GB1252077A - - Google Patents

Info

Publication number
GB1252077A
GB1252077A GB1233869A GB1252077DA GB1252077A GB 1252077 A GB1252077 A GB 1252077A GB 1233869 A GB1233869 A GB 1233869A GB 1252077D A GB1252077D A GB 1252077DA GB 1252077 A GB1252077 A GB 1252077A
Authority
GB
United Kingdom
Prior art keywords
nozzles
duct
nozzle
terminating
aircraft
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
GB1233869A
Other languages
English (en)
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 filed Critical
Publication of GB1252077A publication Critical patent/GB1252077A/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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB1233869A 1969-03-08 1969-03-08 Expired GB1252077A (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1233869 1969-03-08

Publications (1)

Publication Number Publication Date
GB1252077A true GB1252077A (enExample) 1971-11-03

Family

ID=10002660

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1233869A Expired GB1252077A (enExample) 1969-03-08 1969-03-08

Country Status (1)

Country Link
GB (1) GB1252077A (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3520015A1 (de) * 1985-06-04 1987-01-08 Gerhard Nerenberg Duesenanordnung bei einem triebwerk
GB2231009A (en) * 1984-11-17 1990-11-07 Rolls Royce Diverter valve with bypass duct obturator for twin gas turbine engine installation
US4979363A (en) * 1984-11-17 1990-12-25 Rolls-Royce Plc Diverter valve with bypass duct obturator
GB2391846A (en) * 2002-06-28 2004-02-18 Ashley Christopher Bryant Ducted air power plant

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2231009A (en) * 1984-11-17 1990-11-07 Rolls Royce Diverter valve with bypass duct obturator for twin gas turbine engine installation
US4979363A (en) * 1984-11-17 1990-12-25 Rolls-Royce Plc Diverter valve with bypass duct obturator
GB2231009B (en) * 1984-11-17 1991-01-23 Rolls Royce Diverter valve with bypass duct obturator
DE3520015A1 (de) * 1985-06-04 1987-01-08 Gerhard Nerenberg Duesenanordnung bei einem triebwerk
GB2391846A (en) * 2002-06-28 2004-02-18 Ashley Christopher Bryant Ducted air power plant
GB2391846B (en) * 2002-06-28 2005-10-05 Ashley Christopher Bryant Ducted air power plant
US7581381B2 (en) 2002-06-28 2009-09-01 Vtol Technologies Limited Ducted air power plant

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Legal Events

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