GB717760A - Improvements in or relating to air intakes for jet propulsion engines - Google Patents

Improvements in or relating to air intakes for jet propulsion engines

Info

Publication number
GB717760A
GB717760A GB2359251A GB2359251A GB717760A GB 717760 A GB717760 A GB 717760A GB 2359251 A GB2359251 A GB 2359251A GB 2359251 A GB2359251 A GB 2359251A GB 717760 A GB717760 A GB 717760A
Authority
GB
United Kingdom
Prior art keywords
jet propulsion
oct
relating
aircraft
air
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
GB2359251A
Inventor
Charles Vivian Kenmir
Peter Latham Sutcliffe
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.)
Boulton Paul Aircraft Ltd
Original Assignee
Boulton Paul Aircraft Ltd
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 Boulton Paul Aircraft Ltd filed Critical Boulton Paul Aircraft Ltd
Priority to GB2359251A priority Critical patent/GB717760A/en
Publication of GB717760A publication Critical patent/GB717760A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

717,760. Jet propulsion plant. BOULTON PAUL AIRCRAFT, Ltd. Oct. 9, 1952 (Oct. 10, 1951], No. 23592/51. Class 110(3) An air intake duct 1 for a jet propulsion engine comprises a front portion 3 normally in sealing contact with a rear portion but movable forwardly to define a slot 6 which is at an angle to the centre line of said duct and trailing with respect to the direction of flow of air therethrough. The member 3 is slidably mounted on guides 4 and is actuated by hydraulic jacks 5 or screwthreaded actuators driven by electric motors. The member 3 is of plastic or light alloy construction and may house a radar scanner 7. Actuation of the member 3 may be controlled automatically by a power unit responsive to the air speed or Mach number of the aircraft.
GB2359251A 1951-10-10 1951-10-10 Improvements in or relating to air intakes for jet propulsion engines Expired GB717760A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2359251A GB717760A (en) 1951-10-10 1951-10-10 Improvements in or relating to air intakes for jet propulsion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2359251A GB717760A (en) 1951-10-10 1951-10-10 Improvements in or relating to air intakes for jet propulsion engines

Publications (1)

Publication Number Publication Date
GB717760A true GB717760A (en) 1954-11-03

Family

ID=10198170

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2359251A Expired GB717760A (en) 1951-10-10 1951-10-10 Improvements in or relating to air intakes for jet propulsion engines

Country Status (1)

Country Link
GB (1) GB717760A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078375B (en) * 1958-08-08 1960-03-24 Ernst Heinkel Flugzeugbau G M Adjustable air intake especially for jet engines
US2999656A (en) * 1958-08-15 1961-09-12 Rolls Royce Gas turbine engine with canted variable gap augmentary intake
DE1121414B (en) * 1958-07-24 1962-01-04 Ernst Heinkel Flugzeugbau G M Device for controlling additional air in a jet engine
US3058693A (en) * 1960-02-02 1962-10-16 Edmond R Doak Means to supplement the normal thrust of a high speed aircraft at low speed
DE1139701B (en) * 1958-08-15 1962-11-15 Rolls Royce Gas turbine jet engine
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit
EP3388649B1 (en) * 2017-03-31 2021-05-05 Rolls-Royce Deutschland Ltd & Co KG Nacelle for a turbofan engine

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1121414B (en) * 1958-07-24 1962-01-04 Ernst Heinkel Flugzeugbau G M Device for controlling additional air in a jet engine
DE1078375B (en) * 1958-08-08 1960-03-24 Ernst Heinkel Flugzeugbau G M Adjustable air intake especially for jet engines
US2999656A (en) * 1958-08-15 1961-09-12 Rolls Royce Gas turbine engine with canted variable gap augmentary intake
DE1139701B (en) * 1958-08-15 1962-11-15 Rolls Royce Gas turbine jet engine
US3058693A (en) * 1960-02-02 1962-10-16 Edmond R Doak Means to supplement the normal thrust of a high speed aircraft at low speed
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit
GB2274490B (en) * 1993-01-26 1996-09-18 Short Brothers Plc An aircraft propulsive power unit
US5609313A (en) * 1993-01-26 1997-03-11 Short Brothers Plc Aircraft propulsive power unit
EP3388649B1 (en) * 2017-03-31 2021-05-05 Rolls-Royce Deutschland Ltd & Co KG Nacelle for a turbofan engine
US11149637B2 (en) 2017-03-31 2021-10-19 Rolls-Royce Deutschland Ltd & Co Kg Nacelle for a turbofan engine

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