FR1362220A - Avion avec des moteurs sustentateurs prévus aux ailes et disposés symétriquement par rapport à l'axe longitudinal de l'avion - Google Patents

Avion avec des moteurs sustentateurs prévus aux ailes et disposés symétriquement par rapport à l'axe longitudinal de l'avion

Info

Publication number
FR1362220A
FR1362220A FR7796A FR67007796A FR1362220A FR 1362220 A FR1362220 A FR 1362220A FR 7796 A FR7796 A FR 7796A FR 67007796 A FR67007796 A FR 67007796A FR 1362220 A FR1362220 A FR 1362220A
Authority
FR
France
Prior art keywords
airplane
wings
respect
longitudinal axis
arranged symmetrically
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
FR7796A
Other languages
English (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.)
Dornier Werke GmbH
Original Assignee
Dornier Werke GmbH
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 Dornier Werke GmbH filed Critical Dornier Werke GmbH
Application granted granted Critical
Publication of FR1362220A publication Critical patent/FR1362220A/fr
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
    • B64C29/005—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 the motors being fixed relative to the fuselage
    • 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
    • B64C29/0058—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 with vertical jet

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
FR7796A 1962-07-03 1963-07-01 Avion avec des moteurs sustentateurs prévus aux ailes et disposés symétriquement par rapport à l'axe longitudinal de l'avion Expired FR1362220A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED39286A DE1194265B (de) 1962-07-03 1962-07-03 Flugzeug mit symmetrisch zu seiner Laengsachse an den Fluegeln angeordneten Hubtriebwerken

Publications (1)

Publication Number Publication Date
FR1362220A true FR1362220A (fr) 1964-05-29

Family

ID=7044651

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7796A Expired FR1362220A (fr) 1962-07-03 1963-07-01 Avion avec des moteurs sustentateurs prévus aux ailes et disposés symétriquement par rapport à l'axe longitudinal de l'avion

Country Status (4)

Country Link
US (1) US3245638A (fr)
DE (1) DE1194265B (fr)
FR (1) FR1362220A (fr)
GB (1) GB988556A (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2203223B (en) * 1977-08-18 1989-02-15 British Aerospace Control means
GB0116219D0 (en) * 2001-07-03 2002-03-06 Bae Systems Plc An aircraft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2069996A (en) * 1935-02-21 1937-02-09 Curtiss Wright Corp Releasable tank and bomb rack
US2665093A (en) * 1950-12-19 1954-01-05 Manfredi Dario Parachute safety release
US3098632A (en) * 1953-09-11 1963-07-23 Lockheed Aircraft Corp Combination aircraft fuel tank and powerplant arrangement
US2954944A (en) * 1957-06-17 1960-10-04 Brevets H D Soc D Aircraft including propelling units disposed symmetrically with respect to the fore-and-aft axis of the aircraft
US3035797A (en) * 1959-01-26 1962-05-22 Neuschotz Robert Detachable connector assembly for fuel cells
US3066889A (en) * 1960-08-22 1962-12-04 Lockheed Aircraft Corp Vtol aircraft
US3089666A (en) * 1961-04-13 1963-05-14 Boeing Co Airplane having changeable thrust direction

Also Published As

Publication number Publication date
US3245638A (en) 1966-04-12
DE1194265B (de) 1965-06-03
GB988556A (en) 1965-04-07

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