GB2042434B - Gas turbine engine gas deflection apparatus - Google Patents

Gas turbine engine gas deflection apparatus

Info

Publication number
GB2042434B
GB2042434B GB7907150A GB7907150A GB2042434B GB 2042434 B GB2042434 B GB 2042434B GB 7907150 A GB7907150 A GB 7907150A GB 7907150 A GB7907150 A GB 7907150A GB 2042434 B GB2042434 B GB 2042434B
Authority
GB
United Kingdom
Prior art keywords
gas
turbine engine
deflection apparatus
gas turbine
engine gas
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
GB7907150A
Other versions
GB2042434A (en
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB7907150A priority Critical patent/GB2042434B/en
Publication of GB2042434A publication Critical patent/GB2042434A/en
Application granted granted Critical
Publication of GB2042434B publication Critical patent/GB2042434B/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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/14—Transmitting means between initiating means and power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
GB7907150A 1979-02-28 1979-02-28 Gas turbine engine gas deflection apparatus Expired GB2042434B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7907150A GB2042434B (en) 1979-02-28 1979-02-28 Gas turbine engine gas deflection apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7907150A GB2042434B (en) 1979-02-28 1979-02-28 Gas turbine engine gas deflection apparatus

Publications (2)

Publication Number Publication Date
GB2042434A GB2042434A (en) 1980-09-24
GB2042434B true GB2042434B (en) 1982-11-17

Family

ID=10503519

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7907150A Expired GB2042434B (en) 1979-02-28 1979-02-28 Gas turbine engine gas deflection apparatus

Country Status (1)

Country Link
GB (1) GB2042434B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110615089B (en) * 2019-08-22 2022-08-05 南京航空航天大学 Roll-over control mechanism suitable for small vertical take-off and landing fixed wing aircraft

Also Published As

Publication number Publication date
GB2042434A (en) 1980-09-24

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee