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GB1227804A - - Google Patents

Info

Publication number
GB1227804A
GB1227804A GB3559968A GB3559968A GB1227804A GB 1227804 A GB1227804 A GB 1227804A GB 3559968 A GB3559968 A GB 3559968A GB 3559968 A GB3559968 A GB 3559968A GB 1227804 A GB1227804 A GB 1227804A
Authority
GB
United Kingdom
Prior art keywords
flap
flaps
jet
aircraft
july
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
GB3559968A
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 filed Critical
Publication of GB1227804A publication Critical patent/GB1227804A/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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/16—Fairings movable in conjunction with undercarriage elements
    • 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
    • B64C29/0091—Accessories not provided for elsewhere

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Transmission Devices (AREA)

Abstract

1,227,804. Jet deflectors. VEREINIGTE FLUGTECHNISCHE WERKE G.m.b.H. 25 July, 1968 [26 July, 1967], No. 35599/68. Heading B7G. A jet deflecting apparatus comprises two flaps 1 and 6 pivotally connected together and lying one behind the other with respect to the longitudinal axis of an aircraft across the outlet of a lift engine mounted in the fuselage 3 or wing of an aircraft wherein flap 1 may be actuated by a drive mechanism (not shown) to rotate about a transverse shaft 2 and thereby, via lever 4, rod 5 and lever 14 causing flap 6 to pivot in a guideway 10 along which it travels upon two rollers 9, 9<SP>1</SP> whilst being guided by a pivoted arm 12 having one end carrying a slot 11 in which a pin 13 attached to flap 6 is displaceably engaged. The arrangement functions such that as the flaps open from the closed position in which they seal the engine outlet, both flaps deflect rearwardly the jet efflux until the fully open position is reached.
GB3559968A 1967-07-26 1968-07-25 Expired GB1227804A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEV34149A DE1284851B (en) 1967-07-26 1967-07-26 Airplane with at least one lift engine, the outlet of which can be closed by two flaps one behind the other

Publications (1)

Publication Number Publication Date
GB1227804A true GB1227804A (en) 1971-04-07

Family

ID=7588659

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3559968A Expired GB1227804A (en) 1967-07-26 1968-07-25

Country Status (4)

Country Link
US (1) US3486721A (en)
DE (1) DE1284851B (en)
FR (1) FR1579036A (en)
GB (1) GB1227804A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2279629A (en) * 1993-06-25 1995-01-11 Rolls Royce Plc Vectorable nozzle for aircraft.

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4760960A (en) * 1987-05-22 1988-08-02 United Technologies Corporation Linkage for area controlled, thrust vectoring vane cascade
FR2634251B1 (en) * 1988-07-18 1993-08-13 Hispano Suiza Sa DOUBLE-FLOW TURBOREACTOR DRIVE INVERTER HAVING MOBILE DEVIATION EDGES
US5213286A (en) * 1990-10-10 1993-05-25 General Electric Company Door for aircraft nacelle
GB2435637B (en) * 1991-12-06 2008-02-06 British Aerospace Jet Propulsion Outlets
GB0002264D0 (en) * 2000-02-02 2000-03-22 British Aerospace Landing gear doors
US6352221B1 (en) 2000-03-03 2002-03-05 The Boeing Company Rotary landing gear assembly
US6345786B1 (en) 2000-03-03 2002-02-12 The Boeing Company Linked multi-segment landing gear door for aircraft
DE10313729B4 (en) * 2003-03-27 2007-11-29 Airbus Deutschland Gmbh Air outlet valve for an aircraft
US8342920B2 (en) * 2008-10-20 2013-01-01 Honeywell International Inc. Outflow valve having J-shaped bellmouth and cabin pressure control system employing the same
US8376818B2 (en) * 2009-01-29 2013-02-19 Honeywell International Inc. Thrust recovery, or other valve, containing two independently actuated doors and control system
DE102009010150B4 (en) * 2009-02-23 2013-09-19 Airbus Operations Gmbh System and method for emergency ventilation of an aircraft cabin
US20120096772A1 (en) * 2010-10-25 2012-04-26 Hamilton Sundstrand Corporation Door System
US9573690B2 (en) * 2011-09-06 2017-02-21 Honeywell International Inc. Thrust recovery outflow valve with a single bi-fold door and method of controlling aircraft cabin pressure
US9067680B2 (en) * 2011-09-29 2015-06-30 The Boeing Company Aircraft outflow valve
FR3021626B1 (en) * 2014-05-28 2017-12-22 Airbus Operations Sas FUSELAGE EQUIPMENT FORMING A DOOR AND COMPRISING A PRESSURIZING AIR EXHAUST REGULATION VALVE

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3127130A (en) * 1964-03-31 Variable shaped airfoil
DE1109530B (en) * 1959-01-08 1961-06-22 Rolls Royce Vertical take off aircraft
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
GB998341A (en) * 1963-07-02 1965-07-14 Rolls Royce Improvements in or relating to vertical lift jet engines
FR1497434A (en) * 1966-10-25 1967-10-06 Entwicklungsring Sued Gmbh Aircraft wing flap device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2279629A (en) * 1993-06-25 1995-01-11 Rolls Royce Plc Vectorable nozzle for aircraft.
GB2279629B (en) * 1993-06-25 1997-03-05 Rolls Royce Plc Vectorable nozzle for aircraft

Also Published As

Publication number Publication date
DE1284851B (en) 1968-12-05
FR1579036A (en) 1969-08-22
US3486721A (en) 1969-12-30

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees