FR1267920A - Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude - Google Patents

Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude

Info

Publication number
FR1267920A
FR1267920A FR830092A FR830092A FR1267920A FR 1267920 A FR1267920 A FR 1267920A FR 830092 A FR830092 A FR 830092A FR 830092 A FR830092 A FR 830092A FR 1267920 A FR1267920 A FR 1267920A
Authority
FR
France
Prior art keywords
aerodynes
attitude
change
support device
vertical take
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
FR830092A
Other languages
French (fr)
Inventor
Rene Paul Logerot
Hermann Neumann
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
Priority to FR830092A priority Critical patent/FR1267920A/en
Application granted granted Critical
Publication of FR1267920A publication Critical patent/FR1267920A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR830092A 1960-06-15 1960-06-15 Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude Expired FR1267920A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR830092A FR1267920A (en) 1960-06-15 1960-06-15 Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR830092A FR1267920A (en) 1960-06-15 1960-06-15 Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude

Publications (1)

Publication Number Publication Date
FR1267920A true FR1267920A (en) 1961-07-28

Family

ID=8733486

Family Applications (1)

Application Number Title Priority Date Filing Date
FR830092A Expired FR1267920A (en) 1960-06-15 1960-06-15 Support device for aerodynes, and more particularly for aerodynes with vertical take-off without change of attitude

Country Status (1)

Country Link
FR (1) FR1267920A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1247142B (en) * 1962-01-13 1967-08-10 D Aviat Sa Des Atel Aircraft with horizontally arranged, axial flow through lift jet engines
US3379395A (en) * 1965-08-09 1968-04-23 Gene W. Smith V/stol aircraft
US3819134A (en) * 1972-11-30 1974-06-25 Rockwell International Corp Aircraft system lift ejector
US3830451A (en) * 1973-06-28 1974-08-20 Rockwell International Corp Aircraft control system
US3831887A (en) * 1973-06-28 1974-08-27 Rockwell International Corp Aircraft control methods
WO1988010210A1 (en) * 1987-06-25 1988-12-29 Willis Mark T Venturi enhanced airfoil
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1247142B (en) * 1962-01-13 1967-08-10 D Aviat Sa Des Atel Aircraft with horizontally arranged, axial flow through lift jet engines
US3379395A (en) * 1965-08-09 1968-04-23 Gene W. Smith V/stol aircraft
US3819134A (en) * 1972-11-30 1974-06-25 Rockwell International Corp Aircraft system lift ejector
US3830451A (en) * 1973-06-28 1974-08-20 Rockwell International Corp Aircraft control system
US3831887A (en) * 1973-06-28 1974-08-27 Rockwell International Corp Aircraft control methods
WO1988010210A1 (en) * 1987-06-25 1988-12-29 Willis Mark T Venturi enhanced airfoil
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil

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