GB1364692A - Thrust spoilers of ducted fan gas turbine engines - Google Patents

Thrust spoilers of ducted fan gas turbine engines

Info

Publication number
GB1364692A
GB1364692A GB3721171A GB3721171A GB1364692A GB 1364692 A GB1364692 A GB 1364692A GB 3721171 A GB3721171 A GB 3721171A GB 3721171 A GB3721171 A GB 3721171A GB 1364692 A GB1364692 A GB 1364692A
Authority
GB
United Kingdom
Prior art keywords
engine
panels
pylon
gas turbine
casing
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
GB3721171A
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.)
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 GB3721171A priority Critical patent/GB1364692A/en
Priority to DE2237869A priority patent/DE2237869A1/de
Priority to IT27851/72A priority patent/IT963706B/it
Priority to FR7228470A priority patent/FR2148521A1/fr
Priority to JP47079020A priority patent/JPS4827118A/ja
Publication of GB1364692A publication Critical patent/GB1364692A/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB3721171A 1971-08-07 1971-08-07 Thrust spoilers of ducted fan gas turbine engines Expired GB1364692A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB3721171A GB1364692A (en) 1971-08-07 1971-08-07 Thrust spoilers of ducted fan gas turbine engines
DE2237869A DE2237869A1 (de) 1971-08-07 1972-08-01 Mantelstromgasturbinenstrahltriebwerk
IT27851/72A IT963706B (it) 1971-08-07 1972-08-03 Variatori di spinta per motori a turbina a gas a ventola intubata
FR7228470A FR2148521A1 (enExample) 1971-08-07 1972-08-07
JP47079020A JPS4827118A (enExample) 1971-08-07 1972-08-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3721171A GB1364692A (en) 1971-08-07 1971-08-07 Thrust spoilers of ducted fan gas turbine engines

Publications (1)

Publication Number Publication Date
GB1364692A true GB1364692A (en) 1974-08-29

Family

ID=10394686

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3721171A Expired GB1364692A (en) 1971-08-07 1971-08-07 Thrust spoilers of ducted fan gas turbine engines

Country Status (5)

Country Link
JP (1) JPS4827118A (enExample)
DE (1) DE2237869A1 (enExample)
FR (1) FR2148521A1 (enExample)
GB (1) GB1364692A (enExample)
IT (1) IT963706B (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5129225A (en) * 1989-08-05 1992-07-14 Rolls-Royce Plc Diverter valve
CN108533418A (zh) * 2018-04-28 2018-09-14 上海啸风航空科技有限公司 一种新型微小型双涵道混合排气涡扇发动机

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50136982A (enExample) * 1974-04-18 1975-10-30
FR2490731B1 (fr) * 1980-09-19 1985-07-19 Snecma Dispositif d'inverseur de poussee pour turboreacteur multiflux

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5129225A (en) * 1989-08-05 1992-07-14 Rolls-Royce Plc Diverter valve
CN108533418A (zh) * 2018-04-28 2018-09-14 上海啸风航空科技有限公司 一种新型微小型双涵道混合排气涡扇发动机

Also Published As

Publication number Publication date
FR2148521A1 (enExample) 1973-03-23
IT963706B (it) 1974-01-21
JPS4827118A (enExample) 1973-04-10
DE2237869A1 (de) 1973-03-08

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees