GB164305A - Improvements in fuselages or hulls of aircraft - Google Patents

Improvements in fuselages or hulls of aircraft

Info

Publication number
GB164305A
GB164305A GB681821A GB681821A GB164305A GB 164305 A GB164305 A GB 164305A GB 681821 A GB681821 A GB 681821A GB 681821 A GB681821 A GB 681821A GB 164305 A GB164305 A GB 164305A
Authority
GB
United Kingdom
Prior art keywords
fuselages
hulls
aircraft
door
nose
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
GB681821A
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
Filing date
Publication date
Application filed by Zeppelinwerke GmbH filed Critical Zeppelinwerke GmbH
Publication of GB164305A publication Critical patent/GB164305A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/24Steps mounted on, and retractable within, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

164,305. Zeppelin-Werke Ges. June 4, 1920, [Convention date]. Fuselages. - T h e deor of a hull or fuselage is in the nose, or the entrance opening is otherwise in a plane normal to the direction of flight. The complete nose portion a may be adapted to serve as the door, being preferably hinged at its lower edge. Steps b may be formed inside the door to facilitate entrance.
GB681821A 1921-03-02 Improvements in fuselages or hulls of aircraft Expired GB164305A (en)

Publications (1)

Publication Number Publication Date
GB164305A true GB164305A (en) 1922-02-02

Family

ID=1628743

Family Applications (1)

Application Number Title Priority Date Filing Date
GB681821A Expired GB164305A (en) 1921-03-02 Improvements in fuselages or hulls of aircraft

Country Status (1)

Country Link
GB (1) GB164305A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2453937A (en) * 1947-04-23 1948-11-16 Southwest Airways Company Aircraft door

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2453937A (en) * 1947-04-23 1948-11-16 Southwest Airways Company Aircraft door

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