US1424234A - Cooling device for air-cooled engines - Google Patents

Cooling device for air-cooled engines Download PDF

Info

Publication number
US1424234A
US1424234A US417820A US41782020A US1424234A US 1424234 A US1424234 A US 1424234A US 417820 A US417820 A US 417820A US 41782020 A US41782020 A US 41782020A US 1424234 A US1424234 A US 1424234A
Authority
US
United States
Prior art keywords
air
ejector
cooling device
chamber
cooled engines
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
US417820A
Inventor
Bowen James
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 US417820A priority Critical patent/US1424234A/en
Application granted granted Critical
Publication of US1424234A publication Critical patent/US1424234A/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
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • F01P5/08Use of engine exhaust gases for pumping cooling-air

Definitions

  • This invention relates to cooling devices for cooled engines, and in accordance therewith a device is provided comprising an air chamber fitted upon the top of the cylinder around the top fin, suitably perforated to permit of the passage of air from the atmosphere thereinto, and from which chamber the air is drawn through an outlet connected by piping to an ejector fitted at the end of the exhaust pipe, the exhaust gases passing through the nozzle of the ejector at a high velocity, serving to draw the air from the cooling chamber and eject same to the atmosphere; a fresh supply of air rushes into said chamber through the perforations, and a continuous flow of cool air thus passes over and around the cyln1- der head.
  • Figure 1 is a diagrammatic view in elevation, showing the device applied to an internal combustion engine.
  • Figure 2 to an enlarged scale, is a plan of the air-cooling chamber constructed in accordance with .this invention.
  • Figure 3 is a side elevation of same.
  • Figure 4 is a side elevation of an ejector adapted to be connected to the exhaust and to a pipe communicating with the cooling chamber;
  • Figure 5 shows, in sectional side elevation, another form of ejector applicable to the cooling device of this invention.
  • Figure 6 is an end section of same.
  • Figure 7 is a plan of a copper conductor placed on the cylinder head for absorbing heat therefrom and localizing same to facilitate the action of the device.
  • a cooler or air chamber a consisting of an aluminium hollow body, made in one, two or three parts, (in the drawings see particularly Figures 2 and 3it is shown as in three sections l 2 3 to suit the design of the engine to which it is to be fitted, is attached to the cylinder head over and around the top fin b, Figure 1.
  • hollow body is perforated as at b and c- Figures 2 and 3, to permit air to enter same and an outletcZ is provided to which is attached a tube or pipe 6 which may be flexible or rigid, and which is, at its other end, connected to an ejector 7 fixed over the end of the engine exhaust pipe 9 which ejector is formed with a socket or union h for its reception.
  • the ejector comprises (in one form) a hollow chamber formed with a nozzle f, into which a jet 2', into which the end of the exhaust pipe 9 opens, projects and through which the exhaust gases from the engine are ejected at a high velocity, drawing with them air from the cooler at through the pipe 6, and the space around said jet in the hollow chamber I of the ejector aforesaid.
  • a fresh supply of air rushes in through the perforations b and c in the body of cooler a at every exhaust stroke of the engine, hence a constant How of cool air is maintained over the cylinder end.
  • ejector f is shown separately in Figures 5 and 6, wherein said ejector takes the shape of a flattened casing having its sides tapering from near the inlet end A. to the outlet B-see particularly Figure 6-in such manner that the nozzle outlet is in the form of an elongated slot 7.
  • the jet portion z' through which the exhaust gases pass from the engine is similarly tapered at its sides j- Figure 5- and has its ends y"- Figure 6opening out fanwise from the exhaust inlet to the outlet, which latter is also in the form of an elongated slot.
  • the ejector f is formed or fitted with sockets or unions 7t and k for connection with the pipe or tubing 6 leading from the cooling body a, and with the exhaust pipe 9 of engine respectively.
  • Said sockets or unions may be formed integral with the ejector end, or be aflixed thereto; or said ejector inlet end may be formed open and have a detachable cover fitted thereto which may have the sockets or unions aforesaid integral therewith or afiixed thereto.
  • FIG. 7 is illustrated a baffle plate of copper placed over the cylinder head and used in combination with the air chamber as.
  • Z and m are respectively ribs and projections formed on and in said plate which act as guides for the air.
  • a cooling device for air cooled engines comprising a perforated air chamber adapted to be fitted over the cylinder end around the top fin, means consisting of an ejectorfitted on the end of theexhaust pipe ofthe'engine, and connected to said air chamber by suitable piping, all in, such man ner that air. is drawn from the air chamber at each exhaust stroke of the engine and is replacedby fresh air entering through the perforations in said air chamber, and a constant current of cool-air is caused to flow over thewcylinder end while the engine is working.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Exhaust Silencers (AREA)

Description

' APPLICATION FILED OCT. I8, I920.
Patented Aug. 1, 1922;;
3 SHEETS-SHEET I.
J. BOWEN.
COOLING DEVICE FOR AIR COOLED ENGINES. APPLICATION FILED 00?.18, 1920.
1 4:24:,284, Patented Aug. L 1922:.
3 SHEETS-SHEET 2- J. BOWEN. COOLING DEVICE FOR AIR COOLED ENGINES. APPLICATION FILED OCT. 18, 1920.
1 AZ LQSQ Patented Aug. 11, 1922.
3 SHEETS-SHEET 3.
JAMES BOWEN, 0F SWANSEA, WALES.
Mamas.
Specification of Letters Patent.
Patented Aug. 1, 1922.
Application filed October 18, 1920. Serial No. 417,320.
T 0 all whom it'may concern Be it known that 1, JAMES BOWEN, a subject of the King of Great Britain and Ireland, and a resident of Swansea, county of Glamorgan, South Wales, have invented a certain new and useful Improvement 111 Cooling Devices for Air-Cooled Engines, of which the following is a specification.
This invention relates to cooling devices for cooled engines, and in accordance therewith a device is provided comprising an air chamber fitted upon the top of the cylinder around the top fin, suitably perforated to permit of the passage of air from the atmosphere thereinto, and from which chamber the air is drawn through an outlet connected by piping to an ejector fitted at the end of the exhaust pipe, the exhaust gases passing through the nozzle of the ejector at a high velocity, serving to draw the air from the cooling chamber and eject same to the atmosphere; a fresh supply of air rushes into said chamber through the perforations, and a continuous flow of cool air thus passes over and around the cyln1- der head.
And in order that said invention may be fully understood, it will now be described with reference to the accompanying drawings, and figures and letters of reference marked thereon.
Figure 1 is a diagrammatic view in elevation, showing the device applied to an internal combustion engine.
Figure 2, to an enlarged scale, is a plan of the air-cooling chamber constructed in accordance with .this invention.
Figure 3 is a side elevation of same.
Figure 4 is a side elevation of an ejector adapted to be connected to the exhaust and to a pipe communicating with the cooling chamber; and,
Figure 5 shows, in sectional side elevation, another form of ejector applicable to the cooling device of this invention.
Figure 6 is an end section of same.
Figure 7 is a plan of a copper conductor placed on the cylinder head for absorbing heat therefrom and localizing same to facilitate the action of the device.
In carrying the present invention into ef feet, a cooler or air chamber a, consisting of an aluminium hollow body, made in one, two or three parts, (in the drawings see particularly Figures 2 and 3it is shown as in three sections l 2 3 to suit the design of the engine to which it is to be fitted, is attached to the cylinder head over and around the top fin b, Figure 1.
Said: hollow body is perforated as at b and c-Figures 2 and 3, to permit air to enter same and an outletcZ is provided to which is attached a tube or pipe 6 which may be flexible or rigid, and which is, at its other end, connected to an ejector 7 fixed over the end of the engine exhaust pipe 9 which ejector is formed with a socket or union h for its reception. The ejector comprises (in one form) a hollow chamber formed with a nozzle f, into which a jet 2', into which the end of the exhaust pipe 9 opens, projects and through which the exhaust gases from the engine are ejected at a high velocity, drawing with them air from the cooler at through the pipe 6, and the space around said jet in the hollow chamber I of the ejector aforesaid. A fresh supply of air rushes in through the perforations b and c in the body of cooler a at every exhaust stroke of the engine, hence a constant How of cool air is maintained over the cylinder end.
An advantageous form of ejector f is shown separately in Figures 5 and 6, wherein said ejector takes the shape of a flattened casing having its sides tapering from near the inlet end A. to the outlet B-see particularly Figure 6-in such manner that the nozzle outlet is in the form of an elongated slot 7. The jet portion z' through which the exhaust gases pass from the engine is similarly tapered at its sides j-Figure 5- and has its ends y"-Figure 6opening out fanwise from the exhaust inlet to the outlet, which latter is also in the form of an elongated slot.
At its inlet end, the ejector f is formed or fitted with sockets or unions 7t and k for connection with the pipe or tubing 6 leading from the cooling body a, and with the exhaust pipe 9 of engine respectively. Said sockets or unions may be formed integral with the ejector end, or be aflixed thereto; or said ejector inlet end may be formed open and have a detachable cover fitted thereto which may have the sockets or unions aforesaid integral therewith or afiixed thereto.
In Figure 7 is illustrated a baffle plate of copper placed over the cylinder head and used in combination with the air chamber as.
a ready absorber of the heat from the cylin der head, which is thereby concentrated for action thereupon by the flow of coo-l air through the device. Z and m are respectively ribs and projections formed on and in said plate which act as guides for the air.
I claim 1. A cooling device for air cooled engines, comprising a perforated air chamber adapted to be fitted over the cylinder end around the top fin, means consisting of an ejectorfitted on the end of theexhaust pipe ofthe'engine, and connected to said air chamber by suitable piping, all in, such man ner that air. is drawn from the air chamber at each exhaust stroke of the engine and is replacedby fresh air entering through the perforations in said air chamber, and a constant current of cool-air is caused to flow over thewcylinder end while the engine is working. V
fitted on the endof the engine exhaust pipe and communicating with the end of the tube opposite its connection'with the air chamber for the purpose of drawingair through the tube from-said chamber.
.In ,testimony whereof I have afiixedmy signature hereto this 28rd day of September 1920.
JAMES. BOWEN}
US417820A 1920-10-18 1920-10-18 Cooling device for air-cooled engines Expired - Lifetime US1424234A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US417820A US1424234A (en) 1920-10-18 1920-10-18 Cooling device for air-cooled engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US417820A US1424234A (en) 1920-10-18 1920-10-18 Cooling device for air-cooled engines

