BE808700A - Dispositif de fixation d'ogive de moteur - Google Patents

Dispositif de fixation d'ogive de moteur

Info

Publication number
BE808700A
BE808700A BE138928A BE138928A BE808700A BE 808700 A BE808700 A BE 808700A BE 138928 A BE138928 A BE 138928A BE 138928 A BE138928 A BE 138928A BE 808700 A BE808700 A BE 808700A
Authority
BE
Belgium
Prior art keywords
wiggage
engine
mounting device
mounting
wiggage mounting
Prior art date
Application number
BE138928A
Other languages
English (en)
Inventor
P R Hull
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BE808700A publication Critical patent/BE808700A/fr

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)
  • Turbine Rotor Nozzle Sealing (AREA)
BE138928A 1972-11-06 1973-12-14 Dispositif de fixation d'ogive de moteur BE808700A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00304082A US3799693A (en) 1972-11-06 1972-11-06 Bullet nose fastening arrangement

Publications (1)

Publication Number Publication Date
BE808700A true BE808700A (fr) 1974-03-29

Family

ID=23174980

Family Applications (1)

Application Number Title Priority Date Filing Date
BE138928A BE808700A (fr) 1972-11-06 1973-12-14 Dispositif de fixation d'ogive de moteur

Country Status (2)

Country Link
US (1) US3799693A (fr)
BE (1) BE808700A (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4363604A (en) * 1981-01-08 1982-12-14 Du-Bro Products Propeller spinner for model airplanes or the like
FR2502690B1 (fr) * 1981-03-27 1985-09-13 Snecma Dispositif de verrouillage d'aubes de soufflante et de fixation de capot avant d'un turboreacteur
DE3719098A1 (de) * 1987-06-06 1988-12-22 Mtu Muenchen Gmbh Nasenhaube aus faserverbundwerkstoffen
US5573378A (en) * 1995-07-10 1996-11-12 United Technologies Corporation Gas turbine nose cone attachment
GB9828812D0 (en) * 1998-12-29 1999-02-17 Rolls Royce Plc Gas turbine nose cone assembly
US6393831B1 (en) 2000-11-17 2002-05-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Exoskeletal engine
US8292592B2 (en) * 2008-04-02 2012-10-23 United Technologies Corporation Nosecone bolt access and aerodynamic leakage baffle
JP5274877B2 (ja) * 2008-04-11 2013-08-28 Ｈｏｙａ株式会社 ズームレンズ系及びそれを用いた電子撮像装置
US8616854B2 (en) * 2009-03-05 2013-12-31 Rolls-Royce Corporation Nose cone assembly
US8322991B2 (en) * 2009-04-10 2012-12-04 Rolls-Royce Corporation Balance weight
FR2971822B1 (fr) * 2011-02-21 2015-04-24 Snecma Rotor de soufflante, en particulier pour une turbomachine
FR2989733B1 (fr) 2012-04-19 2014-05-02 Snecma Cone d'entree de soufflante de turbomachine
US9759129B2 (en) * 2012-12-28 2017-09-12 United Technologies Corporation Removable nosecone for a gas turbine engine
US9540939B2 (en) * 2012-12-28 2017-01-10 United Technologies Corporation Gas turbine engine with attached nosecone
US9682450B2 (en) 2013-01-11 2017-06-20 United Technologies Corporation Gas turbine engine nose cone attachment configuration
WO2015065712A1 (fr) 2013-10-30 2015-05-07 United Technologies Corporation Embout de protection
US10753277B2 (en) 2016-07-27 2020-08-25 Raytheon Technologies Corporation Inlet cap of an engine
US10507904B2 (en) * 2016-11-03 2019-12-17 Rolls-Royce Corporation Snap fit nose cone assembly
US10344672B2 (en) * 2016-11-03 2019-07-09 Rolls-Royce Corporation Low weight nose cone assembly
FR3063309B1 (fr) * 2017-02-24 2019-06-07 Safran Aircraft Engines Capot d'entree tournant de turbomachine, comprenant une paroi externe aerodynamique et un organe de serrage de cone
FR3063308B1 (fr) * 2017-02-24 2019-04-26 Safran Aircraft Engines Bouchon pour capot d'entree tournant de turbomachine, comprenant une paroi externe aerodynamique et un organe de fixation de cone
US10502133B2 (en) * 2017-06-12 2019-12-10 General Electric Company Fastener cover for flowpath fasteners
US11097831B2 (en) * 2018-07-06 2021-08-24 Raytheon Technologies Corporation Gas turbine engine nose cone assembly
US20200284166A1 (en) * 2019-03-05 2020-09-10 United Technologies Corporation Cover secured by captive fastener

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1807397A (en) * 1927-05-20 1931-05-26 Westinghouse Electric & Mfg Co Propeller type pump or fan
US2548858A (en) * 1949-06-24 1951-04-17 Westinghouse Electric Corp Gas turbine apparatus
US2544490A (en) * 1949-07-07 1951-03-06 Jeffrey Mfg Co Adjustable cowling for fans or the like

Also Published As

Publication number Publication date
US3799693A (en) 1974-03-26

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