US864889A - Rotary engine. - Google Patents
Rotary engine. Download PDFInfo
- Publication number
- US864889A US864889A US35904107A US1907359041A US864889A US 864889 A US864889 A US 864889A US 35904107 A US35904107 A US 35904107A US 1907359041 A US1907359041 A US 1907359041A US 864889 A US864889 A US 864889A
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- US
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- Prior art keywords
- piston
- inlet
- engine
- exhaust
- rotary engine
- Prior art date
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- Expired - Lifetime
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/30—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C2/34—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
- F04C2/344—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F04C2/3446—Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface
Definitions
- An Ubjoot ol my invention is to p1,Vi(lD means WlltllU by steam or other Agency employed in rotary engines is admitted at both ends of the rotary piston huh, and thereby equalize the pr we fill either ornl thereof.
- Another o bjoct is to provide it re large power for the size thereof.
- Figure I s in end View of :rrotnry engine embodying: my invention, the low if spur gear li ing removed to show the inlet and UXljlLt'll-Eli pipes and the nlljnslnhlc steam cut oll.
- Fig. 1?.- is :1. ion showing the end of the rotating; piston :rnzl of the nhntinen" eylinllcr tnlton on line 2 ol .llig. 3 looking in the direction indicated by thearrowheadsf2 thereon. .li'i lsn. control 2 tical section taken on line 25-- 3 of Fig. 1, ports shown in elevation.
- Fig. l --1 in end plnte removed from the engine looking in the direction indicated by the in row heads t l of l3" 3.
- a. piston cylinder and on abutment cylinder said piston cylinder previilod with n piston bltti exhaust grooves and inlet ports, said. abutment cylinder being provided with a recess; end plntes having: linnnlur inlet grooves in their faces and an exhaust port; and o, steam cut oil ntljustably mounted in the inlet grooves;
- a piston cylinder carrying a piston blade the entire length thereof and having in each end thereof an exhaust groove communicating with an exhaust port, the said cylinderhcing provided atcuch end with an exhaust port in ad- VI-ZUCE 01 the piston blades and provided at each end in the rear of the piston blades with inlet ports, in combjnw tion with a casing having in each end thereof an annular inlet groove; and 9. check adjustahly secured in the inlet groove.
Description
' No. 864,889. PATENTED SEPT. 3. 1907.
A. G. EDWARDS. ROTARY ENGINE.
APPLICATION FILED FEB. 25. 1907.
2 SHEETS-SHE??? 1.
PATENTED SEPT. 8, 1907.
A. G. EDWARDS. ROTARY ENGINE.
APPLICIATION ILBD FEB 2 1907 2 SHEETSSHEET 2.
mmmnmmm l yaw/W7 on of litotters lljintent.
li ntentod. Elefp't. -3, 1992/ ilpplloatiou fiiecl February 25, 190'). Serial lilo 359,0 2-1.
To all when: it new concern:
Be it known thnt i, it I. TICANllF-TR ll. l lDVr'MllJE-Q ll. citimen of the United States, n ling in; Long-hutch, in the county of Lon rlngeles znnl finite oi tnlil'ornin, have in.- vented new and usel'nl lilllliUVOlllClllzl in .ltotory l 1-- gines, of which the following is n s ilii'rntion.
An Ubjoot ol my invention is to p1,Vi(lD means WlltllU by steam or other Agency employed in rotary engines is admitted at both ends of the rotary piston huh, and thereby equalize the pr we fill either ornl thereof.
Another ohjectis: to pn Lflt: on inljnslwtlill: cut oil for the inlet ports oi the engine.
Another o bjoct is to provide it re large power for the size thereof.
1 accomplish these object liy moons of tho device described herein ltllll illust red in the :n- )rnpnnying rim-wings, in which:
Figure I s in end View of :rrotnry engine embodying: my invention, the low if spur gear li ing removed to show the inlet and UXljlLt'll-Eli pipes and the nlljnslnhlc steam cut oll. Fig. 1?.- is :1. ion showing the end of the rotating; piston :rnzl of the nhntinen" eylinllcr tnlton on line 2 ol .llig. 3 looking in the direction indicated by thearrowheadsf2 thereon. .li'i lsn. control 2 tical section taken on line 25-- 3 of Fig. 1, ports shown in elevation. Fig. l --1 :in end plnte removed from the engine looking in the direction indicated by the in row heads t l of l3" 3.
Like most engines of this type the rotatio n uton l3 worlnrbly connected with the nhntnicnt mler (l by means ol the usual spin goers 7 tll1(l The piston e indor carries on its pcripltwory :t piston ll which ho. a, sliding Contact With the lower member 10 of the casing,
engine having t while the abutment cylinder has it sliding contnctwith the upper member ll of the song. A recess 12 in the abutment cylinder provides clearztnee for the piston in its revolution. Live steam ismhnitted into the engine through the inlet ipe 13 which passes thenee into the annular groove 14 lsee Fig. 1) in the end plate. -This annular inlet groove extends (H'Ollllil on the inside of the end plate nearly the entire distance it] ill is provided with an adjustable out ell 15 (see Fig. at), which has on air tight lit therein and is holdtightl in its adjusted position by the set screws THE.- lrleginentztl openi s l7 (Fig.1.)are provided in tlleeml plates lo? the pat thorethrongh ol the shnnlasoi the screw-1 In, providing thereby means for the adjustment of the cut oil 15 at any desired position in the inlet groove l li Both eml plates nreprovidcd with these annular grooves, and.
an inlet ilmth ends of the pint strnetion atml each inn exhaust U m passing into the engine 'tln'ongh the inlet Ill pass through the inlet port-125 into the in .1 the inlet pass 3* the l/i've e pipes 13 ,r let groove i l llllll will loss out tl 'o 20 into the (illillllllil' .lll (see Ill" 2) and will [orco piston ttltllllltl in the i lrootion indicated lay the 1 head in the (ll'LLVr'lDg o clzlntnst steam in the motor tnno passing out 0t tie ohinnher ill through the exhaust ports '3 and thence through the exhaust groove out of tho exlnmst ports Y Mn the out oll l5 disposed in the groove l l is so :nljnnlotl therein to stop the zroniission oi strnm into the inlet pausing-e 20 at the proper time, Thus it will be seen thnt i have provided means which enables mete l'ecll thev engine with live :3 tlll and at the some time rovide menus to :;hnust the stoznn. ll 'hen live steznn li-i admitted into th chmnher ll) mil exerts an impulse upon the piston ll to 'U'KBVB it too 'nrdly, lho pit go notion-lily of the exhaust stoznn through ports 2;, the inlet pore being disposed iinrneilinliiv in the rear of the piston :tml the exhaust ports imineilintcly in front thereof. Wi -n the piston blade enter the recess in the abutment eyiinller, the recon will he filled with steznn from hohiinl the pislii niilmle. This steoni will he carried in the recess in ts travel and who" the hhicle leaves tln recess it i l not on the blade tolforcc it for mini until the poo, shownv in Fig. 2 is reached, when admission token pines. lit will be understood that the exhaust is out off from the 8111106., in front of the blade (luring the cnti 3 period in which the hlsnle is in the recess of the abutment oylin ler, so that any stoinn whioh finds its way into the recess Will not be exhausted. Having described my invention what l claim as new and desire to secure by .liettors Patent is:--
1. In a rotary engine, the combination of a. piston cylinder and on abutment cylinder, said piston cylinder previilod with n piston bltti exhaust grooves and inlet ports, said. abutment cylinder being provided with a recess; end plntes having: linnnlur inlet grooves in their faces and an exhaust port; and o, steam cut oil ntljustably mounted in the inlet grooves;
1n 1m ermine or. the character described, :i rotary lllslen cylinder carrying ii piston hlnxle and bovine in one]! end thereof on exlnn l port cormnuni V n; on allotment eyilnder havingon the periphery thereof :1 piston blade wing recess, the said cylinders worknbly (minim-ted by spur gears, in combination with a casing snrronndint, said cylinders :nul having it each end thereof adjnceotto the piston cylinder an annular inlet groove, the snltl piston cylinder having on either 92111 thereof on inlet port communicating with the inlet groove; :1 shut off'adjustably secured in the inlet groove, substantially as herein shown and described 3. In :1 rotary engine 01 the character described, a piston cylinder carrying a piston blade the entire length thereof and having in each end thereof an exhaust groove communicating with an exhaust port, the said cylinderhcing provided atcuch end with an exhaust port in ad- VI-ZUCE 01 the piston blades and provided at each end in the rear of the piston blades with inlet ports, in combjnw tion with a casing having in each end thereof an annular inlet groove; and 9. check adjustahly secured in the inlet groove.
In witness that I claim the foregoing I have hereunto subscribed my name this 16th day of February, 1907.
v ALEXANDER G. EDWARDS.
Witnesses HENRY T. HAZARD, EDMUND A. S'rnwsn.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US35904107A US864889A (en) | 1907-02-25 | 1907-02-25 | Rotary engine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US35904107A US864889A (en) | 1907-02-25 | 1907-02-25 | Rotary engine. |
Publications (1)
Publication Number | Publication Date |
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US864889A true US864889A (en) | 1907-09-03 |
Family
ID=2933339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US35904107A Expired - Lifetime US864889A (en) | 1907-02-25 | 1907-02-25 | Rotary engine. |
Country Status (1)
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US (1) | US864889A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3116666A (en) * | 1961-02-15 | 1964-01-07 | Dewey L Scott | Rotary engine |
WO1995027844A2 (en) * | 1994-03-30 | 1995-10-19 | Gennaro Mark A | Twin rotor expansible/contractible chamber assembly |
US5466138A (en) * | 1993-07-22 | 1995-11-14 | Gennaro; Mark A. | Expansible and contractible chamber assembly and method |
-
1907
- 1907-02-25 US US35904107A patent/US864889A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3116666A (en) * | 1961-02-15 | 1964-01-07 | Dewey L Scott | Rotary engine |
US5466138A (en) * | 1993-07-22 | 1995-11-14 | Gennaro; Mark A. | Expansible and contractible chamber assembly and method |
US5518382A (en) * | 1993-07-22 | 1996-05-21 | Gennaro; Mark A. | Twin rotor expansible/contractible chamber apparauts |
WO1995027844A2 (en) * | 1994-03-30 | 1995-10-19 | Gennaro Mark A | Twin rotor expansible/contractible chamber assembly |
WO1995027844A3 (en) * | 1994-03-30 | 1996-01-25 | Mark A Gennaro | Twin rotor expansible/contractible chamber assembly |
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