GB315792A - Improvements in single spar aircraft wings and damping surfaces - Google Patents

Improvements in single spar aircraft wings and damping surfaces

Info

Publication number
GB315792A
GB315792A GB21904/29A GB2190429A GB315792A GB 315792 A GB315792 A GB 315792A GB 21904/29 A GB21904/29 A GB 21904/29A GB 2190429 A GB2190429 A GB 2190429A GB 315792 A GB315792 A GB 315792A
Authority
GB
United Kingdom
Prior art keywords
spar
wing
covering
ribs
construction
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
GB21904/29A
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 GB315792A publication Critical patent/GB315792A/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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

315,792. Messerschmitt, W. July 18, 1928, [Convention date]. Planes and the like, construction of.-A single spar wing or fin construction, designed to resist torsion, is characterized by the arrangement, at or close to the point of maximum depth in transverse section, of a spar a having thick flanges b, b', and a web c of plate or lattice construction to winch transverse ribs d are attached; a sheet metal covering h strengthened by numerous profile members f is attached to the ribs, the whole forming with the spar a rigid box-like, structure. The rear portion of the wing or fin, Fig. 3, may be constructed in a similar manner, or the rigid structure may be extended only so far as to form a portion k and the wing completed by a further rear portion n which may be detachable and may have ribs secured to the sheet-metal covering of the portion k. The portion k may be constructed in a similar manner to the front part l or its rear wall may be constituted by a channel section, to the flanges of which the covering is secured. Manholes may be provided in the covering to permit of access to points of connection of the component members. In a modification, spar a is constituted by channel flange members and two sheet web members arranged to form a box section.
GB21904/29A 1928-07-18 1929-07-16 Improvements in single spar aircraft wings and damping surfaces Expired GB315792A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE315792X 1928-07-18

Publications (1)

Publication Number Publication Date
GB315792A true GB315792A (en) 1930-10-16

Family

ID=6150294

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21904/29A Expired GB315792A (en) 1928-07-18 1929-07-16 Improvements in single spar aircraft wings and damping surfaces

Country Status (1)

Country Link
GB (1) GB315792A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2312483A (en) * 1996-04-24 1997-10-29 British Aerospace Joint assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2312483A (en) * 1996-04-24 1997-10-29 British Aerospace Joint assembly
US5944286A (en) * 1996-04-24 1999-08-31 British Aerospace Public Limited Company Joint assemblies
GB2312483B (en) * 1996-04-24 2000-02-23 British Aerospace Joint assemblies

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