GB1541706A – Exhaust nozzles for gas turbine engines
– Google Patents
GB1541706A – Exhaust nozzles for gas turbine engines
– Google Patents
Exhaust nozzles for gas turbine engines
Info
Publication number
GB1541706A
GB1541706A
GB26094/76A
GB2609476A
GB1541706A
GB 1541706 A
GB1541706 A
GB 1541706A
GB 26094/76 A
GB26094/76 A
GB 26094/76A
GB 2609476 A
GB2609476 A
GB 2609476A
GB 1541706 A
GB1541706 A
GB 1541706A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engines
exhaust nozzles
nozzles
exhaust
Prior art date
1975-07-01
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
GB26094/76A
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.)
General Electric Co
Original Assignee
General Electric Co
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.)
1975-07-01
Filing date
1976-06-23
Publication date
1979-03-07
1976-06-23
Application filed by General Electric Co
filed
Critical
General Electric Co
1979-03-07
Publication of GB1541706A
publication
Critical
patent/GB1541706A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
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
Y—GENERAL 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
Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
Y02T50/00—Aeronautics or air transport
Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
GB26094/76A
1975-07-01
1976-06-23
Exhaust nozzles for gas turbine engines
Expired
GB1541706A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
US05/592,107
US4000611A
(en)
1975-07-01
1975-07-01
Variable area, load balancing nozzle
Publications (1)
Publication Number
Publication Date
GB1541706A
true
GB1541706A
(en)
1979-03-07
Family
ID=24369319
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB26094/76A
Expired
GB1541706A
(en)
1975-07-01
1976-06-23
Exhaust nozzles for gas turbine engines
Country Status (6)
Country
Link
US
(1)
US4000611A
(en)
JP
(1)
JPS5211315A
(en)
DE
(1)
DE2629049A1
(en)
FR
(1)
FR2316447A1
(en)
GB
(1)
GB1541706A
(en)
IT
(1)
IT1067904B
(en)
Families Citing this family (13)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US4252286A
(en)
*
1979-04-16
1981-02-24
The Boeing Company
Simplified core flow thrust control device
US4280660A
(en)
*
1979-08-17
1981-07-28
General Electric Company
Vectorable nozzle
US4449678A
(en)
*
1981-09-29
1984-05-22
The Boeing Company
Pressure balance nonaxisymmetric high aspect ratio afterburner convergent nozzle
US4451015A
(en)
*
1981-09-29
1984-05-29
The Boeing Company
Jet engine two dimensional, asymmetric afterburner nozzle
US4420932A
(en)
*
1982-03-02
1983-12-20
The United States Of America As Represented By The Secretary Of The Air Force
Pressure control system for convergent-divergent exhaust nozzle
GB2164613B
(en)
*
1984-08-16
1987-09-03
Rolls Royce
Vectorable exhaust nozzle for gas turbine engines
FR2710692B1
(en)
*
1993-09-30
1995-12-22
Europ Propulsion
Steering device in yaw or pitch of an aerospace vehicle equipped with at least one two-dimensional expansion-deflection nozzle.
FR2710693B1
(en)
*
1993-09-30
1995-12-22
Europ Propulsion
Two-dimensional detent-deflection nozzle adaptable to different flight conditions.
US5833140A
(en)
*
1996-12-12
1998-11-10
United Technologies Corporation
Variable geometry exhaust nozzle for a turbine engine
US7669785B2
(en)
*
2006-04-24
2010-03-02
The Boeing Company
Integrated engine exhaust systems and methods for drag and thermal stress reduction
US7793504B2
(en)
*
2006-05-04
2010-09-14
Rolls-Royce Corporation
Nozzle with an adjustable throat
CN108150305B
(en)
*
2018-02-05
2023-05-12
西安航空学院
Self-adaptive pulse detonation engine convergent nozzle
CN113446400B
(en)
*
2021-06-28
2022-05-31
中国空气动力研究与发展中心设备设计与测试技术研究所
Sealing system suitable for continuous wind tunnel semi-flexible wall spray pipe
Family Cites Families (9)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
DE1061569B
(en)
*
1957-11-14
1959-07-16
Bmw Triebwerkbau Ges M B H
Convergent-divergent adjustable thrust nozzle for jet engines
NL121474C
(en)
*
1959-10-05
US3380660A
(en)
*
1966-04-28
1968-04-30
United Aircraft Corp
Variable area exhaust deflector
GB1230778A
(en)
*
1967-08-15
1971-05-05
US3712062A
(en)
*
1968-04-17
1973-01-23
Gen Electric
Cooled augmentor liner
FR2123115B1
(en)
*
1971-01-08
1975-01-17
Serap
GB1444391A
(en)
*
1973-05-02
1976-07-28
Rolls Royce
Exhaust nozzle structures
US3833187A
(en)
*
1973-05-11
1974-09-03
Boeing Co
Thrust control apparatus for pod mounted engine
US3863867A
(en)
*
1973-12-26
1975-02-04
Boeing Co
Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
1975
1975-07-01
US
US05/592,107
patent/US4000611A/en
not_active
Expired – Lifetime
1976
1976-06-23
GB
GB26094/76A
patent/GB1541706A/en
not_active
Expired
1976-06-29
FR
FR7619688A
patent/FR2316447A1/en
not_active
Withdrawn
1976-06-29
DE
DE19762629049
patent/DE2629049A1/en
not_active
Withdrawn
1976-07-01
IT
IT24933/76A
patent/IT1067904B/en
active
1976-07-01
JP
JP51077119A
patent/JPS5211315A/en
active
Pending
Also Published As
Publication number
Publication date
IT1067904B
(en)
1985-03-21
US4000611A
(en)
1977-01-04
FR2316447A1
(en)
1977-01-28
DE2629049A1
(en)
1977-01-27
JPS5211315A
(en)
1977-01-28
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Legal Events
Date
Code
Title
Description
1979-05-23
PS
Patent sealed [section 19, patents act 1949]
1981-02-18
PCNP
Patent ceased through non-payment of renewal fee
