GB9115625D0 - Aircraft engines - Google Patents

Aircraft engines

Info

Publication number
GB9115625D0
GB9115625D0 GB9115625A GB9115625A GB9115625D0 GB 9115625 D0 GB9115625 D0 GB 9115625D0 GB 9115625 A GB9115625 A GB 9115625A GB 9115625 A GB9115625 A GB 9115625A GB 9115625 D0 GB9115625 D0 GB 9115625D0
Authority
GB
United Kingdom
Prior art keywords
aircraft engines
engines
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.)
Withdrawn
Application number
GB9115625A
Other versions
GB2257752A (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.)
BAE Systems PLC
Original Assignee
British Aerospace 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 British Aerospace PLC filed Critical British Aerospace PLC
Priority to GB9115625A priority Critical patent/GB2257752A/en
Publication of GB9115625D0 publication Critical patent/GB9115625D0/en
Publication of GB2257752A publication Critical patent/GB2257752A/en
Withdrawn legal-status Critical Current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
    • F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices
    • 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
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
GB9115625A 1991-07-19 1991-07-19 Gas turbine inlet particle separator. Withdrawn GB2257752A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9115625A GB2257752A (en) 1991-07-19 1991-07-19 Gas turbine inlet particle separator.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9115625A GB2257752A (en) 1991-07-19 1991-07-19 Gas turbine inlet particle separator.

Publications (2)

Publication Number Publication Date
GB9115625D0 true GB9115625D0 (en) 1992-02-19
GB2257752A GB2257752A (en) 1993-01-20

Family

ID=10698636

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9115625A Withdrawn GB2257752A (en) 1991-07-19 1991-07-19 Gas turbine inlet particle separator.

Country Status (1)

Country Link
GB (1) GB2257752A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2951226B1 (en) * 2009-10-14 2013-01-04 Turbomeca AIR FILTERING DEVICE INTO INTERNAL COMBUSTION ENGINE INPUT WITH VENTILATION MEANS
US20120131900A1 (en) * 2010-11-30 2012-05-31 General Electric Company Inlet particle separator system
US20140144123A1 (en) * 2012-11-29 2014-05-29 Honeywell International Inc. Inlet particle separator system with air injection

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1201096A (en) * 1966-11-15 1970-08-05 United Aircraft Corp Air particle separator
GB2095335B (en) * 1981-03-20 1984-05-31 Rolls Royce Gas turbine engine air intake system
GB2203801B (en) * 1987-04-14 1991-11-27 Rolls Royce Plc A gas turbine engine
US4916893A (en) * 1987-09-02 1990-04-17 Sundstrand Corporation Multipurpose auxiliary power unit
US4928480A (en) * 1988-03-04 1990-05-29 General Electric Company Separator having multiple particle extraction passageways

Also Published As

Publication number Publication date
GB2257752A (en) 1993-01-20

Similar Documents

Publication Publication Date Title
IL98630A0 (en) All-wing aircraft
GB2260371B (en) Turbine engines
GB2273318B (en) Aircraft engine arrangement
GB2241745B (en) Turboramjet engine
AU121271S (en) Aircraft
GB8915835D0 (en) Engines
EP0439014A3 (en) Fan-in-wingedge aircraft
GB2258012B (en) Engine system
GB9225467D0 (en) Aircraft construction
GB9020137D0 (en) Aircraft seating
GB9115625D0 (en) Aircraft engines
GB9127198D0 (en) Engine components
AU116067S (en) Aircraft
GB9101937D0 (en) Aircraft
GB9121211D0 (en) Aircraft
GB9118952D0 (en) An aircraft
GB9103594D0 (en) Engine structure
HU910486D0 (en) Engine
GB9106636D0 (en) Syro-kinetic non-combustional engine
HU911019D0 (en) Engine
GB9125777D0 (en) Aircraft construction
GR900200113U (en) Aircraft
GB9225147D0 (en) Flexwing aircraft
AU104015S (en) Axial-fan cowling
IL94669A0 (en) Aircraft construction

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)