US1636799A - Rotary engine - Google Patents

Rotary engine Download PDF

Info

Publication number
US1636799A
US1636799A US444530A US44453021A US1636799A US 1636799 A US1636799 A US 1636799A US 444530 A US444530 A US 444530A US 44453021 A US44453021 A US 44453021A US 1636799 A US1636799 A US 1636799A
Authority
US
United States
Prior art keywords
shaft
pistons
frame
chamber
members
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
US444530A
Inventor
Bernt M Berntsen
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 US444530A priority Critical patent/US1636799A/en
Application granted granted Critical
Publication of US1636799A publication Critical patent/US1636799A/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
    • F02B2730/012Internal-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 piston
    • F02B2730/013Vanes fixed in the centre of the housing; Excentric rotors
    • 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

  • IBERNT M IBERNTSEN, OF BROOKLYN, NEW YORK.
  • This invention relates to rotary engines, and particularly to engines with rotary pistons and one of theprincipal objects is to produce a device of this nature. which shall be simple of construction, cheap to manufacture, and highly eflicient for the purpose for which it is designed.
  • Another object is to produce a device of this kind in which the rotor body and the piston carrying member rotate about respectixirla fixed axes which are arranged eccentrica y.
  • Another object is to provide the rotor with improved packing/means adapted for relative sliding and canting contact with the' several pistons. 7
  • Figure 2 is a vertical sectional view taken substantially on line 22 of Figure 1.
  • Figure 3 is a detailedp'erspective view of one of the packing members.
  • Figure 4 is a side elevation of the engine.
  • 10 represents a frame casting which may be constructed in any suitable manner to support the devices hereinafter described.
  • This frame member 10 is provided with a space 11 in which the water or other cooling medium maycirculate.
  • A. pipe 12 from the carburetor pierces the frame 10 for conduct-' ing fuel to the interior thereof and is provided with a valve 13 'to admit fuel twice on each revolution of the motor.
  • the control may be of any desired well-known type for opening and closing the valve at the proper times.
  • a way 14 is out in'the inner wall of the frame 10 adjacent to the mouth of pipe 12 so as topermit intake of the fu el during a considerable portion of the stroke of the engine.
  • Mountedin hearings in members 50 and 51 secured in'the frame '10 is the drive shaft 15 to which may 'be connected any system of power transmission desired.
  • Mounted on shaft 15 to turn therewith is a gear wheel, the teeth of which-project throu h a slot 52 cut in the tubular inner end 53 0 member 50 and mesh with the teeth of an internal gear 17 formed on or fixedly secured on the inside of a tubular wall 18 of a rotatable piston carrying member mounted eccentrically of shaft 15 and comprising besides the wall 18, an outer flange or wall 19, and four piston blades 20,
  • the wall 19 is provided with four ports 21 intermediate of the pistons 20 for permitting inflow of the.
  • a collar. 54 is mounted in the inner end of member 53 and projects in to the frame 10.
  • the member 53 also carries suitable bearings for member 18 as at 55.
  • a second rotary member or rotor is mounted concentric with shaft '15 and comprising a circular plate 22 and inner and outer flanges 23 and 24.
  • the plate 22 is set into one of the inner faces of the frame 10 and-the flanges 23 and 24 extend into the the two rotating members moving about different fixed centers.
  • each piston 20 is a paekin member such as shown in Figure 3, forme with two curved lugs 26 connected. by a web 27
  • the lugs 26 of each packing member are spaced apart sufiiciently to permit of the necessary movements of the respective piston therebetween, and the sides, of the lugs facing the piston are provided with curved seats in which" are placed semi-cylindrical members 28, the flat faces of which bear against the piston so as to prevent escape of fuel etc.
