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GB658931A - Improvements in or relating to power plants for the propulsion of aircraft - Google Patents

Improvements in or relating to power plants for the propulsion of aircraft

Info

Publication number
GB658931A
GB658931A GB19201/49A GB1920149A GB658931A GB 658931 A GB658931 A GB 658931A GB 19201/49 A GB19201/49 A GB 19201/49A GB 1920149 A GB1920149 A GB 1920149A GB 658931 A GB658931 A GB 658931A
Authority
GB
United Kingdom
Prior art keywords
aircraft
condenser
propulsion
relating
power plants
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
GB19201/49A
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.)
Westinghouse Electric International Co
Original Assignee
Westinghouse Electric International Co
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 Westinghouse Electric International Co filed Critical Westinghouse Electric International Co
Publication of GB658931A publication Critical patent/GB658931A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

<PICT:0658931/III/1> A fuel vapour recovery system for an aircraft gas-turbine plant consists of an air-cooled condenser 33 mounted in the forward end of the engine air inlet 11 and connected by a pipe 32 to the top of the fuel tank 31. The condenser is in the form of a number of coils connected at their lowermost points by openings 36. Condensed vapour is returned to the fuel tank through a pipe 39 fitted with a pump 40. An air vent valve 41 is fitted at the top of the condenser.
GB19201/49A 1948-08-19 1949-07-21 Improvements in or relating to power plants for the propulsion of aircraft Expired GB658931A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US658931XA 1948-08-19 1948-08-19

Publications (1)

Publication Number Publication Date
GB658931A true GB658931A (en) 1951-10-17

Family

ID=22065838

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19201/49A Expired GB658931A (en) 1948-08-19 1949-07-21 Improvements in or relating to power plants for the propulsion of aircraft

Country Status (1)

Country Link
GB (1) GB658931A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1300349B (en) * 1964-07-06 1969-07-31 Rolls Royce Deicing device for a gas turbine jet engine
US20150135726A1 (en) * 2013-11-18 2015-05-21 Unison Industries, Llc Surface Cooler Support Mechanism

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1300349B (en) * 1964-07-06 1969-07-31 Rolls Royce Deicing device for a gas turbine jet engine
US20150135726A1 (en) * 2013-11-18 2015-05-21 Unison Industries, Llc Surface Cooler Support Mechanism
US9677474B2 (en) * 2013-11-18 2017-06-13 Unison Industries, Llc Surface cooler support mechanism

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