interlocking pins 3, thus constituting an interlocked joint horizontally through said casing.
  • my improved piston casin is of semi circular form as to that part in which the pistons move, as will be clearly understood from Fig. 1, in which 1 designatesthe piston casing wall and 1 designates an outer wall, between which are crescent-shaped re enforcement ribs 1.
  • the spaces between said ribs constitute cooling chambers communicating with each other through the ports Any suitable cooling fluid can be supplied through a pipe 4:, with an outlet pipe at 5.
  • Said piston casing is provided with a plurality of intake ports 6, communicating with a main inlet 7.
  • Said piston casing is also provided with similar exhaust ports 8, communicating with a main exhaust 9.
  • Said casing is also provided with auxiliary ports 10, cooperating with an air supply port 11, with which communicates an air supply pipe 12, connected at its other end with a blower casing 13, from which air is supplied under pressure.
  • Said piston casing 1 is open at the side, I
  • each piston comprises a piston vane 20*, a piston body 20 at one side thereof, and a piston lip 20 projectmg in the op osite direction from the other side thereof.
  • istons 20 and 20 have their vanes secured to a hub 20, reenforced with webs 20 which extend into the piston bodies to reenforce the same.
  • the hub 20 of the pistons 20 and 20 is extended into a sleeve 20 provided at its outer end with an elliptical gear 21.
  • the pistons 19 and 19' are the same 111 structure as pistons 20 and 20' with the exception that the have no sleeve extension of their hub 19".
  • Tistons 19 and 19 are secured to the shaft 17 by means of keys 22.
  • the piston vanes are arranged in crossed, overlapping or interlocking relationship to each other at their hub portions.
  • one piston body overlaps the piston lip of the next ad'acent piston, whereby said piston lip forms t e inner wall of a chamber between the end of the piston body, or the piston head, and the opposite end or vane of the next adjacent piston.
  • Said pistons are provided at their piston vane ends with sealing members 23 and at their head ends with sealing members 24 and 25. Sealing members 23 and 24 are similar as to their curved or ring portions. as indicated in Fig.
  • the piston casing is provided at its opposite sides with annular extensions or enlargements 1*, for the puraaaaeaa pose of providing annular recesses 30 between the sides of the piston lips and the piston casing in which recesses are placed specially formed, split sealing rings 31 and 32, each of said rings comprising two parts, a bearing ring 31 and 32,- and a pressure ring 31 and 32.
  • Bearing ring 31 bears against the side of the piston lip 19 and also against the wall of the piston casing.
  • the pressure ring 31' bears against the side wall of the piston casing and against the beveled side of the bearing ring 31 in such manner as to force said bearing ring inwardly and outwardly.
  • Bearing ring 32 also bears against the side of the piston lip 19 and against the inner surface of bearing ring 31, reenforcing said ring 31.
  • Ring 32 bears against the beveled side of the ring 32 arid againstthe side of the piston casing.
  • the four parts of said rings are connected together by means of pins 33, for the purpose of interlocking them so that they will turn together, said members together constituting in effect a floatin sealing rin turning with the piston lips nu at a reduced speed because of their bearing against the sides of the piston casing.
