GB149708A - Improvements in or relating to aeroplanes - Google Patents

Improvements in or relating to aeroplanes

Info

Publication number
GB149708A
GB149708A GB3890/19A GB389019A GB149708A GB 149708 A GB149708 A GB 149708A GB 3890/19 A GB3890/19 A GB 3890/19A GB 389019 A GB389019 A GB 389019A GB 149708 A GB149708 A GB 149708A
Authority
GB
United Kingdom
Prior art keywords
aeroplanes
wings
relating
stout
cabins
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
GB3890/19A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3890/19A priority Critical patent/GB149708A/en
Publication of GB149708A publication Critical patent/GB149708A/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
    • B64C39/10—All-wing aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

149,708. Stout, W. B. Feb. 17, 1919. Aeroplanes; planes, construction of; steering and balancing; cars and cabins.-The wings 2 are formed with symmetrical convex upper and lower surfaces, merging with the surfaces 6, 7 of the central portion or fuselage, which provides an enclosed cockpit and carries the motors &c. The wings taper in outline and in thickness towards the tips, and their sweep is continued by the movable stabilizers 5 and elevators 14. A stream-lined hood 11 is carried beneath the body up to the propeller-boss 13.
GB3890/19A 1919-02-17 1919-02-17 Improvements in or relating to aeroplanes Expired GB149708A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3890/19A GB149708A (en) 1919-02-17 1919-02-17 Improvements in or relating to aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3890/19A GB149708A (en) 1919-02-17 1919-02-17 Improvements in or relating to aeroplanes

Publications (1)

Publication Number Publication Date
GB149708A true GB149708A (en) 1920-08-17

Family

ID=9766780

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3890/19A Expired GB149708A (en) 1919-02-17 1919-02-17 Improvements in or relating to aeroplanes

Country Status (1)

Country Link
GB (1) GB149708A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430820A (en) * 1941-12-04 1947-11-11 United Aircraft Corp Airplane of low aspect ratio
US2431293A (en) * 1940-12-18 1947-11-18 United Aircraft Corp Airplane of low aspect ratio

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431293A (en) * 1940-12-18 1947-11-18 United Aircraft Corp Airplane of low aspect ratio
US2430820A (en) * 1941-12-04 1947-11-11 United Aircraft Corp Airplane of low aspect ratio

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