CA618830A - Device for varying the effective area of a jet propulsion nozzle - Google Patents

Device for varying the effective area of a jet propulsion nozzle

Info

Publication number
CA618830A
CA618830A CA618830A CA618830DA CA618830A CA 618830 A CA618830 A CA 618830A CA 618830 A CA618830 A CA 618830A CA 618830D A CA618830D A CA 618830DA CA 618830 A CA618830 A CA 618830A
Authority
CA
Canada
Prior art keywords
varying
effective area
jet propulsion
propulsion nozzle
nozzle
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.)
Expired
Application number
CA618830A
Inventor
Le Foll Jean
M. L. Maunoury Francois
Bertin Jean
Kadosch Marcel
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication date
Application granted granted Critical
Publication of CA618830A publication Critical patent/CA618830A/en
Expired legal-status Critical Current

Links

CA618830A Device for varying the effective area of a jet propulsion nozzle Expired CA618830A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA618830T

Publications (1)

Publication Number Publication Date
CA618830A true CA618830A (en) 1961-04-25

Family

ID=35861118

Family Applications (1)

Application Number Title Priority Date Filing Date
CA618830A Expired CA618830A (en) Device for varying the effective area of a jet propulsion nozzle

Country Status (1)

Country Link
CA (1) CA618830A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3660982A (en) * 1969-07-28 1972-05-09 Aerospatiale Non-return device for fluid ducts and thrust reversers
US4707981A (en) * 1986-01-27 1987-11-24 Rockwell International Corporation Variable expansion ratio reaction engine
US5996936A (en) * 1997-09-29 1999-12-07 General Electric Company Fluidic throat exhaust nozzle
US6021637A (en) * 1997-09-29 2000-02-08 General Electric Company Integrated fluidic CD nozzle for gas turbine engine
US6336319B1 (en) 2000-05-26 2002-01-08 General Electric Company Fluidic nozzle control system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3660982A (en) * 1969-07-28 1972-05-09 Aerospatiale Non-return device for fluid ducts and thrust reversers
US4707981A (en) * 1986-01-27 1987-11-24 Rockwell International Corporation Variable expansion ratio reaction engine
US5996936A (en) * 1997-09-29 1999-12-07 General Electric Company Fluidic throat exhaust nozzle
US6021637A (en) * 1997-09-29 2000-02-08 General Electric Company Integrated fluidic CD nozzle for gas turbine engine
US6336319B1 (en) 2000-05-26 2002-01-08 General Electric Company Fluidic nozzle control system

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