GB2031523B - Variable area nozzle for a gas turbine engine - Google Patents

Variable area nozzle for a gas turbine engine

Info

Publication number
GB2031523B
GB2031523B GB7919772A GB7919772A GB2031523B GB 2031523 B GB2031523 B GB 2031523B GB 7919772 A GB7919772 A GB 7919772A GB 7919772 A GB7919772 A GB 7919772A GB 2031523 B GB2031523 B GB 2031523B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
variable area
area nozzle
nozzle
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
GB7919772A
Other versions
GB2031523A (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 GB7919772A priority Critical patent/GB2031523B/en
Publication of GB2031523A publication Critical patent/GB2031523A/en
Application granted granted Critical
Publication of GB2031523B publication Critical patent/GB2031523B/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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1253—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure and of a substantially axially movable external member

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
GB7919772A 1978-06-24 1979-06-06 Variable area nozzle for a gas turbine engine Expired GB2031523B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7919772A GB2031523B (en) 1978-06-24 1979-06-06 Variable area nozzle for a gas turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7827820 1978-06-24
GB7919772A GB2031523B (en) 1978-06-24 1979-06-06 Variable area nozzle for a gas turbine engine

Publications (2)

Publication Number Publication Date
GB2031523A GB2031523A (en) 1980-04-23
GB2031523B true GB2031523B (en) 1982-09-22

Family

ID=26268049

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7919772A Expired GB2031523B (en) 1978-06-24 1979-06-06 Variable area nozzle for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB2031523B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2224080B (en) * 1988-10-22 1993-04-07 Rolls Royce Plc Fluid outlet duct
GB2372779A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
US7340883B2 (en) 2004-11-12 2008-03-11 The Boeing Company Morphing structure

Also Published As

Publication number Publication date
GB2031523A (en) 1980-04-23

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Legal Events

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