GB349365A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB349365A
GB349365A GB21943/30A GB2194330A GB349365A GB 349365 A GB349365 A GB 349365A GB 21943/30 A GB21943/30 A GB 21943/30A GB 2194330 A GB2194330 A GB 2194330A GB 349365 A GB349365 A GB 349365A
Authority
GB
United Kingdom
Prior art keywords
connecting member
secured
aircraft
rivets
bores
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
GB21943/30A
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.)
Bayerische Flugzeugwerke A G
Original Assignee
Bayerische Flugzeugwerke A G
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 Bayerische Flugzeugwerke A G filed Critical Bayerische Flugzeugwerke A G
Publication of GB349365A publication Critical patent/GB349365A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0063—Fuselage structures substantially made from particular materials from wood
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

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

Abstract

349,365. Aircraft framework. BAYERISCHE FLUGZEUGWERKE AKT.-GES. and MESSERSCHMITT, W., 118A, Haunstetterstrasse, Augsburg, Germany. July 21, 1930, No. 21943. Convention date, July 19, 1929. [Class 4.] A connection for the parts of aircraft comprises a solid connecting member corresponding to the distance between and the shape of the constituents of a girder frame or the like and provided with one or more bores for the reception of pins, hooks, &c. As shown the frame member 2 comprises two spaced channels 2<1>, 2<2> having between them the connecting member 15 of wood, light metal, &c. and gusset plates 11, 12 the whole being secured together by rivets 16, 17 or screws. The cross spar 7 and strut 9 are secured to the gusset plates by rivets 13, 14 and the member 15 is provided with one or more bores to receive an eyebolt 18 to which a strut for the engine bracket is secured. The connecting member may be of cylindrical, cubical or other simple shape and may be adapted to receive bolts, lugs, or screws.
GB21943/30A 1929-07-19 1930-07-21 Improvements in or relating to aircraft Expired GB349365A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE349365X 1929-07-19

Publications (1)

Publication Number Publication Date
GB349365A true GB349365A (en) 1931-05-28

Family

ID=6258450

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21943/30A Expired GB349365A (en) 1929-07-19 1930-07-21 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB349365A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007011613B4 (en) * 2007-01-22 2011-07-28 Airbus Operations GmbH, 21129 Fitting for the introduction of high forces in a fuselage cell of an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007011613B4 (en) * 2007-01-22 2011-07-28 Airbus Operations GmbH, 21129 Fitting for the introduction of high forces in a fuselage cell of an aircraft

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