GB404606A - Improvements in or relating to aircraft fuselages and aircraft motor gondolas - Google Patents

Improvements in or relating to aircraft fuselages and aircraft motor gondolas

Info

Publication number
GB404606A
GB404606A GB10875/32A GB1087532A GB404606A GB 404606 A GB404606 A GB 404606A GB 10875/32 A GB10875/32 A GB 10875/32A GB 1087532 A GB1087532 A GB 1087532A GB 404606 A GB404606 A GB 404606A
Authority
GB
United Kingdom
Prior art keywords
aircraft
panels
fuselage
covered
dornier
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
GB10875/32A
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
Priority to GB10875/32A priority Critical patent/GB404606A/en
Publication of GB404606A publication Critical patent/GB404606A/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
    • B64C1/08—Geodetic or other open-frame structures
    • 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
    • B64C1/061—Frames
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Details Of Aerials (AREA)

Abstract

404,606. Aircraft fuselages. DORNIER METALLBAUTEN GES., and DORNIER, C., Friedrichshafen, Lake Constance, Germany. April 15, 1932, No. 10875. Void [Abridged as open to inspection under Sect. 91 of the Acts, May 22, 1932]. [Class 4.] In an aircraft fuselage or motor gondola wherein all the stresses occurring are taken up by a spatial skeleton structure a, an outer covering is provided formed by individual reinforced panels b, c, d, e, each covered on one side with fabric, sheet-metal, or ply-wood f, g, h, i. All the panels may be removably secured to the structure a by means of clamps, screws, bolts, or the like, or some only of the panels at places where easy access to the interior of the fuselage is desired, the remainder of the fuselage being provided with a non-removable covering. Each panel is reinforced by a lattice structure, or by profiled members, or by other means and may be mounted with its covered surface towards the interior of the fuselage. The panels may be interchangeable and some may be covered on both sides.
GB10875/32A 1932-04-15 1932-04-15 Improvements in or relating to aircraft fuselages and aircraft motor gondolas Expired GB404606A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10875/32A GB404606A (en) 1932-04-15 1932-04-15 Improvements in or relating to aircraft fuselages and aircraft motor gondolas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10875/32A GB404606A (en) 1932-04-15 1932-04-15 Improvements in or relating to aircraft fuselages and aircraft motor gondolas

Publications (1)

Publication Number Publication Date
GB404606A true GB404606A (en) 1934-01-18

Family

ID=9975930

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10875/32A Expired GB404606A (en) 1932-04-15 1932-04-15 Improvements in or relating to aircraft fuselages and aircraft motor gondolas

Country Status (1)

Country Link
GB (1) GB404606A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180022435A1 (en) * 2016-07-21 2018-01-25 The Boeing Company Space frame fuselage with pressure membrane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180022435A1 (en) * 2016-07-21 2018-01-25 The Boeing Company Space frame fuselage with pressure membrane
US10988231B2 (en) * 2016-07-21 2021-04-27 The Boeing Company Space frame fuselage with pressure membrane

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