  • piston heads are semi-circular in cross section, and that the sealing means is therefore more eflicient than it could be if the pistons were square or rectangular in cross section, requiring four angularjoints instead of two, as here shown.
  • a circular gear 35 Secured to the main shaft 17, %y means of a key 34, is a circular gear 35.
  • a counter shaft 36 having keyed thereto elliptical and circular gears 37 and 38.
  • the elliptical gear 37 meshes with the elliptical gear 21 on the sleeve
  • the circular gear 38 meshes with the circular gear 35, on the shaft.
  • the rotation of the main shaft 17 and the rotation of the counter shaft 36 are uniform in opposite directions by reason of the circular gears 35 and 38, connect ing the same, while the rotation of the sleeve 20' and the counter shaft 36 are variable to each other by reason of the action of the elliptical gears 21 and 37.
  • This provides for the variable movement of the pistons carried by the shaft and the pistons carried by the sleeve with relation to each other.
  • a driving gear 39 for drivin auxiliary mechanism mounted on the outer end of the counter shaft 36 .
  • a vane or blower 40 mounted incense inthe fan or blower casing 13, on the main shaft 17, is a vane or blower 40, for forcing air through the air conduit 12, leading to the piston casing 1, for forcing air through saidcasing .and across the path of the pistons, for the purpose of scavenging the chambers formed between the istons.
  • Said main shaft 17 is also provide at its outer end with a pin 41, for hand startin crank, not shown; The opposite end o said main shaft is extended for any desired driving connections.
  • a spark plug 42 is set in an i ition c amber 43, formed in the iston casing, and communicating with the interior of the piston casing through a relatively small port'44.
  • the reason for connectingsuch an ignition chamber with the piston casing by' means of a small port is to minimize the undersirable effect of the pressure resulting from combustion and exerted upon the sealing means of the pistons when passing the ignition chamber.
  • gear 21 has its long diameter perendicular to the long diameter of gear 37 and in these positions the gear 37 is rotating at a greater rate of speed relatively than the gear 21.
  • a chamber C is shown as just completing an intake of explosive mixture about to be compressed. At C a charge is shown compressed and in register with the ignition port 44.
  • di erent chambers are enlarged and contracted as they move around their course with the continuously moving pistons, the varying relative movements of which cause such expansion and contraction of the chambers, all properly timed to briiig about the proper intake, compression, ex ansion and exhaust actions.
  • Fig. 8 I have shown a modified construction of mechanism for accomplishing the relative movements of the main'shaft 17 and the sleeve 20.
  • said gears are spaced apart and are connected by means .of gear chains.
  • the elliptical gears are designated 21 and 37 and their connecting chain is designated 50.
  • the circular gears, indicated in broken lines, are designated 35 and 38 and their connecting chain isdesignated 51.
  • a piston casing having a piston chamber therein of semicircular form in cross section, and crescentshaped reinforcing ribs projecting from the outer surface of the casing, the ribs being progressively narrower from the center toward each end whereby the maximum strength and cooling area will be efiective in the middle portions of the ribs.
  • a piston casing having a. piston chamber therein of semicircular form in cross section, ,,and reinuse forced on its outer surface with radially dist Signed at Portland, Multnomah County,