  • the packing members are spaced apart, and springs 29 tend constantly to force them apart.
  • An exhaust pipe is shown at and from the combustion chamber.
  • Pipe 31 is provided with a valve. 32 which may be operated by 2mg spark plug 33 of any suitable type may be inserted in the frame for effecting the necessar explosions.
  • cams 34 "and 35 which are fixedly mounted upon a counter-shaft 36-.
  • a gear 37 is also'fixed to the shaft 36 and meshes with a gear 38 on the shaft 15.
  • ratio of the. gears is such that the cam shaft rotates one'revolution'to two revolutions of the shaft 15.
  • the cams operate respective valve operating means 39 and40 of any su1table constructionsuchas shown 1n Figure 4 of the drawings,
  • the fuel is drawn from pipe 12 into meet the combustion chambers, and as the chamber enlarges as it asses to its lowest, sition, none of this 0 arge is expelled tli ough the exhaust pipe when the port 21 comes into register with pipe 30.
  • the combustion chamber is broug t up andowing to 'the crowding action of the packing members the vol- 'ume of the combustion chamber is decreased and compression is efl'ected'
  • the pipe 31 is closed by valve-32 at this time so that the charge is not expelled.
  • the port 21 passes plug33, the charge .is igmted and the piston forcedclockwise in Figure 1.
  • valve 13 As the pipe 12 is closed at this time by valve 13, the s are confined in the com ustion chamber until the pell't 21 is in register with exhaust pipe 30. esucceeding portion of the rotat on effects a compression of the remainder of the burnt gases.
  • the valve 32 opens pipe 31 and when port 21 registers wiltllapipe 31the compressed matter is ex-.
  • chamber #1 is 7 on the. intake stroke
  • chamber #2 is completing the exhaust stroke
  • chamber 3 is on the compression stroke
  • 'while cham r #4 is 7 on the. intake stroke
  • chamber #4. will be the next to fire' and while #4 is firing #3 is on the intake stroke, thereby establishing a fining order of-chambers 1, 2, 4 and 3 011 every two While I have shown the engine .as c onstructed for. use with gasoline, it is obvious that the engine is capable of operation by steam. f
  • a rotatable member comprising a plurality of fixedly mountedlradiating pistons, a second rotatable member m unted' eccentrical ly of the first said rotatable member and comprising flanges loosely embracing said pistons, and a plurality of packing membersyieldingly mounted in the second rotatable member and confined between the flanges thereof and slidably engaging said 2.
  • a rotatable member comprising aplurality of fixedly, mounted radiating pistons, a second rotatable member mounted eccentrically of the first said rotatable member and comprlsmg flanges loosely embracing said pistons, a plurality of packing members yieldlngly mounted in the second rotatable member and confined between the flanges thereof and each embracing a respective one of said pistons, and semi-cylindrical members mounted in said packing'members and slidably engaging said pistons.
  • a rotatable member comprising a plurality of fixedly mounted radiating pistons, a second rotatable member mounted eccentrically of the first said rotatable member and comprising flanges loosely embracing Sflld'PlS. tons,'a plurality of packing members mount ed in the second rotatable member and con fined between the flanges thereof. and each embracing a. respective one of said pistons, sprmgs arranged between adjacent ends of said packing members, and semi-cylindrical members mounted in said packing members and slidably engaging said pistons.
  • combustion cham-' them an outer cylindrical member secured to the outer 'ends of said piston blades and provided with ports intermediate said piston blades, and a second r0- member'mounted concentric with said shaft andprov'ided with means for varying r the volume of said combustion chambers for effecting intake, compression and scaveng ingi, said means including a plurality of packing members, and springs between the .20 adjacent ends-of said membersto. force the same in a direction toward its adjacent piston blade.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Description

