GB844519A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB844519A
GB844519A GB19328/58A GB1932858A GB844519A GB 844519 A GB844519 A GB 844519A GB 19328/58 A GB19328/58 A GB 19328/58A GB 1932858 A GB1932858 A GB 1932858A GB 844519 A GB844519 A GB 844519A
Authority
GB
United Kingdom
Prior art keywords
wing
aircraft
june
extended
axis
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
GB19328/58A
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.)
Helmut Phgar Von Zborowski
Original Assignee
Helmut Phgar Von Zborowski
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 Helmut Phgar Von Zborowski filed Critical Helmut Phgar Von Zborowski
Publication of GB844519A publication Critical patent/GB844519A/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
    • B64C29/0091—Accessories not provided for elsewhere

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)

Abstract

844,519. Annular wing aircraft. ZBOROWSKI, H. P. G. A. R. VON June 17,1958 [June 18, 1957], No. 19328/68. Class 4. In an aircraft having an annular wing 1, nacelle 3 and propulsion unit 2, the upper and lower wing chords L 1 , L 2 are cambered in the same direction in planes of symmetry parallel to a vertical plane passing through the axis XY, preferably from a maximum camber in the vertical plane through XY to a minimum or zero camber in the horizontal XY plane. By this arrangement the axis of the wing may be maintained at zero incidence to the line of flight. As in Fig. 16, the wing and central nacelle, which may house aircrew as well as a propulsion unit, are connected by faired struts 14 extended at 12 outside the wing to support nacelles 11 which provide passenger accommodation and house elements of the undercarriage to be extended when the aircraft is in a vertical take-off attitude.
GB19328/58A 1957-06-18 1958-06-17 Improvements in or relating to aircraft Expired GB844519A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR844519X 1957-06-18

Publications (1)

Publication Number Publication Date
GB844519A true GB844519A (en) 1960-08-10

Family

ID=9312467

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19328/58A Expired GB844519A (en) 1957-06-18 1958-06-17 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB844519A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007001622A1 (en) * 2007-01-03 2008-07-10 Wetzel, Heinz-Eberhard, Dr. Jet engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007001622A1 (en) * 2007-01-03 2008-07-10 Wetzel, Heinz-Eberhard, Dr. Jet engine

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