GB0013835D0 - A gas turbine engine rotor and nose cone assembly - Google Patents

A gas turbine engine rotor and nose cone assembly

Info

Publication number
GB0013835D0
GB0013835D0 GB0013835A GB0013835A GB0013835D0 GB 0013835 D0 GB0013835 D0 GB 0013835D0 GB 0013835 A GB0013835 A GB 0013835A GB 0013835 A GB0013835 A GB 0013835A GB 0013835 D0 GB0013835 D0 GB 0013835D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
nose cone
cone assembly
engine rotor
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Withdrawn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
GB0013835A
Other versions
GB2363170A (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 GB0013835A priority Critical patent/GB2363170A/en
Publication of GB0013835D0 publication Critical patent/GB0013835D0/en
Publication of GB2363170A publication Critical patent/GB2363170A/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Withdrawn legal-status Critical Current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)
GB0013835A 2000-06-08 2000-06-08 Attaching a nose cone to a gas turbine engine rotor Withdrawn GB2363170A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0013835A GB2363170A (en) 2000-06-08 2000-06-08 Attaching a nose cone to a gas turbine engine rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0013835A GB2363170A (en) 2000-06-08 2000-06-08 Attaching a nose cone to a gas turbine engine rotor

Publications (2)

Publication Number Publication Date
GB0013835D0 true GB0013835D0 (en) 2000-07-26
GB2363170A GB2363170A (en) 2001-12-12

Family

ID=9893140

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0013835A Withdrawn GB2363170A (en) 2000-06-08 2000-06-08 Attaching a nose cone to a gas turbine engine rotor

Country Status (1)

Country Link
GB (1) GB2363170A (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002020349A1 (en) * 2000-09-07 2002-03-14 Honeywell International Inc. Two piece spinner
GB0506685D0 (en) * 2005-04-01 2005-05-11 Hopkins David R A design to increase and smoothly improve the throughput of fluid (air or gas) through the inlet fan (or fans) of an aero-engine system
FR2908827B1 (en) * 2006-11-16 2011-06-17 Snecma INPUT CONE FOR TURBOMACHINE
GB0803366D0 (en) 2008-02-26 2008-04-02 Rolls Royce Plc Nose cone assembly
DE102008045546A1 (en) * 2008-09-03 2010-03-04 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine inlet cone
GB0903012D0 (en) * 2009-02-24 2009-04-08 Rolls Royce Plc Mounting arrangement
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
GB2474449B (en) 2009-10-14 2012-02-22 Rolls Royce Plc Annulus filler element for a rotor of a turbomachine
DE102009053000B4 (en) * 2009-11-16 2014-01-02 Rolls-Royce Deutschland Ltd & Co Kg Fan retaining disc for a jet engine
GB201005053D0 (en) 2010-03-26 2010-05-12 Rolls Royce Plc A gas turbine engine nose cone
DE102010062125A1 (en) * 2010-11-29 2012-05-31 Rolls-Royce Deutschland Ltd & Co Kg A method of removing the polyurethane coating from a composite nose cone of a jet engine
GB201020213D0 (en) * 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly
GB201020230D0 (en) * 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly
US9969489B2 (en) * 2013-02-08 2018-05-15 General Electric Company Hybrid spinner support
EP2915953B1 (en) 2014-03-03 2019-01-16 Rolls-Royce Corporation Spinner for a gas turbine engine
DE102014217887A1 (en) 2014-09-08 2016-03-10 Rolls-Royce Deutschland Ltd & Co Kg Filling elements of a fan of a gas turbine
US10024234B2 (en) 2014-09-08 2018-07-17 Rolls-Royce Deutschland Ltd & Co Kg Panels of a fan of a gas turbine
DE102014217884A1 (en) 2014-09-08 2016-03-24 Rolls-Royce Deutschland Ltd & Co Kg Filling elements of a fan of a gas turbine
US10167088B2 (en) * 2015-10-19 2019-01-01 General Electric Company Crosswind performance aircraft engine spinner
US9879698B2 (en) 2015-10-26 2018-01-30 Rolls-Royce North American Technologies Inc. Nose cone and shaft balancing assembly
US10330009B2 (en) 2017-01-13 2019-06-25 United Technologies Corporation Lock for threaded in place nosecone or spinner
US10612405B2 (en) 2017-01-13 2020-04-07 United Technologies Corporation Stator outer platform sealing and retainer
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
EP3750798B1 (en) * 2017-07-13 2022-02-09 Ratier-Figeac SAS Protection of propeller components
FR3089548B1 (en) * 2018-12-07 2021-03-19 Safran Aircraft Engines BLOWER INCLUDING AN INTER-BLADE PLATFORM FIXED UPSTREAM BY A VIROLE
CN109339955B (en) * 2018-12-16 2021-09-03 中国航发沈阳发动机研究所 Supporting structure of deflation valve adjusting mechanism

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2371801A (en) * 1943-08-18 1945-03-20 Arthur C Chester Propeller spinner attaching device
GB650956A (en) * 1947-12-16 1951-03-07 Stanley Ronald Mitchinson Improvements in or relating to model aircraft propeller spinners
US3990814A (en) * 1975-06-25 1976-11-09 United Technologies Corporation Spinner
FR2621554B1 (en) * 1987-10-07 1990-01-05 Snecma NON-ROTATING INPUT COVER OF CENTRALLY FIXED TURBOREACTOR AND TURBOREACTOR THUS EQUIPPED
US5833435A (en) * 1996-12-24 1998-11-10 United Technologies Corporation Inlet nose cone assembly and method for repairing the assembly

Also Published As

Publication number Publication date
GB2363170A (en) 2001-12-12

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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)