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
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 DE19722237869 priority patent/DE2237869A1/en
Priority to IT2785172A priority patent/IT963706B/en
Priority to FR7228470A priority patent/FR2148521A1/fr
Priority to JP7902072A 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)

Abstract

1364692 Aircraft ducted fan gas turbine engines ROLLS-ROYCE (1971) Ltd 7 Aug 1971 37211/71 Heading B7G A ducted fan gas turbine engine on an aerodynamic shaped pylon 28 has an engine casing 12 formed partly with at least one panel 34 pivotable to deflect air from the ducted fan 20 of the engine, e.g. air expelled from the fan duct 18, the pivoting of the or each panel 34 being outwardly of the casing about a pivot 45 joining the upstream edge of the or each panel with said pylon 28. In the embodiment shown the engine is mounted on a pylon forming the aerofoil 28 which depends from an aircraft wing 30, two panels being provided one on each side of the casing and an elongate strut 32 being fixed to and lying between the fan duct cowl and the engine casing. Also further pivots 46 are provided to join the strut with the respective panels. Flanges (56, 58), Fig. 3 (not shown), may extend from the edges of the panels normally thereof to provide a degree of reverse thrust. In a further embodiment, Fig. 4, (not shown), the engine is wing mounted without a pylon, the pivots joining the panels to the wing. The profile of the panels is preferably the same as that of the outlet nozzle of the cold fan.
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
DE19722237869 DE2237869A1 (en) 1971-08-07 1972-08-01 CASE-FLOW GAS TURBINE JET
IT2785172A IT963706B (en) 1971-08-07 1972-08-03 THRUST VARIATORS FOR DUCTED FAN GAS TURBINE ENGINES
FR7228470A FR2148521A1 (en) 1971-08-07 1972-08-07
JP7902072A JPS4827118A (en) 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 (en)
DE (1) DE2237869A1 (en)
FR (1) FR2148521A1 (en)
GB (1) GB1364692A (en)
IT (1) IT963706B (en)

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 (en) * 2018-04-28 2018-09-14 上海啸风航空科技有限公司 A kind of double duct mixing exhaust fanjets of novel microminiature

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50136982A (en) * 1974-04-18 1975-10-30
FR2490731B1 (en) * 1980-09-19 1985-07-19 Snecma PUSH INVERTER DEVICE FOR MULTIFLUX TURBOREACTOR
DE102020117993A1 (en) 2020-07-08 2022-01-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. Jet engine with pylon deployable thrust reverser flaps

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 (en) * 2018-04-28 2018-09-14 上海啸风航空科技有限公司 A kind of double duct mixing exhaust fanjets of novel microminiature

Also Published As

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

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Legal Events

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