GB672917A - Improvements in turbine propulsion units and aircraft fitted with same - Google Patents

Improvements in turbine propulsion units and aircraft fitted with same

Info

Publication number
GB672917A
GB672917A GB1206749A GB1206749A GB672917A GB 672917 A GB672917 A GB 672917A GB 1206749 A GB1206749 A GB 1206749A GB 1206749 A GB1206749 A GB 1206749A GB 672917 A GB672917 A GB 672917A
Authority
GB
United Kingdom
Prior art keywords
aircraft
propulsion unit
speed flight
inlet
duct
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
GB1206749A
Inventor
Frederick Francis Crocombe
Thomas George Guppy
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.)
Blackburn and General Aircraft Ltd
Original Assignee
Blackburn and General 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 Blackburn and General Aircraft Ltd filed Critical Blackburn and General Aircraft Ltd
Priority to GB1206749A priority Critical patent/GB672917A/en
Publication of GB672917A publication Critical patent/GB672917A/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)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

672,917. Air intakes for aircraft. BLACKBURN & GENERAL AIRCRAFT, Ltd. May 25, 1950 [May 5, 1949], No. 12067/49. Class 4. [Also in Group XXVI] An air intake for the turbine propulsion unit of an aircraft comprises a duct of adequate crosssectional area to supply the propulsion unit's maximum requirements, provided with one or more hinged members at the inlet thereto which is or are capable of being swung outwardly from the normal position to increase the inlet area of such duct, which is suitable for high speed flight. The arrangement ensures an adequate supply of air to the propulsion unit during low speed flight or when running on the ground. In the embodiment shown the forward portions 5, 6 of inlet ducts disposed on opposite sides of the fuselage are movable about hinges at their rearward ends by means of jacks 9, 10. The portions 5, 6 are so shaped that their leading edges define cross sectional areas suitable for high speed flight in the normal position shown in full lines. Specifications 651,436 and 672,914 are referred to.
GB1206749A 1949-05-05 1949-05-05 Improvements in turbine propulsion units and aircraft fitted with same Expired GB672917A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1206749A GB672917A (en) 1949-05-05 1949-05-05 Improvements in turbine propulsion units and aircraft fitted with same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1206749A GB672917A (en) 1949-05-05 1949-05-05 Improvements in turbine propulsion units and aircraft fitted with same

Publications (1)

Publication Number Publication Date
GB672917A true GB672917A (en) 1952-05-28

Family

ID=9997834

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1206749A Expired GB672917A (en) 1949-05-05 1949-05-05 Improvements in turbine propulsion units and aircraft fitted with same

Country Status (1)

Country Link
GB (1) GB672917A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2841346A (en) * 1952-06-30 1958-07-01 Folland Aircraft Ltd Jet-propelled aircraft
FR2560291A1 (en) * 1984-02-28 1985-08-30 Messerschmitt Boelkow Blohm DEVICE FOR IMPROVING FLOW CONDITIONS AT AIR INTAKE OF TURBO AIRCRAFT MOUNTED IN AIRCRAFT

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2841346A (en) * 1952-06-30 1958-07-01 Folland Aircraft Ltd Jet-propelled aircraft
FR2560291A1 (en) * 1984-02-28 1985-08-30 Messerschmitt Boelkow Blohm DEVICE FOR IMPROVING FLOW CONDITIONS AT AIR INTAKE OF TURBO AIRCRAFT MOUNTED IN AIRCRAFT

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