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Motors (AREA)

Description

Feb 5, 19240 F. A. BULLINGTON ROTARY ENGINE .-Filed Feb. 24 1919 4 Sheets-Sheet 1 TTORIVMS/V If INVENTOR Feb. 5, 19240 Ilfi$228 F. A. BULLINGTON ROTARY ENGINE Filed Feb. 24 1919 4 Sheets$haet 2 Feb. 5, 1924.
F. A. BULLING'YON ROTARY ENGINE Filed Feb. 24 1919 4 Sheets-ShGQt 3 Feb. 5, 1924. mafiz F. A. BULLINGTON ROTARY ENGI NE Filed Fe 24. 1919 4 Shee'ts-Shee.t 4'
A TTORN patented Feb. d,
FRANK A. BULLIINGTON, (31F PQETLAND, OREGUN.
ROTARY ENGXNE.
Application filed February 24, 1919. Elerial No. 278,880.
To all whom it may concem:
Be it mown that I, FRANK A. BULLING- row, a citizen of the United States, residing in the city of Portland, county of Multnos mah, and State of Oregon, have invented certain new and useful Improvements in R0- tary Engines, of which the following is a specification.
y invention relates to rotary engines 10 of the general type shown and described in my pending application, filed June 17, 1918,
Serial Number 240,443. The present invention has as its principal object to improve and simplify the engine casing, the form of to piston, the operating connections between the pistons, the ignition means, and the pressure sealing means. In my improved engine as disclosed inmy former application, above referred to, and also in this application, the to pistons have a continuous rotary motion within the piston casing, as distinguished from engines in which the pistons have an intermittent stopping functon just preceding or simultaneously with the explosions.
In order to more clearly explain my invention, l have shown one form thereof on the accompanying sheets of drawings, which 1 will now describe:
Figure 1 is a vertical longitudinal sectional view through an engine embodying my improvements, taken on line 1-1 of F1 5. 2 and 4:;
igure 2 is a vertical sectional view through the piston casing, taken on line 2-2 of Fig. 1, with pistons shown in side elevation; v
Figure 3 is a horizontal longitudinal sectional view taken on line 3-3 of 1* igs. and d;
Figure 1 is a. vertical sectional view taken on line 1- 3: of Figs. 1 and 3;
Figure 5 is a diagrammatic view showing the pistons in the positions indicated in Fig. 2 and also showing the relative positions of the operative connecting gears, shown in Fig. d;
igure 6 is a similar view showing the pistons and the operating connecting gears in an advanced position;
Figures 7 and 8 show the operating connecting gears in difierent positions when the difiere-nt pistons of the group occupy the same positions as shown in Figs. 5 and 6, respectively 2 or passageways 1.
Figure 8 is a detail view showing a modified construction of mechanism illustrated in Fig. 4;
Figure 9 is a detail view of one pair of pistons, one piston being shown in section, and the other in side elevation;
Figure 10 is a detail section through one piston on line 1010 of Fig. 9;
Figure 11 is a detail sectional view through one of the pistons on line 1111 of Fig. 9, showing my improved sealing means in position;
Figure 12 is a fragmentary bottom plan view of the piston shown in Fig. 11;
Figure 13 is a fragmentary side elevation of the end of the piston shown in Fig. 11;
and
Figure 14 is a side elevation of my improved sealing means between the casing and the sides of the piston lips.
Referring now in detail to the drawings, myinvention as here shown for purposes of description, comprises a piston casing 1, shown in two parts, designated 1 and 1", the parts of which are connected by meansof suitable bolts 2, and interlocking pins 3, thus constituting an interlocked joint horizontally through said casing. In transverse section my improved piston casin is of semi circular form as to that part in which the pistons move, as will be clearly understood from Fig. 1, in which 1 designatesthe piston casing wall and 1 designates an outer wall, between which are crescent-shaped re enforcement ribs 1. The spaces between said ribs constitute cooling chambers communicating with each other through the ports Any suitable cooling fluid can be supplied through a pipe 4:, with an outlet pipe at 5. Said piston casing is provided with a plurality of intake ports 6, communicating with a main inlet 7. Said piston casing is also provided with similar exhaust ports 8, communicating with a main exhaust 9. Said casing is also provided with auxiliary ports 10, cooperating with an air supply port 11, with which communicates an air supply pipe 12, connected at its other end with a blower casing 13, from which air is supplied under pressure.
Said piston casing 1 is open at the side, I
as'at 14, with acombination closure and bearing plate or member 14. At its opposite side said casing has a bearing 15. Connected with said piston casing 1 is a gear casing 16, with which latter is also connected a blower casing 13, above referred to. Mounted through said casings is a main shaft 17, provided with a fly wheel 18. Mounted on said main shaft 17, within the piston casing 1, are two sets of pistons desi nated, respectively, 19, 19' and 20, 20'.
