GB370056A - Improvements in or relating to aircraft wings - Google Patents

Improvements in or relating to aircraft wings

Info

Publication number
GB370056A
GB370056A GB33565/30A GB3356530A GB370056A GB 370056 A GB370056 A GB 370056A GB 33565/30 A GB33565/30 A GB 33565/30A GB 3356530 A GB3356530 A GB 3356530A GB 370056 A GB370056 A GB 370056A
Authority
GB
United Kingdom
Prior art keywords
covering
profile members
dornier
class
aircraft wing
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
GB33565/30A
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.)
Dornier Metallbauten GmbH
Original Assignee
Dornier Metallbauten GmbH
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 Dornier Metallbauten GmbH filed Critical Dornier Metallbauten GmbH
Publication of GB370056A publication Critical patent/GB370056A/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)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

370,056. Aircraft wing structures. DORNIER-METALLBAUTEN GES. and DORNIER, C., Friedrichshafen-on-Bodensee, Germany. Nov. 7, 1930, No. 33565. Convention date, Dec. 17, 1929. [Class 4.] An aircraft wing comprises a stressed covering c which is attached to rigid profile members extending in the direction of flight and carried by latticework spars a.The profile members may be T-shaped as shown at d, Fig. 2, channel section as at e, or as a lattice beam i<1>. In the arrangement shown at f the covering is secured. by a superposed channel member g. In a further modification lattice-beam profile members are employed and the covering lies on their upper sides. Reference has been directed by the Comptroller to Specifications 157,953, 190,254, and 274,092, [all in Class 4, Aeronautics].
GB33565/30A 1929-12-17 1930-11-07 Improvements in or relating to aircraft wings Expired GB370056A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE370056X 1929-12-17

Publications (1)

Publication Number Publication Date
GB370056A true GB370056A (en) 1932-04-07

Family

ID=6318644

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33565/30A Expired GB370056A (en) 1929-12-17 1930-11-07 Improvements in or relating to aircraft wings

Country Status (1)

Country Link
GB (1) GB370056A (en)

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