GB2009063B - Ducted fan gas turbine engine - Google Patents

Ducted fan gas turbine engine

Info

Publication number
GB2009063B
GB2009063B GB7840911A GB7840911A GB2009063B GB 2009063 B GB2009063 B GB 2009063B GB 7840911 A GB7840911 A GB 7840911A GB 7840911 A GB7840911 A GB 7840911A GB 2009063 B GB2009063 B GB 2009063B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
ducted fan
fan gas
ducted
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
GB7840911A
Other versions
GB2009063A (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 GB7840911A priority Critical patent/GB2009063B/en
Publication of GB2009063A publication Critical patent/GB2009063A/en
Application granted granted Critical
Publication of GB2009063B publication Critical patent/GB2009063B/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
    • F02K1/56—Reversing jet main flow
    • F02K1/566—Reversing jet main flow by blocking the rearward discharge by means of a translatable member
    • 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
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine

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)
GB7840911A 1977-11-29 1978-10-17 Ducted fan gas turbine engine Expired GB2009063B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7840911A GB2009063B (en) 1977-11-29 1978-10-17 Ducted fan gas turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB4953577 1977-11-29
GB7840911A GB2009063B (en) 1977-11-29 1978-10-17 Ducted fan gas turbine engine

Publications (2)

Publication Number Publication Date
GB2009063A GB2009063A (en) 1979-06-13
GB2009063B true GB2009063B (en) 1982-03-03

Family

ID=26266506

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7840911A Expired GB2009063B (en) 1977-11-29 1978-10-17 Ducted fan gas turbine engine

Country Status (1)

Country Link
GB (1) GB2009063B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2669679B1 (en) * 1990-11-28 1994-04-29 Sud Ouest Conception Aeronauti GAS EJECTION NOZZLE FOR A REACTION ENGINE AND A REACTION ENGINE EQUIPPED WITH SUCH A NOZZLE, PARTICULARLY A SEPARATE FLOW TYPE ENGINE.
US8469148B2 (en) 2010-02-22 2013-06-25 Calvidge C. Perry Ladder tray

Also Published As

Publication number Publication date
GB2009063A (en) 1979-06-13

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Legal Events

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