FR2266631B1 - - Google Patents

Info

Publication number
FR2266631B1
FR2266631B1 FR7412150A FR7412150A FR2266631B1 FR 2266631 B1 FR2266631 B1 FR 2266631B1 FR 7412150 A FR7412150 A FR 7412150A FR 7412150 A FR7412150 A FR 7412150A FR 2266631 B1 FR2266631 B1 FR 2266631B1
Authority
FR
France
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
FR7412150A
Other languages
French (fr)
Other versions
FR2266631A1 (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7412150A priority Critical patent/FR2266631A1/fr
Publication of FR2266631A1 publication Critical patent/FR2266631A1/fr
Application granted granted Critical
Publication of FR2266631B1 publication Critical patent/FR2266631B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/02—Influencing air flow over aircraft surfaces, not otherwise provided for by means of rotating members of cylindrical or similar form

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7412150A 1974-04-05 1974-04-05 Supersonic aircraft engine - is conical with central inlet, heat shield and outlet over fuselage Granted FR2266631A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7412150A FR2266631A1 (en) 1974-04-05 1974-04-05 Supersonic aircraft engine - is conical with central inlet, heat shield and outlet over fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7412150A FR2266631A1 (en) 1974-04-05 1974-04-05 Supersonic aircraft engine - is conical with central inlet, heat shield and outlet over fuselage

Publications (2)

Publication Number Publication Date
FR2266631A1 FR2266631A1 (en) 1975-10-31
FR2266631B1 true FR2266631B1 (es) 1978-05-12

Family

ID=9137350

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7412150A Granted FR2266631A1 (en) 1974-04-05 1974-04-05 Supersonic aircraft engine - is conical with central inlet, heat shield and outlet over fuselage

Country Status (1)

Country Link
FR (1) FR2266631A1 (es)

Also Published As

Publication number Publication date
FR2266631A1 (en) 1975-10-31

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Legal Events

Date Code Title Description
ST Notification of lapse