GB620863A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB620863A
GB620863A GB2507/47A GB250747A GB620863A GB 620863 A GB620863 A GB 620863A GB 2507/47 A GB2507/47 A GB 2507/47A GB 250747 A GB250747 A GB 250747A GB 620863 A GB620863 A GB 620863A
Authority
GB
United Kingdom
Prior art keywords
spaced
members
beam portions
aircraft
lattice
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
GB2507/47A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2507/47A priority Critical patent/GB620863A/en
Priority to ES0178645A priority patent/ES178645A1/en
Publication of GB620863A publication Critical patent/GB620863A/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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • 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)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Vibration Dampers (AREA)

Abstract

620,863. Aircraft framework. MENDELSSOHN, H. E. Jan. 27, 1947, No. 2507. [Class 4] An aircraft fuselage has at least one upper longitudinal beam and at least one lower longitudinal beam interconnected by transverse ribs, each beam being formed compositely from spaced beam portions held in spaced relation by strip lattice-work. The spaced beam portions 6, 7 of the lower longitudinal beams 3, 4 are composed of laminated strips secured together and are secured in spaced relation by lattice strip members 8, 9. Associated with the lower beam portions 7 are longitudinal members 11 of rubber formed with integral bosses 12 to which are attached oleo-struts 12a, the whole forming a continuous impactabsorbing gear. Floor sections 25 pivoted on transverse axes and shutter members 27, 28 allow easy egress to be obtained. Skylight panels 24 also provide readily available emergency exits.
GB2507/47A 1947-01-27 1947-01-27 Improvements in or relating to aircraft Expired GB620863A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB2507/47A GB620863A (en) 1947-01-27 1947-01-27 Improvements in or relating to aircraft
ES0178645A ES178645A1 (en) 1947-01-27 1947-06-26 IMPROVEMENTS IN AIRCRAFT CONSTRUCTION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2507/47A GB620863A (en) 1947-01-27 1947-01-27 Improvements in or relating to aircraft

Publications (1)

Publication Number Publication Date
GB620863A true GB620863A (en) 1949-03-31

Family

ID=9740774

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2507/47A Expired GB620863A (en) 1947-01-27 1947-01-27 Improvements in or relating to aircraft

Country Status (2)

Country Link
ES (1) ES178645A1 (en)
GB (1) GB620863A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2827251A (en) * 1952-04-02 1958-03-18 Doman Helicopters Inc Aircraft frame with large side openings
WO2007141176A1 (en) * 2006-06-02 2007-12-13 Airbus Deutschland Gmbh Fuselage structure and method for the production of a fuselage structure
DE102010014638A1 (en) * 2010-04-12 2011-10-13 Premium Aerotec Gmbh Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage
FR2969119A1 (en) * 2010-12-17 2012-06-22 Airbus Operations Sas FRONT PART OF AN AIRCRAFT FUSELAGE INTEGRATING A LANDING TRAIN STORAGE BOX
CN112027053A (en) * 2020-09-10 2020-12-04 中国航空工业集团公司沈阳飞机设计研究所 Framework structure of frame beam of middle fuselage of airplane

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2398287B1 (en) 2010-03-29 2014-01-29 Airbus Operations S.L. FUSELAGE OF AIRCRAFT RESISTANT TO IMPACT AND TOLERANT TO DAMAGE.

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2827251A (en) * 1952-04-02 1958-03-18 Doman Helicopters Inc Aircraft frame with large side openings
WO2007141176A1 (en) * 2006-06-02 2007-12-13 Airbus Deutschland Gmbh Fuselage structure and method for the production of a fuselage structure
US8444088B2 (en) 2006-06-02 2013-05-21 Airbus Operations Gmbh Fuselage structure and method for the production of a fuselage structure
DE102010014638A1 (en) * 2010-04-12 2011-10-13 Premium Aerotec Gmbh Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage
US9162745B2 (en) 2010-04-12 2015-10-20 Premium Aerotec Gmbh Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a fuselage
DE102010014638B4 (en) 2010-04-12 2019-08-01 Airbus Defence and Space GmbH Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage
FR2969119A1 (en) * 2010-12-17 2012-06-22 Airbus Operations Sas FRONT PART OF AN AIRCRAFT FUSELAGE INTEGRATING A LANDING TRAIN STORAGE BOX
US8840066B2 (en) 2010-12-17 2014-09-23 Airbus Operations S.A.S. Front part of an aircraft fuselage incorporating a bay for stowing landing gear
CN112027053A (en) * 2020-09-10 2020-12-04 中国航空工业集团公司沈阳飞机设计研究所 Framework structure of frame beam of middle fuselage of airplane

Also Published As

Publication number Publication date
ES178645A1 (en) 1947-08-16

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