GB1435567A - Vertical take-off and landing aircraft - Google Patents

Vertical take-off and landing aircraft

Info

Publication number
GB1435567A
GB1435567A GB2906573A GB2906573A GB1435567A GB 1435567 A GB1435567 A GB 1435567A GB 2906573 A GB2906573 A GB 2906573A GB 2906573 A GB2906573 A GB 2906573A GB 1435567 A GB1435567 A GB 1435567A
Authority
GB
United Kingdom
Prior art keywords
aircraft
control
thrust
nozzles
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
GB2906573A
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.)
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke Fokker 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 Vereinigte Flugtechnische Werke Fokker GmbH filed Critical Vereinigte Flugtechnische Werke Fokker GmbH
Publication of GB1435567A publication Critical patent/GB1435567A/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
    • B64C29/005—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

1435567 V.T.O.L. aircraft VEREINIGTE FLUGTECHNISCHE WERKE - FOKKER GmbH 19 June 1973 [7 July 1972] 29065/73 Heading B7G A high-wing V.T.O.L. aircraft 31 has a cruise engine 34 provided with laterally-disposed swivelling propulsion nozzles 33 which may be moved from forward-thrust positions to the vertical-lift position shown in the left-hand side of Fig. 3. Each nozzle has an upstream portion 37 mounted on a rotatable ring 36 and a downstream portion 32 pivotally mounted at 38 for arcuate movement under the control of an actuator whereby the direction of thrust may be adjusted in a transverse plane to effect roll control of the aircraft. The aircraft may have puffer jet control nozzles for use during take-off and landing and during transitional flight.
GB2906573A 1972-07-07 1973-06-19 Vertical take-off and landing aircraft Expired GB1435567A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722233352 DE2233352A1 (en) 1972-07-07 1972-07-07 V / STOL PLANE

Publications (1)

Publication Number Publication Date
GB1435567A true GB1435567A (en) 1976-05-12

Family

ID=5849943

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2906573A Expired GB1435567A (en) 1972-07-07 1973-06-19 Vertical take-off and landing aircraft

Country Status (2)

Country Link
DE (1) DE2233352A1 (en)
GB (1) GB1435567A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2188887A (en) * 1986-04-08 1987-10-14 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation
US4840329A (en) * 1986-04-08 1989-06-20 Rolls-Royce Inc. Aircraft with stowable vectorable nozzle and ejector thrust augmentation
US5323606A (en) * 1993-02-23 1994-06-28 Rolls-Royce Plc Stowable nozzle
GB2323065A (en) * 1993-03-13 1998-09-16 Rolls Royce Plc Vectorable nozzle for an aircraft
DE4007875A1 (en) 1989-03-14 2010-06-02 British Aerospace Public Ltd. Co. Schubstrahlauslaß
CN110615089A (en) * 2019-08-22 2019-12-27 南京航空航天大学 Roll-over control mechanism suitable for small vertical take-off and landing fixed wing aircraft
CN114562383A (en) * 2022-01-13 2022-05-31 中国航发沈阳发动机研究所 Adjustable bleed air spray tube of motor long distance
CN114576035A (en) * 2022-01-13 2022-06-03 中国航发沈阳发动机研究所 Rotatable motor long-distance adjustable bleed air spray pipe

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2188887A (en) * 1986-04-08 1987-10-14 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation
US4840329A (en) * 1986-04-08 1989-06-20 Rolls-Royce Inc. Aircraft with stowable vectorable nozzle and ejector thrust augmentation
GB2188887B (en) * 1986-04-08 1989-11-29 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation
US7980508B1 (en) 1989-03-14 2011-07-19 Bae Systems Plc Jet propulsion efflux outlets
DE4007875A1 (en) 1989-03-14 2010-06-02 British Aerospace Public Ltd. Co. Schubstrahlauslaß
US5323606A (en) * 1993-02-23 1994-06-28 Rolls-Royce Plc Stowable nozzle
GB2275235A (en) * 1993-02-23 1994-08-24 Rolls Royce Plc Stowable nozzle
GB2275235B (en) * 1993-02-23 1996-10-09 Rolls Royce Plc Stowable nozzle
US6036142A (en) * 1993-03-13 2000-03-14 Rolls-Royce, Plc Vectorable nozzle for aircraft
GB2323065B (en) * 1993-03-13 1998-12-09 Rolls Royce Plc Vectorable nozzle for aircraft
GB2323065A (en) * 1993-03-13 1998-09-16 Rolls Royce Plc Vectorable nozzle for an aircraft
CN110615089A (en) * 2019-08-22 2019-12-27 南京航空航天大学 Roll-over control mechanism suitable for small vertical take-off and landing fixed wing aircraft
CN114562383A (en) * 2022-01-13 2022-05-31 中国航发沈阳发动机研究所 Adjustable bleed air spray tube of motor long distance
CN114576035A (en) * 2022-01-13 2022-06-03 中国航发沈阳发动机研究所 Rotatable motor long-distance adjustable bleed air spray pipe
CN114576035B (en) * 2022-01-13 2024-01-30 中国航发沈阳发动机研究所 Long-distance adjustable air-guiding spray pipe of rotatable motor
CN114562383B (en) * 2022-01-13 2024-02-23 中国航发沈阳发动机研究所 Motor long-distance adjustable air-guiding spray pipe

Also Published As

Publication number Publication date
DE2233352A1 (en) 1974-01-24

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee