CA961652A - Balanced flap converging/diverging nozzle - Google Patents

Balanced flap converging/diverging nozzle

Info

Publication number: CA961652A
Authority: CA; Canada
Prior art keywords: diverging nozzle; converging; balanced flap; balanced; flap converging
Prior art date: 1971-12-20
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.): Expired

Application number

CA155,215A

Other versions

CA155215S (en

Inventor

Richard E. Teagle

Craig E. Swavely

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.)

Raytheon Technologies Corp

Original Assignee

United Aircraft Corp

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.)

1971-12-20

Filing date

1972-10-30

Publication date

1975-01-28

1972-10-30 Application filed by United Aircraft Corp filed Critical United Aircraft Corp

1975-01-28 Application granted granted Critical

1975-01-28 Publication of CA961652A publication Critical patent/CA961652A/en

Status Expired legal-status Critical Current

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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Supercharger (AREA)
Exhaust Silencers (AREA)

CA155,215A 1971-12-20 1972-10-30 Balanced flap converging/diverging nozzle Expired CA961652A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US20966571A	1971-12-20	1971-12-20

Publications (1)

Publication Number	Publication Date
CA961652A true CA961652A (en)	1975-01-28

Family

ID=22779734

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA155,215A Expired CA961652A (en)	1971-12-20	1972-10-30	Balanced flap converging/diverging nozzle

Country Status (8)

Country	Link
JP (1)	JPS5754614B2 (en)
AU (1)	AU470247B2 (en)
CA (1)	CA961652A (en)
DE (1)	DE2254719C3 (en)
FR (1)	FR2164594B1 (en)
GB (1)	GB1372330A (en)
IT (1)	IT972637B (en)
SE (1)	SE374171B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3979065A (en) *	1974-10-31	1976-09-07	United Technologies Corporation	Cooling liner for an exhaust nozzle
US4375276A (en) *	1980-06-02	1983-03-01	General Electric Company	Variable geometry exhaust nozzle
FR2724977B1 (en) *	1980-12-30	1996-12-13	Snecma	CONVERGENT-DIVERGENT NOZZLE ESPECIALLY FOR A TURBOREACTOR
CN115614179B (en) *	2022-08-31	2024-04-05	中国航发四川燃气涡轮研究院	Throat area adjusting mechanism

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3049875A (en) *	1952-08-15	1962-08-21	United Aircraft Corp	Variable flap plug type nozzle
FR1215236A (en) *	1958-11-12	1960-04-15	Snecma	Adjustable nozzle and jet thruster equipped with such nozzle
US3046730A (en) *	1960-09-21	1962-07-31	Marquardt Corp	Variable area exit nozzle
US3454227A (en) *	1966-08-19	1969-07-08	United Aircraft Corp	Free floating articulate ejector nozzle
FR2030532A5 (en) *	1969-07-03	1970-11-13	Snecma

1972
- 1972-10-30 CA CA155,215A patent/CA961652A/en not_active Expired
- 1972-11-09 DE DE19722254719 patent/DE2254719C3/en not_active Expired
- 1972-11-13 AU AU48787/72A patent/AU470247B2/en not_active Expired
- 1972-11-22 FR FR7242491A patent/FR2164594B1/fr not_active Expired
- 1972-12-02 GB GB5386672A patent/GB1372330A/en not_active Expired
- 1972-12-12 SE SE1616172A patent/SE374171B/xx unknown
- 1972-12-13 JP JP47125107A patent/JPS5754614B2/ja not_active Expired
- 1972-12-20 IT IT3325272A patent/IT972637B/en active

Also Published As

Publication number	Publication date
DE2254719C3 (en)	1982-02-04
AU4878772A (en)	1974-05-23
DE2254719A1 (en)	1973-06-28
FR2164594A1 (en)	1973-08-03
DE2254719B2 (en)	1981-06-25
FR2164594B1 (en)	1977-04-08
SE374171B (en)	1975-02-24
JPS5754614B2 (en)	1982-11-19
AU470247B2 (en)	1976-03-11
IT972637B (en)	1974-05-31
GB1372330A (en)	1974-10-30
JPS4869300A (en)	1973-09-20

Publication	Publication Date	Title
AU460360B2 (en)	1975-04-24	Swirl air nozzle
AU440749B2 (en)	1973-09-24	An improved firehose nozzle
CA952559A (en)	1974-08-06	Spray nozzle
CA953513A (en)	1974-08-27	Nozzle seal
CA952945A (en)	1974-08-13	Spray nozzle
CA954840A (en)	1974-09-17	Sprayer
CA958249A (en)	1974-11-26	Turbine flowmeter
CA927432A (en)	1973-05-29	Deflector
CA962240A (en)	1975-02-04	Contamination-preventing nozzle
CA967620A (en)	1975-05-13	Distribution nozzle
AU464779B2 (en)	1975-08-21	Pigments
AU468680B2 (en)	1976-01-22	Single point refueling nozzle
CA948863A (en)	1974-06-11	Jet nozzle
CA957115A (en)	1974-11-05	Sonic beater nozzle
CA962003A (en)	1975-02-04	Pigments
CA961652A (en)	1975-01-28	Balanced flap converging/diverging nozzle
CA966964A (en)	1975-05-06	Wax injection nozzle
CA930548A (en)	1973-07-24	Whirling hoop toy
AU4264072A (en)	1973-11-29	Suction nozzle
CA1017725A (en)	1977-09-20	Single point refueling nozzle
CA875452A (en)	1971-07-13	Pigments
CA865593A (en)	1971-03-09	Nozzle
AU461349B2 (en)	1972-08-03	Nozzle
AU493977B2 (en)	1977-10-27	Improved nozzle
CA879448A (en)	1971-08-31	Nozzle means