eferring particularly to Figs. 9 and 10, in which pistons 20, 20 are shown in detail, it will be seen that each piston comprises a piston vane 20*, a piston body 20 at one side thereof, and a piston lip 20 projectmg in the op osite direction from the other side thereof. istons 20 and 20 have their vanes secured to a hub 20, reenforced with webs 20 which extend into the piston bodies to reenforce the same. The hub 20 of the pistons 20 and 20 is extended into a sleeve 20 provided at its outer end with an elliptical gear 21. The pistons 19 and 19' are the same 111 structure as pistons 20 and 20' with the exception that the have no sleeve extension of their hub 19". Tistons 19 and 19 are secured to the shaft 17 by means of keys 22. Referring to Figs. 1, 2 and 3, it will be seen that the piston vanes are arranged in crossed, overlapping or interlocking relationship to each other at their hub portions. It will also be noted by reference to Fig. 2 that one piston body overlaps the piston lip of the next ad'acent piston, whereby said piston lip forms t e inner wall of a chamber between the end of the piston body, or the piston head, and the opposite end or vane of the next adjacent piston. Said pistons are provided at their piston vane ends with sealing members 23 and at their head ends with sealing members 24 and 25. Sealing members 23 and 24 are similar as to their curved or ring portions. as indicated in Fig. 11, and comprise ring-like members held yieldingly against the casing wall 1 by means of springs 26 and 27. Springs 2t}, as shown in Figs. 9 and 11, are sim ly straight pressure springs. Referring to ig. 11, sealing meml'er 24 has an overlapping or interfitting conrection with the strai ht sealing member 25, the overlapping joint eing clearly indicated in Figs. 11, 12 and 13. This straight sealin member 25 is rovided for sealing the joint between the piston body and the piston lip of an ad'acent piston, as will be understood from ll ig. 2 in connection with piston 20 and piston lip 19. Springs 27, Fig. 11, bear against wedge blocks 28, which fit into the angle between the ends of the sealing members 24 and 25, in such a way as to press both of said members outwardly against their bearing surfaces, and also to seal the openin 29 in the interfitting joints between the en of said members 24 and 25.
Referring to Fig. 11, the piston casing is provided at its opposite sides with annular extensions or enlargements 1*, for the puraaaaeaa pose of providing annular recesses 30 between the sides of the piston lips and the piston casing in which recesses are placed specially formed, split sealing rings 31 and 32, each of said rings comprising two parts, a bearing ring 31 and 32,- and a pressure ring 31 and 32. Bearing ring 31 bears against the side of the piston lip 19 and also against the wall of the piston casing. The pressure ring 31' bears against the side wall of the piston casing and against the beveled side of the bearing ring 31 in such manner as to force said bearing ring inwardly and outwardly. Bearing ring 32 also bears against the side of the piston lip 19 and against the inner surface of bearing ring 31, reenforcing said ring 31. Ring 32 bears against the beveled side of the ring 32 arid againstthe side of the piston casing. The four parts of said rings are connected together by means of pins 33, for the purpose of interlocking them so that they will turn together, said members together constituting in effect a floatin sealing rin turning with the piston lips nu at a reduced speed because of their bearing against the sides of the piston casing. It will thus be seen that the piston heads are semi-circular in cross section, and that the sealing means is therefore more eflicient than it could be if the pistons were square or rectangular in cross section, requiring four angularjoints instead of two, as here shown.
Referring now to Figs. 1, 3 and at, I will describe the operating connections between the pistons. Secured to the main shaft 17, %y means of a key 34, is a circular gear 35.
his gear is adjacent the elliptical gear 21. on the sleeve 20, on said shaft 17. Mounted in the gear casing 16 is a counter shaft 36. having keyed thereto elliptical and circular gears 37 and 38. The elliptical gear 37 meshes with the elliptical gear 21 on the sleeve, and the circular gear 38 meshes with the circular gear 35, on the shaft. Thus a connection is made between the pistons .19, 19' on the shaft and the pistons 20, 20 on the sleeve. The rotation of the main shaft 17 and the rotation of the counter shaft 36 are uniform in opposite directions by reason of the circular gears 35 and 38, connect ing the same, while the rotation of the sleeve 20' and the counter shaft 36 are variable to each other by reason of the action of the elliptical gears 21 and 37. This provides for the variable movement of the pistons carried by the shaft and the pistons carried by the sleeve with relation to each other. By reason of the inertia of the balance wheel 18, carried by the main shaft 17, the rotation of said shaft 17 and its pistons is made uniform.
Mounted on the outer end of the counter shaft 36 is a driving gear 39 for drivin auxiliary mechanism, as desired. Mounted incense inthe fan or blower casing 13, on the main shaft 17, is a vane or blower 40, for forcing air through the air conduit 12, leading to the piston casing 1, for forcing air through saidcasing .and across the path of the pistons, for the purpose of scavenging the chambers formed between the istons. Said main shaft 17 is also provide at its outer end with a pin 41, for hand startin crank, not shown; The opposite end o said main shaft is extended for any desired driving connections.
Referring to Fi 1, a spark plug 42 is set in an i ition c amber 43, formed in the iston casing, and communicating with the interior of the piston casing through a relatively small port'44. The reason for connectingsuch an ignition chamber with the piston casing by' means of a small port is to minimize the undersirable effect of the pressure resulting from combustion and exerted upon the sealing means of the pistons when passing the ignition chamber.
The use and operation of my invention may be briefly described as follows, refer-.
ring especially to Figs. 5, 6, 7 and 8:
Assuming that the pistons are in the positions shown in Fig. 5, and are moving in the direction indicated by the arrow, and with the elliptical gears in the relationship to each other as shown, it will be seen that their lon diameters are parallel with each other an that their engagement is on their mean diameters. In these positions they will,have amomentary uniform speed. Moving from these positions to the positions shown in Fig. 6, gear 21 has its long diameter perendicular to the long diameter of gear 37 and in these positions the gear 37 is rotating at a greater rate of speed relatively than the gear 21. Moving from these positions to the positions shown in Fig. 7 where the long diameters of the gears are again parallel to each other and their mean diameters are in engagement with each other, but at a different point, their movements are again momentarily uniform. In Fig. 8 they are shown to have advanced to positions opposite those shown in Fig. 6, and the gear 21 is rotating at a greater rate of speed relatively than gear 37 As these gear connections control the movements of the pistons, it will be understood that said pistons must have a corresponding movement. These movements of the pistons cause the chambers formed therebetween -to be alternately contracted and. enlarged for the performance of their functions. Referring to Fig. 5, a chamber C is shown as just completing an intake of explosive mixture about to be compressed. At C a charge is shown compressed and in register with the ignition port 44. At C an exhaust is commencing, and at C the exhaust is completed and a position is reached in register with the air port 11, receiving my special scavenging blast of air under pressure, preliminary to taking in another charge of explosive mixture prior to reaching the position C 11 Fig. 6 the pistons are shown in different advanced positions resulting in the chambers being shown as substantially uniform in size. Chamber C is shown in the act of compressing; chamber C in the act of expanding under explosion; chamber C in the act of exhausting the burnt charge, and chamber C in the act of drawing in the fresh char e.
Thus the di erent chambers are enlarged and contracted as they move around their course with the continuously moving pistons, the varying relative movements of which cause such expansion and contraction of the chambers, all properly timed to briiig about the proper intake, compression, ex ansion and exhaust actions.
eferring now to Fig. 8, I have shown a modified construction of mechanism for accomplishing the relative movements of the main'shaft 17 and the sleeve 20. Instead of having the gears mesh with each other direct, as. in Fig. 4., said gears are spaced apart and are connected by means .of gear chains. In this figure the elliptical gears are designated 21 and 37 and their connecting chain is designated 50. The circular gears, indicated in broken lines, are designated 35 and 38 and their connecting chain isdesignated 51. With these 'ars thus connected the counter shaft 36 and the main shaft 17 of course, rotate'in the same direction. This construction provides for a more extensive distribution or application of the power impulse from the explosions to the gears by reason of the chains bein at all times in connection with approx1- mately one half the teeth of their respective gears.
I am aware that changes can be made in the embodiment of my invention as here shown for illustrative purposes without departing from the spirit thereof, and I do not, therefore, limit my invention to the form of the invention here shown, except as I may be limited by the hereto appended claims.
I claim:
1. In a rotary engine, a piston casing having a piston chamber therein of semicircular form in cross section, and crescentshaped reinforcing ribs projecting from the outer surface of the casing, the ribs being progressively narrower from the center toward each end whereby the maximum strength and cooling area will be efiective in the middle portions of the ribs.
2. In a rotary engine, a piston casing having a. piston chamber therein of semicircular form in cross section, ,,and reinuse forced on its outer surface with radially dist Signed at Portland, Multnomah County,
posed, cteseent-shaped ribs, the ribs being Oregon, this 7th day of February, 1919.'
progresslvely narrower from the center toward the ends so that the widest portion is FRANK BULLINGTON' 5 in the middle, and an outer shell over said In presence of ribs to form a cooling chamber between the I. M. GRIFFIN,
ribs, the piston casing and the outer shell. W. R. LITZENBERG.
US278880A 1919-02-24 1919-02-24 Rotary engine Expired - Lifetime US1482628A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US278880A US1482628A (en) 1919-02-24 1919-02-24 Rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US278880A US1482628A (en) 1919-02-24 1919-02-24 Rotary engine