Publications (1)

Publication Number Publication Date
US1424234A true US1424234A (en) 1922-08-01

Family

ID=23655513

Family Applications (1)

Application Number Title Priority Date Filing Date
US417820A Expired - Lifetime US1424234A (en) 1920-10-18 1920-10-18 Cooling device for air-cooled engines

Country Status (1)

Country Link
US (1) US1424234A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4905633A (en) * 1987-10-16 1990-03-06 Yoshiaki Kakuta Air cooling mechanism for internal center of internal combustion engine
US4909034A (en) * 1987-12-21 1990-03-20 Yoshiaki Kakuta Low speed back pressure generator for affecting torque of an internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4905633A (en) * 1987-10-16 1990-03-06 Yoshiaki Kakuta Air cooling mechanism for internal center of internal combustion engine
US4909034A (en) * 1987-12-21 1990-03-20 Yoshiaki Kakuta Low speed back pressure generator for affecting torque of an internal combustion engine

Similar Documents

Publication Publication Date Title
US1424234A (en) Cooling device for air-cooled engines
US2372250A (en) Combined engine cooling and jet propulsion means
US2209996A (en) Internal combustion engine
KR920007889B1 (en) Air cooling mechanism for internal center of internal combustion engine
US2756730A (en) Water cooler and hot air intake assembly
US1439506A (en) Silencer of internal-combustion engines
US1938537A (en) Cooling system for aeronautical engines
US3165095A (en) Cylinder head
US2864235A (en) Exhaust gas ejector tubes in association with explosion engines or internal combustion engines
US2022982A (en) Exhaust manifold
ITMO20070072A1 (en) POWER AIR HEATER
US2439898A (en) Engine cooling system
US1546262A (en) Silencer for multicylinder internal-combustion engines
US1507950A (en) Auxiliary fuel supplier
GB1390894A (en) Aircooled reciprocating-piston internal combustion engine
US1307619A (en) of wolverhampton
US2424010A (en) Field compressor
US1635039A (en) Means for cooling heated surfaces
US1386381A (en) Cooling-jacket for internal-combustion engines
GB261232A (en) Improved method of and means for withdrawing the exhaust from internal combustion engines
US1528416A (en) Internal-combustion engine
GB642312A (en) Method and means for cooling internal-combustion engines
GB254480A (en) Improvements in or relating to water cooling radiators
US1645188A (en) Cooling system for gas engines
GB567173A (en) Improvements in or relating to cooling systems for internal combustion engines