GB475329A - Improvements in and relating to the charging of internal combustion engines for aircraft - Google Patents

Improvements in and relating to the charging of internal combustion engines for aircraft

Info

Publication number
GB475329A
GB475329A GB14169/37A GB1416937A GB475329A GB 475329 A GB475329 A GB 475329A GB 14169/37 A GB14169/37 A GB 14169/37A GB 1416937 A GB1416937 A GB 1416937A GB 475329 A GB475329 A GB 475329A
Authority
GB
United Kingdom
Prior art keywords
pump
pitch
engine
propeller blades
charging
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
Application number
GB14169/37A
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.)
Airbus Defence and Space GmbH
Junkers Flugzeug und Motorenwerke AG
Original Assignee
Messerschmitt Bolkow Blohm AG
Junkers Flugzeug und Motorenwerke AG
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 Messerschmitt Bolkow Blohm AG, Junkers Flugzeug und Motorenwerke AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB475329A publication Critical patent/GB475329A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
    • F02D2700/07—Automatic control systems according to one of the preceding groups in combination with control of the mechanism receiving the engine power

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Rotary Pumps (AREA)

Abstract

475,329. Regulating. JUNKERS FLUGZEUG - UND - MOTORENWERKE AKT.-GES. May 21, 1937, No. 14169. Convention date, May 22, 1936. [Class 7 (vi)] [Also in Group XXIX] In aircraft engines charged by a pump driven by the engine, the temperature of the charge delivered by the pump is maintained substantially constant by adjustment of the pitch of the propeller blades by means of a thermostatic device arranged in the pumpdelivering conduit. When the temperature of the charge rises too high, the pitch of the propeller blades is increased so as to reduce the speed of the engine and pump, and vice versa, The Figure shows an engine 20 driving a charging-pump 30, in the delivery pipe of which is arranged a heat-sensitive member 32 actuating, through a capsule 33, the valve 16 of a servomotor piston 11 which adjusts the pitch of the propeller blades through racks 8, 9 and pinions 6, 7.
GB14169/37A 1936-05-22 1937-05-21 Improvements in and relating to the charging of internal combustion engines for aircraft Expired GB475329A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE475329X 1936-05-22

Publications (1)

Publication Number Publication Date
GB475329A true GB475329A (en) 1937-11-17

Family

ID=6541830

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14169/37A Expired GB475329A (en) 1936-05-22 1937-05-21 Improvements in and relating to the charging of internal combustion engines for aircraft

Country Status (1)

Country Link
GB (1) GB475329A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2453651A (en) * 1942-04-27 1948-11-09 Bendix Aviat Corp Control for internal-combustion engines
US2501994A (en) * 1940-04-09 1950-03-28 Dewey David Brainard Control means for regulating feathering members
US2683493A (en) * 1949-05-04 1954-07-13 Bristol Aeroplane Co Ltd Valve means for controlling hydraulically operated propeller pitch change mechanism

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2501994A (en) * 1940-04-09 1950-03-28 Dewey David Brainard Control means for regulating feathering members
US2453651A (en) * 1942-04-27 1948-11-09 Bendix Aviat Corp Control for internal-combustion engines
US2683493A (en) * 1949-05-04 1954-07-13 Bristol Aeroplane Co Ltd Valve means for controlling hydraulically operated propeller pitch change mechanism

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