GB2119022B - Gas turbine engine nozzle - Google Patents

Gas turbine engine nozzle

Info

Publication number
GB2119022B
GB2119022B GB08309841A GB8309841A GB2119022B GB 2119022 B GB2119022 B GB 2119022B GB 08309841 A GB08309841 A GB 08309841A GB 8309841 A GB8309841 A GB 8309841A GB 2119022 B GB2119022 B GB 2119022B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine nozzle
nozzle
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
GB08309841A
Other versions
GB8309841D0 (en
GB2119022A (en
Inventor
Gary Frank Szuminski
Douglas John Nightingale
Robert Francis Tape
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.)
Individual
Original Assignee
Individual
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
Priority claimed from US06/372,016 external-priority patent/US4502639A/en
Priority claimed from US06/372,015 external-priority patent/US4502638A/en
Application filed by Individual filed Critical Individual
Publication of GB8309841D0 publication Critical patent/GB8309841D0/en
Publication of GB2119022A publication Critical patent/GB2119022A/en
Application granted granted Critical
Publication of GB2119022B publication Critical patent/GB2119022B/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
    • F02K1/36Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/822Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infra-red radiation suppressors
    • F02K1/825Infra-red radiation suppressors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
GB08309841A 1982-04-26 1983-04-12 Gas turbine engine nozzle Expired GB2119022B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/372,016 US4502639A (en) 1982-04-26 1982-04-26 Turbomachine ejector nozzle
US06/372,015 US4502638A (en) 1982-04-26 1982-04-26 Turbomachine ejector nozzle and thrust reverser

Publications (3)

Publication Number Publication Date
GB8309841D0 GB8309841D0 (en) 1983-05-18
GB2119022A GB2119022A (en) 1983-11-09
GB2119022B true GB2119022B (en) 1985-03-13

Family

ID=27005610

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08309841A Expired GB2119022B (en) 1982-04-26 1983-04-12 Gas turbine engine nozzle

Country Status (3)

Country Link
DE (1) DE3314956C2 (en)
FR (1) FR2525688A1 (en)
GB (1) GB2119022B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3666072D1 (en) * 1986-08-18 1989-11-09 Rolls Royce Plc TURBOMACHINE EJECTOR NOZZLES
US10087884B2 (en) 2014-12-15 2018-10-02 United Technologies Corporation Stepped fairing modulated exhaust cooling

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2481330A (en) * 1946-08-06 1949-09-06 Gen Electric Variable jet nozzle
GB777803A (en) * 1953-01-15 1957-06-26 Pye Ltd Improvements in or relating to television receivers
GB833250A (en) * 1956-10-09 1960-04-21 United Aircraft Corp Variable area nozzle
US3392529A (en) * 1965-07-23 1968-07-16 Rolls Royce Aircraft provided with a gas turbine vertical lift engine
DE1481543A1 (en) * 1967-01-31 1969-10-23 Entwicklungsring Sued Gmbh Nozzle for jet engine
US3403858A (en) * 1967-03-31 1968-10-01 United Aircraft Corp Exhaust nozzle actuation system
BE755612A (en) * 1969-06-18 1971-02-15 Gen Electric PROPULSION TUBES WITH IMPROVED NOISE CANCELLATION SYSTEM
US3610533A (en) * 1970-06-29 1971-10-05 Gen Electric Variable area and thrust-reversing nozzle
US3753700A (en) * 1970-07-02 1973-08-21 Raychem Corp Heat recoverable alloy
FR2153146B1 (en) * 1971-09-20 1977-01-28 Snecma
US3747855A (en) * 1972-03-01 1973-07-24 Gen Electric Propulsion nozzles
GB1438677A (en) * 1973-07-09 1976-06-09 Snecma Variable-geometry nozzle with a muffler or silencer effect for a jet engine
SE7702923L (en) * 1976-03-17 1977-09-18 Rolls Royce 197 Ltd DEVICE AT THE NOZZLE FOR TURBOJET ENGINES

Also Published As

Publication number Publication date
FR2525688B1 (en) 1985-04-12
GB8309841D0 (en) 1983-05-18
FR2525688A1 (en) 1983-10-28
DE3314956A1 (en) 1983-11-03
DE3314956C2 (en) 1986-04-24
GB2119022A (en) 1983-11-09

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19960412