FR2079257B1 - - Google Patents

Info

Publication number
FR2079257B1
FR2079257B1 FR7103692A FR7103692A FR2079257B1 FR 2079257 B1 FR2079257 B1 FR 2079257B1 FR 7103692 A FR7103692 A FR 7103692A FR 7103692 A FR7103692 A FR 7103692A FR 2079257 B1 FR2079257 B1 FR 2079257B1
Authority
FR
France
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
FR7103692A
Other languages
French (fr)
Other versions
FR2079257A1 (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
Publication of FR2079257A1 publication Critical patent/FR2079257A1/fr
Application granted granted Critical
Publication of FR2079257B1 publication Critical patent/FR2079257B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
FR7103692A 1970-02-05 1971-02-04 Expired FR2079257B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB547670 1970-02-05

Publications (2)

Publication Number Publication Date
FR2079257A1 FR2079257A1 (en) 1971-11-12
FR2079257B1 true FR2079257B1 (en) 1975-06-06

Family

ID=9796916

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7103692A Expired FR2079257B1 (en) 1970-02-05 1971-02-04

Country Status (4)

Country Link
US (1) US3684857A (en)
DE (1) DE2103035C3 (en)
FR (1) FR2079257B1 (en)
GB (1) GB1328993A (en)

Families Citing this family (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2069053B (en) * 1980-02-09 1983-04-13 Rolls Royce Water separator in gas turbine inlet
GB2069054B (en) * 1980-02-09 1983-06-02 Rolls Royce Water separator gas turbine engine intake
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
EP1828547B1 (en) 2004-12-01 2011-11-30 United Technologies Corporation Turbofan comprising a plurality of individually controlled inlet guide vanes and corresponding controlling method
US7937927B2 (en) * 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
US8104257B2 (en) * 2004-12-01 2012-01-31 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
DE602004019710D1 (en) 2004-12-01 2009-04-09 United Technologies Corp REMOTE CONTROL FOR AN ADJUSTABLE STAGE OF A COMPRESSOR FOR A TURBINE ENGINE
DE602004032186D1 (en) 2004-12-01 2011-05-19 United Technologies Corp Turbine blade group of a fan rotor and method for assembling such a group
WO2006060001A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
WO2006060000A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
US7631480B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Modular tip turbine engine
EP1825177B1 (en) 2004-12-01 2012-01-25 United Technologies Corporation Inflatable bleed valve for turbine engine and method of controlling bleed air
WO2006059979A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
WO2006110125A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Stacked annular components for turbine engines
US7887296B2 (en) 2004-12-01 2011-02-15 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
WO2006059970A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US8033092B2 (en) 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006059973A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with a heat exchanger
WO2006060011A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
WO2006059997A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Annular turbine ring rotor
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
DE602004027766D1 (en) 2004-12-01 2010-07-29 United Technologies Corp HYDRAULIC SEAL FOR A GEARBOX OF A TOP TURBINE ENGINE
WO2006060013A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
EP1828683B1 (en) 2004-12-01 2013-04-10 United Technologies Corporation Combustor for turbine engine
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
WO2006059978A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Cantilevered tip turbine engine
EP2333287A1 (en) * 2004-12-01 2011-06-15 United Technologies Corporation Vectoring transition duct for turbine engine
US8061968B2 (en) 2004-12-01 2011-11-22 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
EP1825170B1 (en) 2004-12-01 2009-03-18 United Technologies Corporation Gearbox lubrication supply system for a tip turbine engine
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
US7874163B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Starter generator system for a tip turbine engine
EP1828567B1 (en) * 2004-12-01 2011-10-12 United Technologies Corporation Diffuser aspiration for a tip turbine engine
DE602004019709D1 (en) * 2004-12-01 2009-04-09 United Technologies Corp TIP TURBINE ENGINE AND CORRESPONDING OPERATING PROCESS
WO2006059996A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
DE602004029950D1 (en) 2004-12-01 2010-12-16 United Technologies Corp SLIDED GEAR ASSEMBLY FOR A TOP TURBINE ENGINE
WO2006059994A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
US7921635B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006059990A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
US7690186B2 (en) * 2005-11-09 2010-04-06 Pratt & Whitney Canada Corp. Gas turbine engine including apparatus to transfer power between multiple shafts
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US9857017B2 (en) * 2015-10-30 2018-01-02 Akron Brass Company Debris diverting inlet
CN109339948B (en) * 2018-11-23 2021-01-08 江西洪都航空工业集团有限责任公司 Gas turbine engine air inlet device for bombs

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2791668A (en) * 1951-08-21 1957-05-07 Napier & Son Ltd Electrically heated de-icing or antifreezing apparatus
US3063031A (en) * 1959-12-28 1962-11-06 Gen Motors Corp Electrical aircraft heater
US3534548A (en) * 1969-06-30 1970-10-20 Avco Corp Separator apparatus for engine air inlets

Also Published As

Publication number Publication date
DE2103035C3 (en) 1975-03-27
US3684857A (en) 1972-08-15
GB1328993A (en) 1973-09-05
DE2103035B2 (en) 1974-08-01
DE2103035A1 (en) 1971-08-26
FR2079257A1 (en) 1971-11-12

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
ST Notification of lapse