GB8903673D0 - An exhaust nozzle for a gas turbine aeroengine - Google Patents

An exhaust nozzle for a gas turbine aeroengine

Info

Publication number
GB8903673D0
GB8903673D0 GBGB8903673.5A GB8903673A GB8903673D0 GB 8903673 D0 GB8903673 D0 GB 8903673D0 GB 8903673 A GB8903673 A GB 8903673A GB 8903673 D0 GB8903673 D0 GB 8903673D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
exhaust nozzle
turbine aeroengine
aeroengine
exhaust
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.)
Granted
Application number
GBGB8903673.5A
Other versions
GB2435676A (en
GB2435676B (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 GB8903673A priority Critical patent/GB2435676B/en
Priority to DE19904004919 priority patent/DE4004919A1/en
Priority to FR9001869A priority patent/FR2894630A1/en
Publication of GB8903673D0 publication Critical patent/GB8903673D0/en
Publication of GB2435676A publication Critical patent/GB2435676A/en
Application granted granted Critical
Publication of GB2435676B publication Critical patent/GB2435676B/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • 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
    • 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
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • F02K1/085—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone by transversely deforming an internal member
GB8903673A 1989-02-17 1989-02-17 An exhaust nozzle for a gas turbine aeroengine Expired - Lifetime GB2435676B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB8903673A GB2435676B (en) 1989-02-17 1989-02-17 An exhaust nozzle for a gas turbine aeroengine
DE19904004919 DE4004919A1 (en) 1989-02-17 1990-02-16 Jet nozzle for an aircraft gas turbine engine
FR9001869A FR2894630A1 (en) 1989-02-17 1990-02-16 Turbojet ejector nozzle for aircraft, especially of vertical take-off or landing type, has transversely movable shutter projecting through ejector opening, to vary distribution, width and aeration of ejection section

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8903673A GB2435676B (en) 1989-02-17 1989-02-17 An exhaust nozzle for a gas turbine aeroengine

Publications (3)

Publication Number Publication Date
GB8903673D0 true GB8903673D0 (en) 2007-04-11
GB2435676A GB2435676A (en) 2007-09-05
GB2435676B GB2435676B (en) 2008-01-09

Family

ID=37966093

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8903673A Expired - Lifetime GB2435676B (en) 1989-02-17 1989-02-17 An exhaust nozzle for a gas turbine aeroengine

Country Status (3)

Country Link
DE (1) DE4004919A1 (en)
FR (1) FR2894630A1 (en)
GB (1) GB2435676B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105697191B (en) * 2014-11-28 2017-11-10 中国航空工业集团公司沈阳发动机设计研究所 A kind of Novel Dual plug nozzle
PL423418A1 (en) * 2017-11-12 2019-05-20 Bryzik Grzegorz Driving unit of a flying vehicle

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB861819A (en) * 1957-07-29 1961-03-01 Boeing Co Noise suppressor and thrust reverser for jet propulsion engines

Also Published As

Publication number Publication date
FR2894630A1 (en) 2007-06-15
DE4004919A1 (en) 2009-02-26
GB2435676A (en) 2007-09-05
GB2435676B (en) 2008-01-09

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20090216