DE2103035C3 - Lufteinlaß für Gasturbinentriebwerke - Google Patents

Lufteinlaß für Gasturbinentriebwerke

Info

Publication number
DE2103035C3
DE2103035C3 DE2103035A DE2103035A DE2103035C3 DE 2103035 C3 DE2103035 C3 DE 2103035C3 DE 2103035 A DE2103035 A DE 2103035A DE 2103035 A DE2103035 A DE 2103035A DE 2103035 C3 DE2103035 C3 DE 2103035C3
Authority
DE
Germany
Prior art keywords
air
air inlet
upstream
air guide
downstream
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
DE2103035A
Other languages
German (de)
English (en)
Other versions
DE2103035A1 (de
DE2103035B2 (de
Inventor
George Henry London Bennett
Richard George Salisbury Wiltshire Harvey
Frederick William Walton Castle Donington Derby Morley
Alan Winchester Hampshire Wilson
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE2103035A1 publication Critical patent/DE2103035A1/de
Publication of DE2103035B2 publication Critical patent/DE2103035B2/de
Application granted granted Critical
Publication of DE2103035C3 publication Critical patent/DE2103035C3/de
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

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)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Supercharger (AREA)
  • Filtering Of Dispersed Particles In Gases (AREA)
DE2103035A 1970-02-05 1971-01-22 Lufteinlaß für Gasturbinentriebwerke Expired DE2103035C3 (de)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
DE2103035A1 DE2103035A1 (de) 1971-08-26
DE2103035B2 DE2103035B2 (de) 1974-08-01
DE2103035C3 true DE2103035C3 (de) 1975-03-27

Family

ID=9796916

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2103035A Expired DE2103035C3 (de) 1970-02-05 1971-01-22 Lufteinlaß für Gasturbinentriebwerke

Country Status (4)

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

Families Citing this family (49)

* 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
WO2006059980A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Diffuser aspiration for a tip turbine engine
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
DE602004027766D1 (de) 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
EP1825114B1 (en) * 2004-12-01 2008-08-20 United Technologies Corporation Tip turbine engine with a heat exchanger
WO2006059988A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Modular tip turbine engine
US8033094B2 (en) 2004-12-01 2011-10-11 United Technologies Corporation Cantilevered tip turbine engine
EP1841960B1 (en) 2004-12-01 2011-05-25 United Technologies Corporation Starter generator system for a 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
WO2006060003A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
WO2006059996A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
EP1825111B1 (en) 2004-12-01 2011-08-31 United Technologies Corporation Counter-rotating compressor case for a tip turbine engine
EP1828683B1 (en) 2004-12-01 2013-04-10 United Technologies Corporation Combustor for 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
US8033092B2 (en) 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006110125A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Stacked annular components for turbine engines
WO2006059995A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Gearbox lubrication supply system for a tip turbine engine
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US7937927B2 (en) * 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
DE602004032186D1 (de) 2004-12-01 2011-05-19 United Technologies Corp Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
EP1825128B1 (en) 2004-12-01 2011-03-02 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
WO2006059979A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
DE602004031986D1 (de) 2004-12-01 2011-05-05 United Technologies Corp Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
US8104257B2 (en) * 2004-12-01 2012-01-31 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
US7921635B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006060011A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
US7883315B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US7959406B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a 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
WO2006059997A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Annular turbine ring rotor
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
EP1831520B1 (en) * 2004-12-01 2009-02-25 United Technologies Corporation Tip turbine engine and corresponding operating method
WO2006059972A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
WO2006110123A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Vectoring transition duct for turbine engine
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
WO2006059989A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine support structure
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for 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 (zh) * 2018-11-23 2021-01-08 江西洪都航空工业集团有限责任公司 弹用燃气涡轮发动机进气装置
US12326114B2 (en) 2023-08-15 2025-06-10 Rtx Corporation Gas turbine engine with core debris protection

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
DE2103035A1 (de) 1971-08-26
GB1328993A (en) 1973-09-05
US3684857A (en) 1972-08-15
FR2079257B1 (en:Method) 1975-06-06
FR2079257A1 (en:Method) 1971-11-12
DE2103035B2 (de) 1974-08-01

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
EGA New person/name/address of the applicant
8339 Ceased/non-payment of the annual fee