GB1335771A - Vertical take off and landing wingless aircraft - Google Patents

Vertical take off and landing wingless aircraft

Info

Publication number
GB1335771A
GB1335771A GB1335771DA GB1335771A GB 1335771 A GB1335771 A GB 1335771A GB 1335771D A GB1335771D A GB 1335771DA GB 1335771 A GB1335771 A GB 1335771A
Authority
GB
United Kingdom
Prior art keywords
aircraft
landing
fold
away
fuselage
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
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.)
Pedrick A P
Original Assignee
Pedrick A P
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 Pedrick A P filed Critical Pedrick A P
Publication of GB1335771A publication Critical patent/GB1335771A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)

Abstract

1335771 VTOL aircraft A P PEDRICK 12 June 1972 6385/71 Headings B7G and B7W A wingless vertical-take-off aircraft having a fuselage 1 shaped to provide sufficient aerodynamic lift during normal flight to support the weight of the aircraft and having sufficient pivotally mounted ducted fan turbo-jet engines 13 ... 15 to provide an upward thrust which is greater than the weight of the aircraft. Control during take-off and landing is provided by compressed air jets at the nose 20, tail and at the ends of fold-away booms 16, 17. Fold-away fan wings are provided to permit an emergency landing. The normal undercarriage may be replaced by an inflatable bag. The fuselage may be detachable from the tail and engines in an emergency and provided with a parachute. A fold-away fan tailplane may be provided.
GB1335771D 1972-06-12 1972-06-12 Vertical take off and landing wingless aircraft Expired GB1335771A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB638571 1972-06-12

Publications (1)

Publication Number Publication Date
GB1335771A true GB1335771A (en) 1973-10-31

Family

ID=9813551

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1335771D Expired GB1335771A (en) 1972-06-12 1972-06-12 Vertical take off and landing wingless aircraft

Country Status (1)

Country Link
GB (1) GB1335771A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2442766A1 (en) * 1978-04-27 1980-06-27 Guichard Jean Luc Short take off and landing aircraft - has extendable flexible delta wing used temporarily in addition to permanent wings
GB2209314A (en) * 1987-09-02 1989-05-10 Manuel Munoz Saiz Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft
CN111976947A (en) * 2020-07-06 2020-11-24 西安飞机工业(集团)有限责任公司 Vertical take-off and landing variable wing cruising heavy-load unmanned aerial vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2442766A1 (en) * 1978-04-27 1980-06-27 Guichard Jean Luc Short take off and landing aircraft - has extendable flexible delta wing used temporarily in addition to permanent wings
GB2209314A (en) * 1987-09-02 1989-05-10 Manuel Munoz Saiz Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft
CN111976947A (en) * 2020-07-06 2020-11-24 西安飞机工业(集团)有限责任公司 Vertical take-off and landing variable wing cruising heavy-load unmanned aerial vehicle
CN111976947B (en) * 2020-07-06 2022-09-20 西安飞机工业(集团)有限责任公司 Vertical take-off and landing variable wing cruising heavy-load unmanned aerial vehicle

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees