US1482221A - Explosion engine - Google Patents

Explosion engine Download PDF

Info

Publication number
US1482221A
US1482221A US326191A US32619119A US1482221A US 1482221 A US1482221 A US 1482221A US 326191 A US326191 A US 326191A US 32619119 A US32619119 A US 32619119A US 1482221 A US1482221 A US 1482221A
Authority
US
United States
Prior art keywords
piston
cylinder
air
engine
current
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
US326191A
Inventor
Joseph L Cato
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 US326191A priority Critical patent/US1482221A/en
Application granted granted Critical
Publication of US1482221A publication Critical patent/US1482221A/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
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/16Pistons  having cooling means
    • F02F3/18Pistons  having cooling means the means being a liquid or solid coolant, e.g. sodium, in a closed chamber in piston

Definitions

  • the ob ect of my invention is to provide an internal combustion engine having an effective coolingmeans, which is of such character that an engineprovided with said cooling means will have less weight than the engines using previouslyknown cooling 7 of the engine.
  • Figure 2 is a bottom View of said piston
  • Figure 3 is a transverse section of said piston
  • Figure 4 is another transverse section of the same taken on line M of Figure 3.
  • a cylinder 1 of an aeroplane engine of internal combustion type having at the top thereof a closure 2, provided with a spark plug 3 at one side thereof, an inlet port 4; for a fuel mixture, controlled by a valve 5, and an outlet port 6 for the products of combustion, controlled by a valve 7
  • a port 8 for the passage of air which at all times communicates with a longitudinal passagetransverse strengthening partition 13.
  • passageway 9 opposite to the location of the way 9 on one side of a piston 10, the lower endof which passageway 9 isclosed by'a flange 11, but the upper end of which is vopen to communicate with a plurality of transverse passageways 12,"formed by Ia n ()n the side of the passageway 9, there is a further passageway 15, which is open at the top, but the lower end of which is closed by a stationary piston 16, carried by the lower end of thecylins der 1, and held in place by a plurality of screws 17, passing from the cylinder 1 into a crank casing 18.
  • the passageways 9 and 15 are connected by a hollow crank pin 19, held in place in the piston 10 by a screw 20, and which supports a connecting rod 21. cooling is secured in this way. If desired, a still greater cooling eiiect may be obtained by providing fins 22 on the outside of the cylinder 1.
  • An internal combustion engine having in a cylinder means for providing therein a current of air, comprising a stationary partition cooperating with an engine piston and fitting in a passageway located at one side of the piston.
  • An internal combustion engine having in a cylinder means for providing therein a current ofair, comprising a stationary par- Additional tition cooperating with an engine piston and fitting in a passageway located atone side the piston in contact with said current of air.
  • An internal combustion engine having in a cylinder means for providing therein a current-of air, comprising a stationary partition cooperating with an engine piston, a continuously openport in the cylinder, and
  • a fin extending transversely through'the a a current otair, comprising astationary piston in contact with said current of air.
  • An lnternal' combustion engine having ma cyllndermeansfor providing therein ,partition cooperating. with an engine piston and fitting ma passageway located atone side of the piston, a continuously open port in the cylinder, andafin extending transversely through the piston in contact with said current of air.
  • An internal combustion engine having inva cylinderameans'j for providing therein a .currentof air, comprising a stationary partition cooperating withan engine piston,v
  • An internal combustion engine having in a ylinder means for providing therein a current of 'air, comprising longitudinal and transverse passageways in the piston, said transverse passagewayhaving a cooling fin therein, a po rt ⁇ in' thecylinder leading to a longitudinal passageway, and a stationary partition nearisaidflporb.
  • An internal combustion engine having in a cylinder-means for providing therein a currentof air, comprising longitudinal and transverse passageways in'thepiston, and a crank pin passageway, also, connectingthe longitudinal passageways.
  • Aniinternal combustion engine having in a cylinder-means for providing therein a current of air, comprising longitudinal and transverse passageways-in the piston, said .transversepassageway having a cooling'ifin therein, and a crank. in passageway also connecting the longitu inal passageways.
  • An internal combustion engine having ma cylinder means forproviding therein .a current of air, comprising longitudinal passageways in thepiston and. a crank pin passageway connecting the same.

Description

Jan. 29, 1924.
J. L. CATO EXPLOS ION ENGINE Filed Sept. 24, 1919 2 Sheets-Sheet 2 Patented Jan. 29, 1924.
name 4 stars s a p E FM QCE.
JOSEPH L. CATO, F ELMI-IURSI, NEW YORK.
nxrnosron ENGINE.
Application filed September 24, 1919. Serial No. 326,191.
T 0 all whom it may concern Be it known that I, JosnPH L. CATO, a citizen of the United States, residin Elmhurst, in the county of Queens and tate of New York, have'invented a certain new anduseful Improvement in Explosion Engines, of which the .i'ollowing is a specification. j p i My invention is applicable to internal combustion engines of many different kinds,
but is especially applicable to such engines used for driving automobiles or aeroplanes. .The ob ect of my invention is to provide an internal combustion engine having an effective coolingmeans, which is of such character that an engineprovided with said cooling means will have less weight than the engines using previouslyknown cooling 7 of the engine. t
Further objects of my invention will appearfrom the detaileddescription thereof contained hereinafter."
.While my invention is capable of embojdiment in many diflerent forms, for the purpose of illustration I have shown only one form of the same in the accompanying drawings, in which:
Figural is a cross-section of a portion of an engine cylinder and piston made in accordance with my invention,
Figure 2 is a bottom View of said piston;
Figure 3 is a transverse section of said piston; and
Figure 4 is another transverse section of the same taken on line M of Figure 3.
In the drawings, I have shown a cylinder 1 of an aeroplane engine of internal combustion type, having at the top thereof a closure 2, provided with a spark plug 3 at one side thereof, an inlet port 4; for a fuel mixture, controlled by a valve 5, and an outlet port 6 for the products of combustion, controlled by a valve 7 In the cylinder 1, there is provided a port 8 for the passage of air, which at all times communicates with a longitudinal passagetransverse strengthening partition 13. the passageways 12 there are a plurality of transverse fins 1 1, to increase the cooling eliect of the air. piston 10 opposite to the location of the way 9 on one side of a piston 10, the lower endof which passageway 9 isclosed by'a flange 11, but the upper end of which is vopen to communicate with a plurality of transverse passageways 12,"formed by Ia n ()n the side of the passageway 9, there is a further passageway 15, which is open at the top, but the lower end of which is closed by a stationary piston 16, carried by the lower end of thecylins der 1, and held in place by a plurality of screws 17, passing from the cylinder 1 into a crank casing 18. It will also be noted that the passageways 9 and 15 are connected by a hollow crank pin 19, held in place in the piston 10 by a screw 20, and which supports a connecting rod 21. cooling is secured in this way. If desired, a still greater cooling eiiect may be obtained by providing fins 22 on the outside of the cylinder 1.
In the operation of my invention, as the piston 10 reciprocates, currents of air are first drawn in through the port 8 upon the upward stroke of said piston, and are forced out through the port 8 upon the downward stroke of said piston, owing to the pres.
ence of the stationary piston 16. These currents of air pass not only over much of the interior of the piston 10, but come into contact with the cooling fins 14, aswell as the interior of the crank pin 19, so that the cylinder 1 is effectively cooled from the inside by these currents of (t11. 'A further cooling effect is secured by the presence of the fins 22 on the outside of the cylinder 1.
While I have described my invention above in detail, I wish it to be understood that many changes may be made therein without departing from the spirit of the same.
I claim:
1. An internal combustion engine having in a cylinder means for providing therein a current of air, comprising a stationary partition cooperating with an engine piston and fitting in a passageway located at one side of the piston.
2. An internal combustion engine having in a cylinder means for providing therein a current ofair, comprising a stationary par- Additional tition cooperating with an engine piston and fitting in a passageway located atone side the piston in contact with said current of air.
5. .An internal combustion engine having in a cylinder means for provldingthereln a current of air, comprising astationaryrpar- ;tit-ion cooperating with an engine piston and fitting in a passageway located atone side of the piston and a fin extending transversely through the piston in contact with said current of air.
6. An internal combustion engine having in a cylinder means for providing therein a current-of air, comprising a stationary partition cooperating with an engine piston, a continuously openport in the cylinder, and
.. a fin extending transversely through'the a a current otair, comprising astationary piston in contact with said current of air.
7.; An lnternal' combustion engine having ma cyllndermeansfor providing therein ,partition cooperating. with an engine piston and fitting ma passageway located atone side of the piston, a continuously open port in the cylinder, andafin extending transversely through the piston in contact with said current of air.
8. An internal combustion enginehaving inva cylinderameans'j for providing therein a .currentof air, comprising a stationary partition cooperating withan engine piston,v
a continuously open portin the cylinder :00- operating with a passageway 1n the piston,
and a fin extendingtransversely throu h the piston incontact with said current 'o-fair.
9. An internal combustion engine having in a cylinder means for providing therein a current-of aim-comprising a stationary partition cooperating with an engine piston and fitting in a passageway located at one side of thepiston, a continuously open port in the cylinder cooperating wit-h the passageway in the piston, and a fin ,eXtendingtr-ans versely through the piston=incontact with saidcurrent of air.
10. "An internal combustioneengine having in a cylinder-means for provid ng therein a current of air, comprising longitudinal and transverseipassageways in the piston,- a port in the cylinder leading to a' longitudinal passageway,- and a stationary-partitionnear. said-port.
11. An internal combustion engine having in a ylinder means for providing therein a current of 'air, comprising longitudinal and transverse passageways in the piston, said transverse passagewayhaving a cooling fin therein, a po rt{in' thecylinder leading to a longitudinal passageway, and a stationary partition nearisaidflporb.
'12. An internal combustion engine having in a cylinder-means for providing therein a currentof air, comprising longitudinal and transverse passageways in'thepiston, and a crank pin passageway, also, connectingthe longitudinal passageways.
F13. Aniinternal combustion engine having in a cylinder-means for providing therein a current of air, comprising longitudinal and transverse passageways-in the piston, said .transversepassageway having a cooling'ifin therein, and a crank. in passageway also connecting the longitu inal passageways.
14.. An internal combustion engine having ma cylinder means forproviding therein .a current of air, comprising longitudinal passageways in thepiston and. a crank pin passageway connecting the same.
In testimony that I claim 'thefforegoing, I have hereunto set my hand thisfiQQhdday of September, 1919.
JOSEPH L. CATO.
US326191A 1919-09-24 1919-09-24 Explosion engine Expired - Lifetime US1482221A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US326191A US1482221A (en) 1919-09-24 1919-09-24 Explosion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US326191A US1482221A (en) 1919-09-24 1919-09-24 Explosion engine

