GB157269A - Improvements in monoplane flying machines - Google Patents

Improvements in monoplane flying machines

Info

Publication number
GB157269A
GB157269A GB1163/21A GB116321A GB157269A GB 157269 A GB157269 A GB 157269A GB 1163/21 A GB1163/21 A GB 1163/21A GB 116321 A GB116321 A GB 116321A GB 157269 A GB157269 A GB 157269A
Authority
GB
United Kingdom
Prior art keywords
fuselage
planes
plane
forces acting
monoplane
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
GB1163/21A
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.)
Zeppelin GmbH
Original Assignee
Zeppelinwerke 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 Zeppelinwerke GmbH filed Critical Zeppelinwerke GmbH
Publication of GB157269A publication Critical patent/GB157269A/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)
  • Bridges Or Land Bridges (AREA)

Abstract

157,269. Zeppelin-Werke Ges., and Rohrbach, A. Oct. 15, 1919, [Convention date]. Planes, construction of and connecting to machine; propelling; tanks and like containers, arrangement and disposition of.-The planes of monoplanes are rigid with the fuselage, and are stiffened against forces acting from above by an internal girder extending from one wing to the other and against forces acting from below by tension cables 4. Turning moments about an axis transverse to the direction of flight are counteracted by forming the internal girder as a boxshaped member by connecting two beams together. The plane 1 may be connected to the fuselage 2 by a frame 3, Fig. 1, or it may be connected thereto as shown in Fig. 3, to give access to the motors and the fuel and oil tanks when carried within the plane.
GB1163/21A 1919-10-15 1921-01-10 Improvements in monoplane flying machines Expired GB157269A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE157269X 1919-10-15

Publications (1)

Publication Number Publication Date
GB157269A true GB157269A (en) 1922-07-10

Family

ID=5678497

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1163/21A Expired GB157269A (en) 1919-10-15 1921-01-10 Improvements in monoplane flying machines

Country Status (1)

Country Link
GB (1) GB157269A (en)

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