GB1319223A - Aerodynamic arrangement ofr reducing drag by a propeller-wing combination - Google Patents

Aerodynamic arrangement ofr reducing drag by a propeller-wing combination

Info

Publication number
GB1319223A
GB1319223A GB1319223DA GB1319223A GB 1319223 A GB1319223 A GB 1319223A GB 1319223D A GB1319223D A GB 1319223DA GB 1319223 A GB1319223 A GB 1319223A
Authority
GB
United Kingdom
Prior art keywords
propeller
mainplane
ofr
reducing drag
tips
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.)
Jackson B J
Original Assignee
Jackson B J
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 Jackson B J filed Critical Jackson B J
Publication of GB1319223A publication Critical patent/GB1319223A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/066—Aircraft not otherwise provided for having disc- or ring-shaped wings having channel wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft

Landscapes

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

Abstract

1319223 Aircraft B J JACKSON 4 Jan 1972 [5 Jan 1971] 366/71 Heading B7W A low powered aircraft having a biplane negative staggered configuration comprises an upper mainplane 1 and a low mainplane 3 which, outboard of vertical planes containing the tips of main plane 1, is cranked upwardly and outwardly to form outer wing panels 6, thereby forming gaps 2. A propeller 4 is mounted at each tip of mainplane 1 so that the tips of the blades clear the upper surface of the cranked portion of mainplane 3 and the planes containing the propeller blades are in chordwise alignment on said upper surfaces with the position of boundary flow transition, thereby causing supercirculation. A canard noseplane 5 is provided.
GB1319223D 1971-01-05 1971-01-05 Aerodynamic arrangement ofr reducing drag by a propeller-wing combination Expired GB1319223A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36671 1971-01-05

Publications (1)

Publication Number Publication Date
GB1319223A true GB1319223A (en) 1973-06-06

Family

ID=9703146

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1319223D Expired GB1319223A (en) 1971-01-05 1971-01-05 Aerodynamic arrangement ofr reducing drag by a propeller-wing combination

Country Status (1)

Country Link
GB (1) GB1319223A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016200502A3 (en) * 2015-05-01 2017-03-09 Transition Robotics, Inc. Remotely controlled modular vtol aircraft and re-configurable system using same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016200502A3 (en) * 2015-05-01 2017-03-09 Transition Robotics, Inc. Remotely controlled modular vtol aircraft and re-configurable system using same
US10377482B2 (en) 2015-05-01 2019-08-13 Transition Robotics, Inc. Remotely controlled modular VTOL aircraft and re-configurable system using same

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed