GB315793A - Improvements in single spar aircraft wings and damping surfaces - Google Patents

Improvements in single spar aircraft wings and damping surfaces

Info

Publication number
GB315793A
GB315793A GB21905/29A GB2190529A GB315793A GB 315793 A GB315793 A GB 315793A GB 21905/29 A GB21905/29 A GB 21905/29A GB 2190529 A GB2190529 A GB 2190529A GB 315793 A GB315793 A GB 315793A
Authority
GB
United Kingdom
Prior art keywords
sections
spar
wing
stiffening
plates
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
GB21905/29A
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
Publication of GB315793A publication Critical patent/GB315793A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

315,793. Messerschmitt, W. July 18, 1928, [Convention date]. Planes and the like, construction of.-A single spar aircraft wing or damping surface is constructed with the stiffening ribs divided into several sections R' - - R<4>, these sections being combined with the adjoining plates a-b, a-c, b-d, c-e of the outer skin B extending along the whole or a, large portion of the span and with continuous stiffening sections P secured to the plates, to form partial aggregates which may be trough-shaped or flat according to the shape of the part of the wing which they form, and are singly connected to the spar H to form a final continuous structure in which all the parts, including the skin B, contribute to the strength of the wing. The rib sections are T-section and are attached to spar H and to a light division G by angle sections n; one or more diagonals D may be included. Rivets or screws may be used in assembling and additional stiffening may be provided at the connections.
GB21905/29A 1928-07-18 1929-07-16 Improvements in single spar aircraft wings and damping surfaces Expired GB315793A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE315793X 1928-07-18

Publications (1)

Publication Number Publication Date
GB315793A true GB315793A (en) 1930-08-21

Family

ID=6150295

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21905/29A Expired GB315793A (en) 1928-07-18 1929-07-16 Improvements in single spar aircraft wings and damping surfaces

Country Status (1)

Country Link
GB (1) GB315793A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433999A (en) * 1944-06-10 1948-01-06 Vidal Corp Wing and stabilizer structure for gliders
US2451458A (en) * 1943-06-28 1948-10-12 Budd Co Aircraft airfoil construction
US2451454A (en) * 1943-06-28 1948-10-12 Budd Co Method of fabricating airfoils

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451458A (en) * 1943-06-28 1948-10-12 Budd Co Aircraft airfoil construction
US2451454A (en) * 1943-06-28 1948-10-12 Budd Co Method of fabricating airfoils
US2433999A (en) * 1944-06-10 1948-01-06 Vidal Corp Wing and stabilizer structure for gliders

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