GB1388406A - Gas turbine ducted fan engines - Google Patents

Gas turbine ducted fan engines

Info

Publication number
GB1388406A
GB1388406A GB5818571A GB5818571A GB1388406A GB 1388406 A GB1388406 A GB 1388406A GB 5818571 A GB5818571 A GB 5818571A GB 5818571 A GB5818571 A GB 5818571A GB 1388406 A GB1388406 A GB 1388406A
Authority
GB
United Kingdom
Prior art keywords
cowl
vanes
exposes
duct
fan
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
GB5818571A
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 GB5818571A priority Critical patent/GB1388406A/en
Priority to DE19722261025 priority patent/DE2261025A1/de
Priority to IT3288872A priority patent/IT971846B/it
Priority to JP12605672A priority patent/JPS4891414A/ja
Priority to FR7244797A priority patent/FR2163688B1/fr
Publication of GB1388406A publication Critical patent/GB1388406A/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

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)
  • Control Of Turbines (AREA)
GB5818571A 1971-12-15 1971-12-15 Gas turbine ducted fan engines Expired GB1388406A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB5818571A GB1388406A (en) 1971-12-15 1971-12-15 Gas turbine ducted fan engines
DE19722261025 DE2261025A1 (de) 1971-12-15 1972-12-13 Mantelstromgasturbinenstrahltriebwerk
IT3288872A IT971846B (it) 1971-12-15 1972-12-14 Motori a turbina a gas a ventola intubata
JP12605672A JPS4891414A (cg-RX-API-DMAC7.html) 1971-12-15 1972-12-15
FR7244797A FR2163688B1 (cg-RX-API-DMAC7.html) 1971-12-15 1972-12-15

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5818571A GB1388406A (en) 1971-12-15 1971-12-15 Gas turbine ducted fan engines

Publications (1)

Publication Number Publication Date
GB1388406A true GB1388406A (en) 1975-03-26

Family

ID=10480969

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5818571A Expired GB1388406A (en) 1971-12-15 1971-12-15 Gas turbine ducted fan engines

Country Status (5)

Country Link
JP (1) JPS4891414A (cg-RX-API-DMAC7.html)
DE (1) DE2261025A1 (cg-RX-API-DMAC7.html)
FR (1) FR2163688B1 (cg-RX-API-DMAC7.html)
GB (1) GB1388406A (cg-RX-API-DMAC7.html)
IT (1) IT971846B (cg-RX-API-DMAC7.html)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2311968A (en) * 1996-04-12 1997-10-15 Robert Geoffrey Marshall Gas turbine jet pipe blocker valve
FR2871776A1 (fr) * 2004-06-21 2005-12-23 Snecma Moteurs Sa Procede de freinage d'un avion et turboreacteur a double flux pour la mise en oeuvre du procede
RU2538348C2 (ru) * 2009-11-05 2015-01-10 Эрсель Устройство реверса тяги
RU2656169C1 (ru) * 2017-05-24 2018-05-31 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Устройство для перекрытия газового потока в корпусе турбореактивного двигателя
RU2688642C1 (ru) * 2018-06-07 2019-05-21 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Реверсивное устройство турбореактивного двигателя
RU2711743C2 (ru) * 2018-06-07 2020-01-21 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Устройство отклонения вектора реверсированной тяги турбореактивного двигателя

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996002746A1 (en) * 1994-07-14 1996-02-01 Grumman Aerospace Corporation Thrust reverser
CN110230552B (zh) * 2018-03-06 2020-05-12 中国航发商用航空发动机有限责任公司 阻流支板式反推装置及包括其的发动机

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
GB1197028A (en) * 1968-10-24 1970-07-01 Rolls Royce Thrust Reverser for Jet-Propulsion Engines
US3599432A (en) * 1970-04-02 1971-08-17 Rohr Corp Thrust reversing apparatus for turbo-fan propulsion unit

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2311968A (en) * 1996-04-12 1997-10-15 Robert Geoffrey Marshall Gas turbine jet pipe blocker valve
FR2871776A1 (fr) * 2004-06-21 2005-12-23 Snecma Moteurs Sa Procede de freinage d'un avion et turboreacteur a double flux pour la mise en oeuvre du procede
EP1609719A1 (fr) * 2004-06-21 2005-12-28 Snecma Procédé de freinage d'un avion et turboréacteur à double flux pour la mise en oeuvre du procédé
US7469528B2 (en) 2004-06-21 2008-12-30 Snecma Aircraft braking method and ducted fan jet engine for implementing the method
RU2415287C2 (ru) * 2004-06-21 2011-03-27 Снекма Двухконтурный турбовентиляторный двигатель
RU2538348C2 (ru) * 2009-11-05 2015-01-10 Эрсель Устройство реверса тяги
RU2656169C1 (ru) * 2017-05-24 2018-05-31 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Устройство для перекрытия газового потока в корпусе турбореактивного двигателя
RU2688642C1 (ru) * 2018-06-07 2019-05-21 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Реверсивное устройство турбореактивного двигателя
RU2711743C2 (ru) * 2018-06-07 2020-01-21 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Устройство отклонения вектора реверсированной тяги турбореактивного двигателя

Also Published As

Publication number Publication date
JPS4891414A (cg-RX-API-DMAC7.html) 1973-11-28
FR2163688B1 (cg-RX-API-DMAC7.html) 1977-12-23
FR2163688A1 (cg-RX-API-DMAC7.html) 1973-07-27
IT971846B (it) 1974-05-10
DE2261025A1 (de) 1973-07-05

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees