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

Dispositif de fixation d'ogive de moteur

Info

Publication number: BE808700A
Authority: BE; Belgium
Prior art keywords: wiggage; engine; mounting device; mounting; wiggage mounting
Prior art date: 1972-11-06

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.)

1972-11-06

Filing date

1973-12-14

Publication date

1974-03-29

1973-12-14 Application filed by Gen Electric filed Critical Gen Electric

1974-03-29 Publication of BE808700A publication Critical patent/BE808700A/fr

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
US9540939B2 (en) *	2012-12-28	2017-01-10	United Technologies Corporation	Gas turbine engine with attached nosecone
US9759129B2 (en) *	2012-12-28	2017-09-12	United Technologies Corporation	Removable nosecone for a gas turbine engine
US9682450B2 (en)	2013-01-11	2017-06-20	United Technologies Corporation	Gas turbine engine nose cone attachment configuration
US10352236B2 (en)	2013-10-30	2019-07-16	United Technologies Corporation	Nosecap
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

1972
- 1972-11-06 US US00304082A patent/US3799693A/en not_active Expired - Lifetime
1973
- 1973-12-14 BE BE138928A patent/BE808700A/fr unknown

Also Published As

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

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