DE68910808T2 - Mantelgebläsetriebwerk mit einer Nasenhaube. - Google Patents

Mantelgebläsetriebwerk mit einer Nasenhaube.

Info

Publication number
DE68910808T2
DE68910808T2 DE1989610808 DE68910808T DE68910808T2 DE 68910808 T2 DE68910808 T2 DE 68910808T2 DE 1989610808 DE1989610808 DE 1989610808 DE 68910808 T DE68910808 T DE 68910808T DE 68910808 T2 DE68910808 T2 DE 68910808T2
Authority
DE
Germany
Prior art keywords
sheathed
nose cover
blower engine
blower
engine
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 - Lifetime
Application number
DE1989610808
Other languages
English (en)
Other versions
DE68910808D1 (de
Inventor
David John Nicholas
Tony Frederick Mortimer
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
Application granted granted Critical
Publication of DE68910808D1 publication Critical patent/DE68910808D1/de
Publication of DE68910808T2 publication Critical patent/DE68910808T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/14—Spinners
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Catching Or Destruction (AREA)
DE1989610808 1989-02-28 1989-12-11 Mantelgebläsetriebwerk mit einer Nasenhaube. Expired - Lifetime DE68910808T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB898904478A GB8904478D0 (en) 1989-02-28 1989-02-28 Gas turbine engine air intake

Publications (2)

Publication Number Publication Date
DE68910808D1 DE68910808D1 (de) 1993-12-23
DE68910808T2 true DE68910808T2 (de) 1994-03-31

Family

ID=10652415

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1989610808 Expired - Lifetime DE68910808T2 (de) 1989-02-28 1989-12-11 Mantelgebläsetriebwerk mit einer Nasenhaube.

Country Status (6)

Country Link
EP (1) EP0393283B1 (de)
JP (1) JP3012661B2 (de)
DE (1) DE68910808T2 (de)
ES (1) ES2045472T3 (de)
GB (1) GB8904478D0 (de)
RU (1) RU1814703C (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5275531A (en) * 1993-04-30 1994-01-04 Teleflex, Incorporated Area ruled fan blade ends for turbofan jet engine
JP3671330B2 (ja) * 1998-12-18 2005-07-13 徹也 小合 物体推進装置
US9896936B2 (en) 2014-02-07 2018-02-20 United Technologies Corporation Spinner for electrically grounding fan blades
US10167088B2 (en) * 2015-10-19 2019-01-01 General Electric Company Crosswind performance aircraft engine spinner

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4220171A (en) * 1979-05-14 1980-09-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Curved centerline air intake for a gas turbine engine
EP0111785A1 (de) * 1982-12-20 1984-06-27 The Boeing Company Mit Laminarströmung und kleinem stossbedingtem Widerstandsprofil
FR2605587B1 (fr) * 1986-10-23 1989-06-16 Onera (Off Nat Aerospatiale) Perfectionnements apportes aux helices aeriennes, notamment pour propulseurs d'aeronef
US4744214A (en) * 1987-06-29 1988-05-17 United Technologies Corporation Engine modularity

Also Published As

Publication number Publication date
JP3012661B2 (ja) 2000-02-28
GB8904478D0 (en) 1989-04-12
JPH02233830A (ja) 1990-09-17
RU1814703C (ru) 1993-05-07
DE68910808D1 (de) 1993-12-23
EP0393283A1 (de) 1990-10-24
EP0393283B1 (de) 1993-11-18
ES2045472T3 (es) 1994-01-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee