GB121990A - Improvements in Airplanes. - Google Patents

Improvements in Airplanes.

Info

Publication number
GB121990A
GB121990A GB18180/17A GB1818017A GB121990A GB 121990 A GB121990 A GB 121990A GB 18180/17 A GB18180/17 A GB 18180/17A GB 1818017 A GB1818017 A GB 1818017A GB 121990 A GB121990 A GB 121990A
Authority
GB
United Kingdom
Prior art keywords
planes
dihedral
tail
fin
main
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
GB18180/17A
Inventor
Joshua Gaskill Jackson
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 GB18180/17A priority Critical patent/GB121990A/en
Publication of GB121990A publication Critical patent/GB121990A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/08Aircraft not otherwise provided for having multiple wings

Landscapes

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

Abstract

121,990. Jackson, J. G. Dec. 7, 1917. Aerial machines without aerostats; planes, construction and arrangement of.-In aeroplanes of the kind provided with dihedral main planes and a tail portion comprising dihedral planes with a vertical fin underneath, the arrangement being such that the laterally projected areas of the dihedral surfaces equals the area of the fin, the dihedral and vertical tail-planes are made of increasing width from front to rear, and the main planes are arranged at an angle of incidence slightly greater than that of the tail-planes. Figs. 4 and 5 show the application to a hydro-aeroplane. The fuselage 23 is fitted with dihedral main planes 33 and tail-planes 28, 29 and with a fin 27. One or more additional main planes 34 may be provided. The invention is shown also applied to a flying-boat and to a land machine.
GB18180/17A 1917-12-07 1917-12-07 Improvements in Airplanes. Expired GB121990A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18180/17A GB121990A (en) 1917-12-07 1917-12-07 Improvements in Airplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18180/17A GB121990A (en) 1917-12-07 1917-12-07 Improvements in Airplanes.

Publications (1)

Publication Number Publication Date
GB121990A true GB121990A (en) 1919-01-07

Family

ID=32672375

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18180/17A Expired GB121990A (en) 1917-12-07 1917-12-07 Improvements in Airplanes.

Country Status (1)

Country Link
GB (1) GB121990A (en)

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