July '26; 1927.
ROTARY ENGINE! Filed Feb. 12, 1921 3 Sheets-Sheet 1 1,636,799 Jul-y 1927' B. M. BERNTSEN 1 ROTARY ENGINE Filed Feb. 12, 1921 3 Sheets-Shut 2 INVENTOR B. M. BERNTSEN ROTARY ENGINE Filed Feb. 12, 1921 3 Sheets-Sheet 3 Earn: 25% Be/"2; 53:62?
INVENTOR W5 BY ATTO R N EY,
WITNESS:
Patented July 26, 1927.
IBERNT M. IBERNTSEN, OF BROOKLYN, NEW YORK.
ROTARY ENGINE.-
Ap'plicationfiled February 12, 1921. Serial No. 444,580.
This invention relates to rotary engines, and particularly to engines with rotary pistons and one of theprincipal objects is to produce a device of this nature. which shall be simple of construction, cheap to manufacture, and highly eflicient for the purpose for which it is designed.
Another object is to produce a device of this kind in which the rotor body and the piston carrying member rotate about respectixirla fixed axes which are arranged eccentrica y. I
Another object is to provide the rotor with improved packing/means adapted for relative sliding and canting contact with the' several pistons. 7
With these and other objects in view which will be more apparent as thespecification proceeds, the invention consists of certain novel construction and combination and arrangement of parts, the essential features of which are hereinafter fully described, are particularly pointed out in the appended claims, and are illustrated in the accompanying drawing, in which Figure 1 is a vertical sectional view of my improved engine.
Figure 2 is a vertical sectional view taken substantially on line 22 of Figure 1.
Figure 3 is a detailedp'erspective view of one of the packing members.
Figure 4 is a side elevation of the engine.
with parts broken away in section.- Like characters of reference refer to like parts in all views.
Referring to the drawing in detail, 10 represents a frame casting which may be constructed in any suitable manner to support the devices hereinafter described. This frame member 10 is provided with a space 11 in which the water or other cooling medium maycirculate. A. pipe 12 from the carburetor pierces the frame 10 for conduct-' ing fuel to the interior thereof and is provided with a valve 13 'to admit fuel twice on each revolution of the motor. The control may be of any desired well-known type for opening and closing the valve at the proper times. A way 14 is out in'the inner wall of the frame 10 adjacent to the mouth of pipe 12 so as topermit intake of the fu el during a considerable portion of the stroke of the engine.
Mountedin hearings in members 50 and 51 secured in'the frame '10 is the drive shaft 15 to which may 'be connected any system of power transmission desired. Mounted on shaft 15 to turn therewith is a gear wheel, the teeth of which-project throu h a slot 52 cut in the tubular inner end 53 0 member 50 and mesh with the teeth of an internal gear 17 formed on or fixedly secured on the inside of a tubular wall 18 of a rotatable piston carrying member mounted eccentrically of shaft 15 and comprising besides the wall 18, an outer flange or wall 19, and four piston blades 20, The wall 19 is provided with four ports 21 intermediate of the pistons 20 for permitting inflow of the. fuel to the combustion chambers defined by the pistons, and to permit the exhaust of the burnt gases and products of combustion after explosion. A collar. 54 is mounted in the inner end of member 53 and projects in to the frame 10. The member 53 also carries suitable bearings for member 18 as at 55.
A second rotary member or rotor is mounted concentric with shaft '15 and comprising a circular plate 22 and inner and outer flanges 23 and 24. The plate 22 is set into one of the inner faces of the frame 10 and-the flanges 23 and 24 extend into the the two rotating members moving about different fixed centers.
Straddling each piston 20 is a paekin member such as shown in Figure 3, forme with two curved lugs 26 connected. by a web 27 The lugs 26 of each packing member are spaced apart sufiiciently to permit of the necessary movements of the respective piston therebetween, and the sides, of the lugs facing the piston are provided with curved seats in which" are placed semi-cylindrical members 28, the flat faces of which bear against the piston so as to prevent escape of fuel etc. The packing members are spaced apart, and springs 29 tend constantly to force them apart.
An exhaust pipe is shown at and from the combustion chamber.
pierces the frame member-10, its inner end ,being situated so as to receive the exhaust from the combustion chambers. An 9,l1Xll-- forced upon the scavenging portion of the rotation. Pipe 31 is provided with a valve. 32 which may be operated by 2mg spark plug 33 of any suitable type may be inserted in the frame for effecting the necessar explosions.
In or er to facilitate the correct opening and closing of the valves 13 and 32, I provide respective cams 34 "and 35 which are fixedly mounted upon a counter-shaft 36-. A gear 37 is also'fixed to the shaft 36 and meshes with a gear 38 on the shaft 15. The
ratio of the. gears is such that the cam shaft rotates one'revolution'to two revolutions of the shaft 15. The cams operate respective valve operating means 39 and40 of any su1table constructionsuchas shown 1n Figure 4 of the drawings,
In operation, the fuel is drawn from pipe 12 into meet the combustion chambers, and as the chamber enlarges as it asses to its lowest, sition, none of this 0 arge is expelled tli ough the exhaust pipe when the port 21 comes into register with pipe 30. As the rotation roce'eds, the combustion chamber is broug t up andowing to 'the crowding action of the packing members the vol- 'ume of the combustion chamber is decreased and compression is efl'ected' The pipe 31 is closed by valve-32 at this time so that the charge is not expelled. As the port 21 passes plug33, the charge .is igmted and the piston forcedclockwise in Figure 1. As the pipe 12 is closed at this time by valve 13, the s are confined in the com ustion chamber until the pell't 21 is in register with exhaust pipe 30. esucceeding portion of the rotat on effects a compression of the remainder of the burnt gases. The valve 32 opens pipe 31 and when port 21 registers wiltllapipe 31the compressed matter is ex-.
With reference toFigure 1 of the drawings, it will be seen that the chamber #1 is 7 on the. intake stroke, chamber #2 is completing the exhaust stroke, chamber 3 is on the compression stroke, 'while cham r #4.
is at the completionof' the power stroke. In the operation of the engine, gas is being taken into the chamber'#1, and upon 0 ockwise rotation of'therotor, the gas is compressed and when brought into register with the spark plu 33,'thesame will explode 'the charge. 1e chamber #2 during this time has completed the exhaust stroke and taken in charge of gas, and will follow the same operation as the chamber #1 thus causing two successive;- explosions in the respective -chambers'#1 and #2 upon the first revolution fromthe point shown. It will understood that chamber #3 which is shown on the compression stroke hasfired of the rotor.
chamber #4. will be the next to fire' and while #4 is firing #3 is on the intake stroke, thereby establishing a fining order of- chambers 1, 2, 4 and 3 011 every two While I have shown the engine .as c onstructed for. use with gasoline, it is obvious that the engine is capable of operation by steam. f
revolutions I While I have described what I deem to be the most desirable embodiment 'of my in tails may be varied without'in any way departing from the spirit of my invention, and
vention limited only by the appended claims.
What is claimed asnew is 1. In a device of the class described, theso vention, it is obvious that many of the decombination with the framework thereof, of
a rotatable member comprising a plurality of fixedly mountedlradiating pistons, a second rotatable member m unted' eccentrical ly of the first said rotatable member and comprising flanges loosely embracing said pistons, and a plurality of packing membersyieldingly mounted in the second rotatable member and confined between the flanges thereof and slidably engaging said 2. In a device of the class described, the
pistons.
combination with the framework thereof, of
a rotatable member comprising aplurality of fixedly, mounted radiating pistons, a second rotatable member mounted eccentrically of the first said rotatable member and comprlsmg flanges loosely embracing said pistons, a plurality of packing members yieldlngly mounted in the second rotatable member and confined between the flanges thereof and each embracing a respective one of said pistons, and semi-cylindrical members mounted in said packing'members and slidably engaging said pistons.
3 In a device of the class described, the
.combination with the framework thereof, of
a rotatable member comprising a plurality of fixedly mounted radiating pistons, a second rotatable member mounted eccentrically of the first said rotatable member and comprising flanges loosely embracing Sflld'PlS. tons,'a plurality of packing members mount ed in the second rotatable member and con fined between the flanges thereof. and each embracing a. respective one of said pistons, sprmgs arranged between adjacent ends of said packing members, and semi-cylindrical members mounted in said packing members and slidably engaging said pistons.
4. In a device of the class described, the
rtary combinationof frame, a shaft rotatably mounted in'said frame, a gear fixedly mounted on said shaft, a cylindrical member enclosin said shaft and mounted .110 ro- 6 tate eccentrically of said shaft, an internal I gear fixedly secured in said cylindrical memher and meshin with the first said gear, piston blades ra 'ating' from said cylindrical member and defining. combustion cham-' them, an outer cylindrical member secured to the outer 'ends of said piston blades and provided with ports intermediate said piston blades, and a second r0- member'mounted concentric with said shaft andprov'ided with means for varying r the volume of said combustion chambers for effecting intake, compression and scaveng ingi, said means including a plurality of packing members, and springs between the .20 adjacent ends-of said membersto. force the same in a direction toward its adjacent piston blade. i
5. In a device of the class described, the
' combination of the main frame, a shaft rotatably mounted in said frame, agear fixed- 1y mounted on said shaft, a cylindrical member enclosing said shaft and mounted to ro- .tate eccentrically of said shaft, an internal packing members, and springs between. the 1 adjacent ends of said members to force the same in a direction towards its adjacent iston blade, and a feed pipe and a plurality of exhaust pipes extending through said main frame and positioned to register with the ports in the second said cylindrical memher, said exhaust pi es being effective one after the other to e ect more perfect scav- 50 whereof I have aflixed my BERNT M. BEBiITsEN.
'enging.
In testimony signature.
US444530A 1921-02-12 1921-02-12 Rotary engine Expired - Lifetime US1636799A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US444530A US1636799A (en) 1921-02-12 1921-02-12 Rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US444530A US1636799A (en) 1921-02-12 1921-02-12 Rotary engine

