GB2496999B - Transcowl assembly for gas turbine engine thrust reverser. - Google Patents

Transcowl assembly for gas turbine engine thrust reverser.

Info

Publication number
GB2496999B
GB2496999B GB201221728A GB201221728A GB2496999B GB 2496999 B GB2496999 B GB 2496999B GB 201221728 A GB201221728 A GB 201221728A GB 201221728 A GB201221728 A GB 201221728A GB 2496999 B GB2496999 B GB 2496999B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
thrust reverser
engine thrust
transcowl assembly
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 - Fee Related
Application number
GB201221728A
Other versions
GB2496999A (en
Inventor
Chi-Ling Michael Tsou
Carl Francis Holdren
William Andrew Bailey
Dean Thomas Lenahan
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to GB201221728A priority Critical patent/GB2496999B/en
Publication of GB2496999A publication Critical patent/GB2496999A/en
Application granted granted Critical
Publication of GB2496999B publication Critical patent/GB2496999B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/70—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
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/431—Rubber
GB201221728A 2008-10-31 2008-10-31 Transcowl assembly for gas turbine engine thrust reverser. Expired - Fee Related GB2496999B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB201221728A GB2496999B (en) 2008-10-31 2008-10-31 Transcowl assembly for gas turbine engine thrust reverser.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB201221728A GB2496999B (en) 2008-10-31 2008-10-31 Transcowl assembly for gas turbine engine thrust reverser.

Publications (2)

Publication Number Publication Date
GB2496999A GB2496999A (en) 2013-05-29
GB2496999B true GB2496999B (en) 2013-10-02

Family

ID=48306916

Family Applications (1)

Application Number Title Priority Date Filing Date
GB201221728A Expired - Fee Related GB2496999B (en) 2008-10-31 2008-10-31 Transcowl assembly for gas turbine engine thrust reverser.

Country Status (1)

Country Link
GB (1) GB2496999B (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
US5853148A (en) * 1995-12-19 1998-12-29 Societe De Construction Des Avions Hurel-Dubois Thrust reverser with adjustable section nozzle for aircraft jet engine
GB2395175A (en) * 2000-10-19 2004-05-19 Short Brothers Plc Aircraft engine thrust reverser
GB2443934A (en) * 2006-11-14 2008-05-21 Gen Electric A thrust reverser assembly for a turbofan engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
US5853148A (en) * 1995-12-19 1998-12-29 Societe De Construction Des Avions Hurel-Dubois Thrust reverser with adjustable section nozzle for aircraft jet engine
GB2395175A (en) * 2000-10-19 2004-05-19 Short Brothers Plc Aircraft engine thrust reverser
GB2443934A (en) * 2006-11-14 2008-05-21 Gen Electric A thrust reverser assembly for a turbofan engine

Also Published As

Publication number Publication date
GB2496999A (en) 2013-05-29

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Legal Events

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

Effective date: 20171031