GB691302A - Devices for deflecting a fluid flow and applications thereof - Google Patents

Devices for deflecting a fluid flow and applications thereof

Info

Publication number
GB691302A
GB691302A GB20601/49A GB2060149A GB691302A GB 691302 A GB691302 A GB 691302A GB 20601/49 A GB20601/49 A GB 20601/49A GB 2060149 A GB2060149 A GB 2060149A GB 691302 A GB691302 A GB 691302A
Authority
GB
United Kingdom
Prior art keywords
deflecting
applications
devices
fluid flow
interceptor
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
GB20601/49A
Inventor
Marcel Kadosch
Francois Gilbert Paris
Jean Bertin
Raymond Hippolyte Marchal
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
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of GB691302A publication Critical patent/GB691302A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

691,302. Pulse jets. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. Aug. 8, 1949 [Aug. 11, 1948], No. 20601/49. Class 110(iii) [Also in Groups XXVII and XXXIII] The forward inlet 11 of a pulse jet is free of valves but is provided with an interceptor 2 opposite a curved portion 3 of the inlet duct, the interceptor serving to deflect a portion of the explosion gases around the curved wall 3 into a rearwardly directed duct 13, which may be connected to the reaction nozzle 12 or the rear end of the combustion chamber 10.
GB20601/49A 1948-08-11 1949-08-08 Devices for deflecting a fluid flow and applications thereof Expired GB691302A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR691302X 1948-08-11

Publications (1)

Publication Number Publication Date
GB691302A true GB691302A (en) 1953-05-13

Family

ID=9033014

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20601/49A Expired GB691302A (en) 1948-08-11 1949-08-08 Devices for deflecting a fluid flow and applications thereof

Country Status (1)

Country Link
GB (1) GB691302A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807137A (en) * 1953-07-15 1957-09-24 Snecma Jet deflecting device for jet propulsion units
US3096616A (en) * 1959-06-11 1963-07-09 Bendix Corp Jet propelled vehicle
US4050631A (en) * 1976-03-26 1977-09-27 The Boeing Company Jet engine nozzle for controlling the direction of thrust

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807137A (en) * 1953-07-15 1957-09-24 Snecma Jet deflecting device for jet propulsion units
US3096616A (en) * 1959-06-11 1963-07-09 Bendix Corp Jet propelled vehicle
US4050631A (en) * 1976-03-26 1977-09-27 The Boeing Company Jet engine nozzle for controlling the direction of thrust

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