GB321364A - Improvements in and relating to aeroplanes - Google Patents

Improvements in and relating to aeroplanes

Info

Publication number
GB321364A
GB321364A GB2681/29A GB268129A GB321364A GB 321364 A GB321364 A GB 321364A GB 2681/29 A GB2681/29 A GB 2681/29A GB 268129 A GB268129 A GB 268129A GB 321364 A GB321364 A GB 321364A
Authority
GB
United Kingdom
Prior art keywords
fuselage
corners
struts
plane
braced
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
GB2681/29A
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 GB2681/29A priority Critical patent/GB321364A/en
Publication of GB321364A publication Critical patent/GB321364A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

321,364. Prest, C. O. Jan. 25, 1929. Planes connecting to machine; fuselages. - The fuselage of an aeroplane is made of square section bevelled at the nose to form an apex at the axial centre of the fuselage and is positioned with its corners at the top, bottom and sides as shown. The planes and undercarriage are connected to opposite sides of the corners of the fuselage by struts 22, 24, 26 and saddle pieces, the upper corner saddle piece being directly connected to the plane at 19. A biplane structure also is described in which the lower plane is connected directly to the lower corner and braced by struts to the two lateral corners of the fuselage. A modified monoplane has the plane braced by pairs of struts to the top and lateral corners of the fuselage.
GB2681/29A 1929-01-25 1929-01-25 Improvements in and relating to aeroplanes Expired GB321364A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2681/29A GB321364A (en) 1929-01-25 1929-01-25 Improvements in and relating to aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2681/29A GB321364A (en) 1929-01-25 1929-01-25 Improvements in and relating to aeroplanes

Publications (1)

Publication Number Publication Date
GB321364A true GB321364A (en) 1929-11-07

Family

ID=9743891

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2681/29A Expired GB321364A (en) 1929-01-25 1929-01-25 Improvements in and relating to aeroplanes

Country Status (1)

Country Link
GB (1) GB321364A (en)

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