GB0017357D0 - Gas turbine nose cone assembly - Google Patents

Gas turbine nose cone assembly

Info

Publication number
GB0017357D0
GB0017357D0 GB0017357A GB0017357A GB0017357D0 GB 0017357 D0 GB0017357 D0 GB 0017357D0 GB 0017357 A GB0017357 A GB 0017357A GB 0017357 A GB0017357 A GB 0017357A GB 0017357 D0 GB0017357 D0 GB 0017357D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
nose cone
cone assembly
turbine nose
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.)
Withdrawn
Application number
GB0017357A
Other versions
GB2364748A (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
Priority to GB0017357A priority Critical patent/GB2364748A/en
Publication of GB0017357D0 publication Critical patent/GB0017357D0/en
Publication of GB2364748A publication Critical patent/GB2364748A/en
Withdrawn legal-status Critical Current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)
GB0017357A 2000-07-15 2000-07-15 Gas turbine engine nose cone with tool access hole plug/cover Withdrawn GB2364748A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0017357A GB2364748A (en) 2000-07-15 2000-07-15 Gas turbine engine nose cone with tool access hole plug/cover

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0017357A GB2364748A (en) 2000-07-15 2000-07-15 Gas turbine engine nose cone with tool access hole plug/cover

Publications (2)

Publication Number Publication Date
GB0017357D0 true GB0017357D0 (en) 2000-08-30
GB2364748A GB2364748A (en) 2002-02-06

Family

ID=9895700

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0017357A Withdrawn GB2364748A (en) 2000-07-15 2000-07-15 Gas turbine engine nose cone with tool access hole plug/cover

Country Status (1)

Country Link
GB (1) GB2364748A (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4064174B2 (en) * 2002-07-18 2008-03-19 本田技研工業株式会社 Engine cover structure of outboard motor
GB2414521B (en) 2004-05-28 2007-04-11 Rolls Royce Plc Rotor assembly and annulus filler for gas turbine engine compressor
DE602005009232D1 (en) * 2005-12-23 2008-10-02 Techspace Aero Milmort Acoustic insulation of the stator of a low-pressure compressor
FR2908827B1 (en) * 2006-11-16 2011-06-17 Snecma INPUT CONE FOR TURBOMACHINE
US8616854B2 (en) 2009-03-05 2013-12-31 Rolls-Royce Corporation Nose cone assembly
DE102009016802A1 (en) * 2009-04-09 2010-10-14 Rolls-Royce Deutschland Ltd & Co Kg Fiber composite inlet cone for a gas turbine engine
US8322991B2 (en) 2009-04-10 2012-12-04 Rolls-Royce Corporation Balance weight
GB201020230D0 (en) * 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly
GB201020213D0 (en) 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly
US9481448B2 (en) 2013-03-11 2016-11-01 Rolls-Royce Corporation Aerodynamic fairings secondarily attached to nosecone
US9482236B2 (en) 2013-03-13 2016-11-01 Rolls-Royce Corporation Modulated cooling flow scheduling for both SFC improvement and stall margin increase
FR3063308B1 (en) * 2017-02-24 2019-04-26 Safran Aircraft Engines CAP FOR TURBOMACHINE ROTATING INPUT COVER, COMPRISING AERODYNAMIC EXTERNAL WALL AND CONE FASTENER
US10583913B2 (en) 2017-03-14 2020-03-10 General Electric Company Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole
US11097831B2 (en) * 2018-07-06 2021-08-24 Raytheon Technologies Corporation Gas turbine engine nose cone assembly

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573378A (en) * 1995-07-10 1996-11-12 United Technologies Corporation Gas turbine nose cone attachment

Also Published As

Publication number Publication date
GB2364748A (en) 2002-02-06

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Legal Events

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