BE812501A - Moteur a double flux - Google Patents

Moteur a double flux

Info

Publication number: BE812501A
Authority: BE; Belgium
Prior art keywords: double; stream motor; stream; motor
Prior art date: 1973-03-19

Application number

BE142165A

Other languages

English (en)

French (fr)

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.)

1973-03-19

Filing date

1974-03-19

Publication date

1974-09-19

1974-03-19 Application filed filed Critical

1974-09-19 Publication of BE812501A publication Critical patent/BE812501A/xx

Links

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Turbine Rotor Nozzle Sealing (AREA)

BE142165A 1973-03-19 1974-03-19 Moteur a double flux BE812501A (fr)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US342767A US3881315A (en)	1973-03-19	1973-03-19	Fan duct flow deflector

Publications (1)

Publication Number	Publication Date
BE812501A true BE812501A (fr)	1974-09-19

Family

ID=23343194

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BE142165A BE812501A (fr)	1973-03-19	1974-03-19	Moteur a double flux

Country Status (7)

Country	Link
US (1)	US3881315A (xx)
JP (1)	JPS5922062B2 (xx)
BE (1)	BE812501A (xx)
CA (1)	CA1002765A (xx)
DE (1)	DE2412242C2 (xx)
FR (1)	FR2222541B3 (xx)
GB (1)	GB1468726A (xx)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4410150A (en) *	1980-03-03	1983-10-18	General Electric Company	Drag-reducing nacelle
CA1185101A (en) *	1980-03-03	1985-04-09	Daniel J. Lahti	Drag-reducing nacelle
JPS58133455A (ja) *	1982-01-27	1983-08-09	ザ・ギヤレツト・コ−ポレ−シヨン	エンジン装置
US4567960A (en) *	1982-08-23	1986-02-04	The Boeing Company	Fixed geometry controlled entrainment ventilated convergent nozzle and method
US5265408A (en) *	1992-02-13	1993-11-30	Allied-Signal Inc.	Exhaust eductor cooling system
GB2356897B (en) *	1999-12-01	2003-05-14	Secr Defence	Improved nozzle
US6651929B2 (en) *	2001-10-29	2003-11-25	Pratt & Whitney Canada Corp.	Passive cooling system for auxiliary power unit installation
FR2972224B1 (fr)	2011-03-04	2018-04-20	Safran Aircraft Engines	Tuyere avec noyau aval presentant une forte courbure
US8998575B2 (en)	2011-11-14	2015-04-07	United Technologies Corporation	Structural stator airfoil
US10436120B2 (en)	2013-02-06	2019-10-08	United Technologies Corporation	Exhaust nozzle for an elongated gear turbofan with high bypass ratio
PL414889A1 (pl) *	2015-11-23	2017-06-05	General Electric Company	Okapotowanie sprężające dla wylotu silnika odrzutowego

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3060679A (en) *	1958-10-24	1962-10-30	Gen Electric	Powerplant
US3044258A (en) *	1958-11-25	1962-07-17	Gen Electric	Adjustable converging-diverging nozzle
US3068646A (en) *	1959-01-28	1962-12-18	Rolls Royce	Improvements in by-pass type gas turbine engines
US3017140A (en) *	1959-03-27	1962-01-16	John R Barnard	Propulsion and lifting surface system for aerial vehicles
US3261164A (en) *	1964-09-23	1966-07-19	United Aircraft Corp	Convergent-divergent co-annular primary nozzle
GB1069033A (en) *	1965-01-30	1967-05-17	Rolls Royce	Improvements in or relating to gas turbine jet propulsion engines
US3374630A (en) *	1966-10-03	1968-03-26	United Aircraft Corp	Marine propulsion system
US3463402A (en) *	1966-12-28	1969-08-26	United Aircraft Corp	Jet sound suppressing means

1973
- 1973-03-19 US US342767A patent/US3881315A/en not_active Expired - Lifetime
1974
- 1974-02-18 CA CA192,847A patent/CA1002765A/en not_active Expired
- 1974-03-14 DE DE2412242A patent/DE2412242C2/de not_active Expired
- 1974-03-15 FR FR7408813A patent/FR2222541B3/fr not_active Expired
- 1974-03-18 GB GB1189874A patent/GB1468726A/en not_active Expired
- 1974-03-18 JP JP49030137A patent/JPS5922062B2/ja not_active Expired
- 1974-03-19 BE BE142165A patent/BE812501A/xx unknown

Also Published As

Publication number	Publication date
JPS5922062B2 (ja)	1984-05-24
FR2222541B3 (xx)	1976-12-24
FR2222541A1 (xx)	1974-10-18
CA1002765A (en)	1977-01-04
DE2412242C2 (de)	1983-12-15
US3881315A (en)	1975-05-06
DE2412242A1 (de)	1974-09-26
GB1468726A (en)	1977-03-30
JPS5025920A (xx)	1975-03-18

Publication	Publication Date	Title
IT1014815B (it)	1977-04-30	Complesso a bobina
BE745774A (fr)	1970-08-10	Moteur a induction
BE826779A (fr)	1975-07-16	Essieu moteur
AT340351B (de)	1977-12-12	Vortriebsmaschine
BE811858A (fr)	1974-09-04	Moteur pas a pas lineaire
CU34050A (es)	1981-09-09	Compuestos polienicos
BE808368A (fr)	1974-03-29	Moteur a induction lineaire bilateral
FR2322475A1 (fr)	1977-03-25	Moteur a induction
AT330582B (de)	1976-07-12	Zahnradmaschine
FR2322280A1 (fr)	1977-03-25	Moteur hydraulique
FR2275325A1 (fr)	1976-01-16	Canot a moteur
IT1019810B (it)	1977-11-30	Separatore a trascinamento
FR2291375A1 (fr)	1976-06-11	Moteur hydraulique
BE812501A (fr)	1974-09-19	Moteur a double flux
BE786347A (fr)	1972-11-16	Moteur a piston rotatif
AT338730B (de)	1977-09-12	Vortriebsmaschine
IT1011240B (it)	1977-01-20	Complesso a rotore
BE815710A (fr)	1974-09-16	Moteur rotatif.
BE833528A (fr)	1976-01-16	Moteur rotatif
IT1036526B (it)	1979-10-30	Macchina motrice
IT1020498B (it)	1977-12-20	Motore ad ingranaggi
BE847426A (fr)	1977-02-14	Bequilles a moteur,
FR2331676A1 (fr)	1977-06-10	Moteur hydraulique
BE814967A (fr)	1974-09-02	Moteur
BR7405153A (pt)	1976-02-17	Motor sincromo