GB2263505B - Shielded vectored thrust engines - Google Patents

Shielded vectored thrust engines

Info

Publication number
GB2263505B
GB2263505B GB8035103A GB8035103A GB2263505B GB 2263505 B GB2263505 B GB 2263505B GB 8035103 A GB8035103 A GB 8035103A GB 8035103 A GB8035103 A GB 8035103A GB 2263505 B GB2263505 B GB 2263505B
Authority
GB
United Kingdom
Prior art keywords
shielded
vectored thrust
thrust engines
engines
vectored
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 - Fee Related
Application number
GB8035103A
Other versions
GB2263505A (en
Inventor
Roger Hurd
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 GB8035103A priority Critical patent/GB2263505B/en
Publication of GB2263505A publication Critical patent/GB2263505A/en
Application granted granted Critical
Publication of GB2263505B publication Critical patent/GB2263505B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F02K1/48—Corrugated nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infra-red radiation suppressors
    • F02K1/825—Infra-red radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
GB8035103A 1980-10-31 1980-10-31 Shielded vectored thrust engines Expired - Fee Related GB2263505B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8035103A GB2263505B (en) 1980-10-31 1980-10-31 Shielded vectored thrust engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8035103A GB2263505B (en) 1980-10-31 1980-10-31 Shielded vectored thrust engines

Publications (2)

Publication Number Publication Date
GB2263505A GB2263505A (en) 1993-07-28
GB2263505B true GB2263505B (en) 1994-01-26

Family

ID=10517010

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8035103A Expired - Fee Related GB2263505B (en) 1980-10-31 1980-10-31 Shielded vectored thrust engines

Country Status (1)

Country Link
GB (1) GB2263505B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5992140A (en) * 1997-06-24 1999-11-30 Sikorsky Aircraft Corporation Exhaust nozzle for suppressing infrared radiation
DE10033653A1 (en) * 2000-06-16 2002-03-07 Sandor Nagy Drive system for e.g. aircraft, is formed multistage with drives units such that the drive system is combined with at least one negative pressure system
DE10126632A1 (en) * 2000-08-08 2002-09-12 Sandor Nagy Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines
US6971240B2 (en) * 2004-03-30 2005-12-06 General Electric Company Methods and apparatus for exhausting gases from gas turbine engines
US7418813B2 (en) * 2004-12-27 2008-09-02 General Electric Company Gas turbine engine exhaust nozzle including an infrared suppression system having a plurality of U-shaped blocking fins and method of assembling said exhaut nozzle
CN115614176B (en) * 2022-08-29 2024-04-19 中国航发四川燃气涡轮研究院 Infrared and radar comprehensive stealth device based on internal and external culvert structure integration

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1110113A (en) * 1964-04-23 1968-04-18 Bristol Siddeley Engines Ltd Jet propulsion power plants
GB1231760A (en) * 1968-02-29 1971-05-12

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1110113A (en) * 1964-04-23 1968-04-18 Bristol Siddeley Engines Ltd Jet propulsion power plants
GB1231760A (en) * 1968-02-29 1971-05-12

Also Published As

Publication number Publication date
GB2263505A (en) 1993-07-28

Similar Documents

Publication Publication Date Title
DE3168335D1 (en) Noise-shielding panel for engines
GB2077360B (en) Variable geometry exhaust nozzle
JPS5741428A (en) 2-cycle engine
JPS5759053A (en) Fuel processor
DE3175723D1 (en) Extending rocket engine exhaust nozzle assembly
JPS57330A (en) Aircraft gasturbine engine
GB2015086B (en) Jet engine multiduct noise suppressor
GB2143282B (en) Ramjet missile
GB2263505B (en) Shielded vectored thrust engines
JPS56129736A (en) Combustion engine
GB2083420B (en) Disposition of engine on aircraft
JPS551483A (en) Jet engine
GB2091855B (en) Chaff rocket
JPS5744701A (en) Pinston engine
GB2301403B (en) Convergent-divergent nozzles
GB2038421B (en) Turbofan engine
GB2131883B (en) Thrust nozzle arrangement
JPS55114799A (en) Injector for backkfilling
GB2089745B (en) Thrust deflector
JPS5711201A (en) Cover for secretary part
JPS56164296A (en) Shielding structure
JPS5733706A (en) Fuel atmizer
JPS5758582A (en) Holding structure of engine for autobicycle
JPS56125689A (en) Fuel assembly
GB2265188B (en) Turbo-jet nozzle

Legal Events

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

Effective date: 19951031