GB1132157A - Improvements in movable nozzles for directing the thrust of jet-propelled aircraft - Google Patents

Improvements in movable nozzles for directing the thrust of jet-propelled aircraft

Info

Publication number
GB1132157A
GB1132157A GB1710266A GB1710266A GB1132157A GB 1132157 A GB1132157 A GB 1132157A GB 1710266 A GB1710266 A GB 1710266A GB 1710266 A GB1710266 A GB 1710266A GB 1132157 A GB1132157 A GB 1132157A
Authority
GB
United Kingdom
Prior art keywords
aircraft
nozzle
contour
requires
skin
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
GB1710266A
Other languages
English (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.)
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.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of GB1132157A publication Critical patent/GB1132157A/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
    • F02K1/002—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
    • F02K1/004—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 by using one or more swivable nozzles rotating about their own axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
GB1710266A 1965-04-19 1966-04-19 Improvements in movable nozzles for directing the thrust of jet-propelled aircraft Expired GB1132157A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US44903465A 1965-04-19 1965-04-19

Publications (1)

Publication Number Publication Date
GB1132157A true GB1132157A (en) 1968-10-30

Family

ID=23782608

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1710266A Expired GB1132157A (en) 1965-04-19 1966-04-19 Improvements in movable nozzles for directing the thrust of jet-propelled aircraft

Country Status (7)

Country Link
BE (1) BE679612A (enrdf_load_stackoverflow)
CH (1) CH456357A (enrdf_load_stackoverflow)
DE (1) DE1481554A1 (enrdf_load_stackoverflow)
FR (1) FR1506309A (enrdf_load_stackoverflow)
GB (1) GB1132157A (enrdf_load_stackoverflow)
NL (1) NL6605188A (enrdf_load_stackoverflow)
SE (1) SE313741B (enrdf_load_stackoverflow)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5042746A (en) * 1988-06-01 1991-08-27 British Aerospace Public Limited Company Nozzle assembly for aircraft
CN104875898A (zh) * 2015-06-23 2015-09-02 中国航空工业集团公司西安飞机设计研究所 一种飞机用尾部喷管组件及具有其的飞机
CN111237083A (zh) * 2018-11-28 2020-06-05 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4478377A (en) * 1980-12-22 1984-10-23 British Aerospace Public Limited Company Aircraft
GB2188887B (en) * 1986-04-08 1989-11-29 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5042746A (en) * 1988-06-01 1991-08-27 British Aerospace Public Limited Company Nozzle assembly for aircraft
CN104875898A (zh) * 2015-06-23 2015-09-02 中国航空工业集团公司西安飞机设计研究所 一种飞机用尾部喷管组件及具有其的飞机
CN111237083A (zh) * 2018-11-28 2020-06-05 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机

Also Published As

Publication number Publication date
FR1506309A (fr) 1967-12-22
BE679612A (enrdf_load_stackoverflow) 1966-09-16
NL6605188A (enrdf_load_stackoverflow) 1966-10-20
CH456357A (de) 1968-07-15
SE313741B (enrdf_load_stackoverflow) 1969-08-18
DE1481554A1 (de) 1970-01-22

Similar Documents

Publication Publication Date Title
GB1040510A (en) Improvements in jet propulsion engines having thrust deflectors
GB848679A (en) Noise suppressor and thrust reverser for aircraft jet engines
GB933612A (en) Jet engine thrust reversers
GB1448017A (en) Aircraft having jet lift ejector means
GB1179788A (en) Variable Area Exhaust Deflection System for a Gas Turbine Engine
GB1258202A (enrdf_load_stackoverflow)
GB976449A (en) Improvements in thrust vectoring and modulating device
GB1132157A (en) Improvements in movable nozzles for directing the thrust of jet-propelled aircraft
GB1161949A (en) Improvements in Aircraft Gas Generator Exhaust Nozzle Structures
GB1170809A (en) Discharge Nozzle Apparatus for Jet Aircraft
GB1055607A (en) Supersonic intake for a jet engine
GB1139005A (en) Improvements in or relating to gas turbine by-pass engines
GB1448245A (en) Combination jet engine clam-shell thrust reverser and variable nozzle area ramp
GB1114478A (en) Jet propulsion nozzle having a central bulbous body
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
GB1387160A (en) Exhaust nozzles for jet propulsion engines for supersonic aircraft or vehicles
GB1033583A (en) Thrust reverser for a jet propulsion engine
GB1117266A (en) Supersonic intake for a jet propulsion engine
GB1101663A (en) Variable area nozzles for jet propulsion engines
GB1167039A (en) Jet Propulsion Engine Thrust Deflector.
GB1142660A (en) Improvements in combination jet exhaust nozzle and thrust reverser
GB1071075A (en) Improvements in aircraft
GB859993A (en) Retractable noise suppressor for jet propulsion engines
GB1357370A (en) Ducted fan gas turbine jet propulsion engine with thrust control means
GB908479A (en) Improvements in reingestion control means