FR1130131A - Improvement in the control of stator-reactor or annular wing aerodynes - Google Patents

Improvement in the control of stator-reactor or annular wing aerodynes

Info

Publication number
FR1130131A
FR1130131A FR1130131DA FR1130131A FR 1130131 A FR1130131 A FR 1130131A FR 1130131D A FR1130131D A FR 1130131DA FR 1130131 A FR1130131 A FR 1130131A
Authority
FR
France
Prior art keywords
stator
reactor
improvement
control
annular wing
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
Other languages
French (fr)
Inventor
Marcel Kadosch
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
Application granted granted Critical
Publication of FR1130131A publication Critical patent/FR1130131A/en
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
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1130131D 1955-07-12 1955-07-12 Improvement in the control of stator-reactor or annular wing aerodynes Expired FR1130131A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1130131T 1955-07-12

Publications (1)

Publication Number Publication Date
FR1130131A true FR1130131A (en) 1957-01-31

Family

ID=9637256

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1130131D Expired FR1130131A (en) 1955-07-12 1955-07-12 Improvement in the control of stator-reactor or annular wing aerodynes

Country Status (1)

Country Link
FR (1) FR1130131A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000177A (en) * 1956-07-11 1961-09-19 Snecma Multiple-flow jet-propulsion engines
US3103102A (en) * 1958-07-18 1963-09-10 Bristol Siddeley Engines Ltd Propulsion power plants for aircraft
US3402894A (en) * 1966-06-01 1968-09-24 United Aircraft Corp Base-thrust nozzles
US20230323809A1 (en) * 2022-04-12 2023-10-12 General Electric Company Combined cycle propulsion system for hypersonic flight

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000177A (en) * 1956-07-11 1961-09-19 Snecma Multiple-flow jet-propulsion engines
US3103102A (en) * 1958-07-18 1963-09-10 Bristol Siddeley Engines Ltd Propulsion power plants for aircraft
US3402894A (en) * 1966-06-01 1968-09-24 United Aircraft Corp Base-thrust nozzles
US20230323809A1 (en) * 2022-04-12 2023-10-12 General Electric Company Combined cycle propulsion system for hypersonic flight

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