Publications (1)

Publication Number Publication Date
US1482221A true US1482221A (en) 1924-01-29

Family

ID=23271184

Family Applications (1)

Application Number Title Priority Date Filing Date
US326191A Expired - Lifetime US1482221A (en) 1919-09-24 1919-09-24 Explosion engine

Country Status (1)

Country Link
US (1) US1482221A (en)

Similar Documents

Publication Publication Date Title
US3046958A (en) Internal combustion device
US1482221A (en) Explosion engine
US2442217A (en) Two-cycle crankcase compression engine, fuel distribution control
US1464906A (en) Diesel engine
US1938537A (en) Cooling system for aeronautical engines
US1510651A (en) Supercharging internal-combustion-engine valve mechanism
US1638288A (en) Internal-combustion engine
US2196252A (en) Two-cycle engine
US1541207A (en) Internal-combustion engine
US1777656A (en) Mixing device
US2077457A (en) Internal combustion engine
US1921510A (en) Two-stroke cycle internal combustion engine
US1778817A (en) Steam engine
US1661558A (en) Internal-combustion engine
US2376968A (en) Two-cycle gas engine
US1649817A (en) Internal-combustion engine
US1694642A (en) Internal-combustion engine
US2373924A (en) Internal-combustion engine
US1618614A (en) Cooling means for internal-combustion engines
US1585377A (en) Internal-combustion engine
GB301079A (en) Improved combustion product power plant
US2731959A (en) kratzer
US1337077A (en) Internal-combustion engine
US1530539A (en) Internal-combustion engine
US1386381A (en) Cooling-jacket for internal-combustion engines