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GB1551216A - Nozzles for gas turbine engines - Google Patents

Nozzles for gas turbine engines

Info

Publication number
GB1551216A
GB1551216A GB1933175A GB1933175A GB1551216A GB 1551216 A GB1551216 A GB 1551216A GB 1933175 A GB1933175 A GB 1933175A GB 1933175 A GB1933175 A GB 1933175A GB 1551216 A GB1551216 A GB 1551216A
Authority
GB
United Kingdom
Prior art keywords
nozzles
gas turbine
turbine engines
engines
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
GB1933175A
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 GB1933175A priority Critical patent/GB1551216A/en
Priority to DE19762620098 priority patent/DE2620098A1/en
Publication of GB1551216A publication Critical patent/GB1551216A/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
    • F02K1/1207—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
GB1933175A 1975-05-08 1975-05-08 Nozzles for gas turbine engines Expired GB1551216A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB1933175A GB1551216A (en) 1975-05-08 1975-05-08 Nozzles for gas turbine engines
DE19762620098 DE2620098A1 (en) 1975-05-08 1976-05-06 ADJUSTABLE THROTTLE FOR GAS TURBINE ENGINES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1933175A GB1551216A (en) 1975-05-08 1975-05-08 Nozzles for gas turbine engines

Publications (1)

Publication Number Publication Date
GB1551216A true GB1551216A (en) 1979-08-22

Family

ID=10127566

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1933175A Expired GB1551216A (en) 1975-05-08 1975-05-08 Nozzles for gas turbine engines

Country Status (2)

Country Link
DE (1) DE2620098A1 (en)
GB (1) GB1551216A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4311276A (en) * 1978-06-24 1982-01-19 Rolls-Royce Limited Variable area nozzle for a gas turbine engine
GB2588653A (en) * 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
US11306680B2 (en) 2019-10-31 2022-04-19 Rolls-Royce Plc Exhaust nozzle
US11473526B2 (en) 2019-10-31 2022-10-18 Rolls-Royce Plc Exhaust nozzle
CN116838498A (en) * 2023-07-27 2023-10-03 西北工业大学 S-bend spray pipe comprising web type bearing structure and application

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4311276A (en) * 1978-06-24 1982-01-19 Rolls-Royce Limited Variable area nozzle for a gas turbine engine
GB2588653A (en) * 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
US11306680B2 (en) 2019-10-31 2022-04-19 Rolls-Royce Plc Exhaust nozzle
US11319896B2 (en) 2019-10-31 2022-05-03 Rolls-Royce Plc Exhaust nozzle
US11473526B2 (en) 2019-10-31 2022-10-18 Rolls-Royce Plc Exhaust nozzle
CN116838498A (en) * 2023-07-27 2023-10-03 西北工业大学 S-bend spray pipe comprising web type bearing structure and application

Also Published As

Publication number Publication date
DE2620098A1 (en) 1976-11-18

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Legal Events

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