GB697286A - Flexible coupling between tail cone and jet pipe of a gas turbine engine - Google Patents

Flexible coupling between tail cone and jet pipe of a gas turbine engine

Info

Publication number
GB697286A
GB697286A GB844950A GB844950A GB697286A GB 697286 A GB697286 A GB 697286A GB 844950 A GB844950 A GB 844950A GB 844950 A GB844950 A GB 844950A GB 697286 A GB697286 A GB 697286A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
jet pipe
flexible coupling
tail cone
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
GB844950A
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.)
AV Roe Canada Ltd
Original Assignee
AV Roe Canada 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 AV Roe Canada Ltd filed Critical AV Roe Canada Ltd
Priority to GB844950A priority Critical patent/GB697286A/en
Priority to US219148A priority patent/US2674844A/en
Publication of GB697286A publication Critical patent/GB697286A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04Mounting of an exhaust cone in the jet pipe
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • F02K1/80Couplings or connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

697,286. Locking nuts. BOYD, W., PASHLEY, A. E., and ROE CANADA, Ltd., A. V. April 3, 1951 [April 4, 1950], No. 8449/50. Class 89 (i) [Also in Groups XXVI and XXVIII] A nut 37 is locked in position by a spring-actuated plunger 32 having a head 36 adapted to engage projections 37a on the nut. A rivet 34 prevents the plunger from rotating.
GB844950A 1950-04-04 1950-04-04 Flexible coupling between tail cone and jet pipe of a gas turbine engine Expired GB697286A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB844950A GB697286A (en) 1950-04-04 1950-04-04 Flexible coupling between tail cone and jet pipe of a gas turbine engine
US219148A US2674844A (en) 1950-04-04 1951-04-04 Flexible coupling between tail cone and jet pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB844950A GB697286A (en) 1950-04-04 1950-04-04 Flexible coupling between tail cone and jet pipe of a gas turbine engine

Publications (1)

Publication Number Publication Date
GB697286A true GB697286A (en) 1953-09-16

Family

ID=9852698

Family Applications (1)

Application Number Title Priority Date Filing Date
GB844950A Expired GB697286A (en) 1950-04-04 1950-04-04 Flexible coupling between tail cone and jet pipe of a gas turbine engine

Country Status (1)

Country Link
GB (1) GB697286A (en)

Similar Documents

Publication Publication Date Title
GB627832A (en) Improvement in propulsion plant comprising a gas turbine driven airscrew
GB654344A (en) Method of regulating gas turbine jet-propulsion plants, and means therefor
GB586572A (en) Improvements in internal combustion turbine plant for propulsion by jet action, at least in part
GB622627A (en) Means for preventing an internal-combustion turbine unit from icing
GB697286A (en) Flexible coupling between tail cone and jet pipe of a gas turbine engine
GB907741A (en) Improvements relating to rockets
GB602584A (en) Improvements in or relating to internal combustion turbine power plants
GB847500A (en) Improvements in piping systems or channels for the passage of fluids
GB770004A (en) Means for mounting a rotor on a shaft
GB587512A (en) Improvements relating to exhaust systems of jet propulsion installations in aircraft
GB937024A (en) Arrangement for preventing icing at air intakes or like apertures in aircraft
GB603283A (en) Improvements in or relating to internal combustion turbine power plants
GB1127653A (en) Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner
GB632049A (en) Improvements in or relating to pipe joints
GB649375A (en) Improvements in or relating to gas-turbine engines
GB588092A (en) Improvements in or relating to internal combustion turbine power plants
GB679530A (en) Improvements in gas turbine blades
GB588085A (en) Improvements relating to propulsive thrust augmentors
GB579140A (en) Improvements in or relating to gas turbines
GB750490A (en) Co-ordinated fuel feed and exhaust jet control for gas turbine engines
GB659604A (en) Adjutage for the nozzles of radial impulse turbines
GB715133A (en) Improvements in or relating to reverse-thrust and/or torque sensitive devices
GB584169A (en) Improvements in or relating to power plants for aircraft
GB703701A (en) Fuel supply means for a gas turbine engine
GB550844A (en) Improvements in reaction propulsion engines