Publications (1)

Publication Number Publication Date
US1482628A true US1482628A (en) 1924-02-05

Family

ID=23066763

Family Applications (1)

Application Number Title Priority Date Filing Date
US278880A Expired - Lifetime US1482628A (en) 1919-02-24 1919-02-24 Rotary engine

Country Status (1)

Country Link
US (1) US1482628A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553954A (en) * 1948-10-22 1951-05-22 Bancroft Charles Rotary machine of the alternating piston type
US3302625A (en) * 1964-05-15 1967-02-07 Cunningham Kelly Gore Engine
US3769946A (en) * 1969-07-14 1973-11-06 W Scherrer Rotary engines
US4338067A (en) * 1980-02-14 1982-07-06 Greenfield Stuart T Alternating piston machine with rotating end walls and chain drive
EP0215194A1 (en) * 1985-09-09 1987-03-25 John E. Stauffer Rotary internal combustion engine
DE4315155A1 (en) * 1993-05-07 1994-11-10 Markus Rieck Rotary engine with periodically varying working chambers
WO1995017582A1 (en) * 1993-12-23 1995-06-29 Janosi Marcell Rotary motion drive, especially for internal combustion engines
US6739307B2 (en) 2002-03-26 2004-05-25 Ralph Gordon Morgado Internal combustion engine and method
FR2873401A1 (en) * 2004-07-26 2006-01-27 Alfred Lang Engine with angular movement for use as compressor, has cylinder and piston assembly fixed to shafts, and elliptical shaped pinions fixed on shafts and on power take-off shaft, where pinions permit angular variations to obtain working phase
EP2138740A1 (en) 2008-06-24 2009-12-30 Josep Galceran Sole Drive mechanism for an oscillating piston rotor
US20150040855A1 (en) * 2013-08-06 2015-02-12 Pratt & Whitney Canada Corp. Rotary Internal Combustion Engine with Static Oil Seal

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553954A (en) * 1948-10-22 1951-05-22 Bancroft Charles Rotary machine of the alternating piston type
US3302625A (en) * 1964-05-15 1967-02-07 Cunningham Kelly Gore Engine
US3769946A (en) * 1969-07-14 1973-11-06 W Scherrer Rotary engines
US4338067A (en) * 1980-02-14 1982-07-06 Greenfield Stuart T Alternating piston machine with rotating end walls and chain drive
EP0215194A1 (en) * 1985-09-09 1987-03-25 John E. Stauffer Rotary internal combustion engine
DE4315155C2 (en) * 1993-05-07 1998-04-09 Markus Rieck Rotary lobe machine with periodically variable working chambers
DE4315155A1 (en) * 1993-05-07 1994-11-10 Markus Rieck Rotary engine with periodically varying working chambers
WO1995017582A1 (en) * 1993-12-23 1995-06-29 Janosi Marcell Rotary motion drive, especially for internal combustion engines
US6739307B2 (en) 2002-03-26 2004-05-25 Ralph Gordon Morgado Internal combustion engine and method
US20040211387A1 (en) * 2002-03-26 2004-10-28 Morgado Ralph Gordon Internal combustion engine and method
FR2873401A1 (en) * 2004-07-26 2006-01-27 Alfred Lang Engine with angular movement for use as compressor, has cylinder and piston assembly fixed to shafts, and elliptical shaped pinions fixed on shafts and on power take-off shaft, where pinions permit angular variations to obtain working phase
EP2138740A1 (en) 2008-06-24 2009-12-30 Josep Galceran Sole Drive mechanism for an oscillating piston rotor
US20150040855A1 (en) * 2013-08-06 2015-02-12 Pratt & Whitney Canada Corp. Rotary Internal Combustion Engine with Static Oil Seal
US9334795B2 (en) * 2013-08-06 2016-05-10 Pratt & Whitney Canada Corp. Rotary internal combustion engine with static oil seal

Similar Documents

Publication Publication Date Title
US1482628A (en) Rotary engine
US1792026A (en) Rotary internal-combustion engine
US3799126A (en) Rotary machines
US2370217A (en) Turbine type engine
US3897756A (en) Tandem rotor rotary engine
US1790256A (en) Internal-combustion engine
US3314401A (en) Two-stroke cycle rotary engine
US3207425A (en) Rolling body engine with multiple rotors
US1949225A (en) Rotary internal combustion engine
US4007715A (en) Rotary engines, compressors and vacuum pumps
US1701534A (en) Rotary engine
US1329625A (en) Internal-combustion rotary engine
US3921595A (en) Rotary internal combustion engine
US3895610A (en) Rotary Nutating engine
US1482627A (en) Rotary internal-combustion engine
US1603630A (en) Rotary motor
US3323501A (en) Rotary blade piston engine
US2189728A (en) Rotary internal combustion engine
US3881847A (en) Rotary expansion engine of the type having planetating rotor
US3034486A (en) Pulsating rotary engine
US1874239A (en) Rotary internal combustion engine
US1856839A (en) Rotary internal combustion engine
US3447513A (en) Rotary internal combustion engine
US3886909A (en) Rotary internal combustion engine
US1405326A (en) Rotary engine