Publications (1)

Publication Number Publication Date
US1636799A true US1636799A (en) 1927-07-26

Family

ID=23765295

Family Applications (1)

Application Number Title Priority Date Filing Date
US444530A Expired - Lifetime US1636799A (en) 1921-02-12 1921-02-12 Rotary engine

Country Status (1)

Country Link
US (1) US1636799A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2513447A (en) * 1946-05-17 1950-07-04 Brown And Brown Rotary pump or motor
US2516051A (en) * 1945-07-10 1950-07-18 Faitout Andre Charles Rotary internal-combustion engine
US3198085A (en) * 1962-06-14 1965-08-03 Eugene O Cornell Liquid power booster
US3256867A (en) * 1962-08-27 1966-06-21 John L Betzen Rotary combustion engines
US3307526A (en) * 1966-06-17 1967-03-07 John L Betzen Internal combustion engines
US3782341A (en) * 1972-04-06 1974-01-01 T Eells Rotary internal combustion engine
US3807912A (en) * 1972-09-25 1974-04-30 Keller Corp Fluid flow device having high degree of flexibility
US20060204392A1 (en) * 2003-09-10 2006-09-14 Sharudenko Andrey Y Rotary machine (variants), a working member therefor and an propulsion device using said rotary machine
US20100300400A1 (en) * 2007-10-17 2010-12-02 Jose Fernando Bittencourt Rotary internal combustion engine
US9664106B2 (en) * 2015-02-17 2017-05-30 Ted Nae-Kuan Chiang Rotary combustion engine system having toroidal compression and expansion chambers

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2516051A (en) * 1945-07-10 1950-07-18 Faitout Andre Charles Rotary internal-combustion engine
US2513447A (en) * 1946-05-17 1950-07-04 Brown And Brown Rotary pump or motor
US3198085A (en) * 1962-06-14 1965-08-03 Eugene O Cornell Liquid power booster
US3256867A (en) * 1962-08-27 1966-06-21 John L Betzen Rotary combustion engines
US3307526A (en) * 1966-06-17 1967-03-07 John L Betzen Internal combustion engines
US3782341A (en) * 1972-04-06 1974-01-01 T Eells Rotary internal combustion engine
US3807912A (en) * 1972-09-25 1974-04-30 Keller Corp Fluid flow device having high degree of flexibility
US20060204392A1 (en) * 2003-09-10 2006-09-14 Sharudenko Andrey Y Rotary machine (variants), a working member therefor and an propulsion device using said rotary machine
US7353796B2 (en) * 2003-09-10 2008-04-08 Sharudenko Andrey Y Rotary machine
US20100300400A1 (en) * 2007-10-17 2010-12-02 Jose Fernando Bittencourt Rotary internal combustion engine
US9027528B2 (en) * 2007-10-17 2015-05-12 Jose Fernando Bittencourt Rotary internal combustion engine
US9664106B2 (en) * 2015-02-17 2017-05-30 Ted Nae-Kuan Chiang Rotary combustion engine system having toroidal compression and expansion chambers

Similar Documents

Publication Publication Date Title
US1636799A (en) Rotary engine
GB1578644A (en) Rotary internal combustion engine
US1792026A (en) Rotary internal-combustion engine
US4033299A (en) Rotary engine
US3207425A (en) Rolling body engine with multiple rotors
US1637958A (en) Internal-combustion engine
US1575860A (en) Internal-combustion engine
US2295117A (en) Rotary engine
US3361119A (en) Internal combustion engine
US1329625A (en) Internal-combustion rotary engine
US1748568A (en) Rotary internal-combustion engine
US2248029A (en) Internal combustion engine
US1856839A (en) Rotary internal combustion engine
US1829391A (en) Rotary internal combustion engine
US1874239A (en) Rotary internal combustion engine
US2263361A (en) Internal combustion engine
US3312201A (en) Rotary fluid driven or fluid pumping apparatus
US2571642A (en) Rotary internal-combustion engine
US1856242A (en) Internal combustion engine
US2342515A (en) Internal combustion engine
US1713378A (en) Rotary engine
US3913533A (en) Rotary internal combustion engine
US1247973A (en) Rotary internal-combustion engine.
US2904019A (en) Rotary internal combustion engine
US1721855A (en) Motob