GB201701491D0 - Space frame structure for an aircraft - Google Patents

Space frame structure for an aircraft

Info

Publication number
GB201701491D0
GB201701491D0 GBGB1701491.1A GB201701491A GB201701491D0 GB 201701491 D0 GB201701491 D0 GB 201701491D0 GB 201701491 A GB201701491 A GB 201701491A GB 201701491 D0 GB201701491 D0 GB 201701491D0
Authority
GB
United Kingdom
Prior art keywords
aircraft
frame structure
space frame
space
frame
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.)
Withdrawn
Application number
GBGB1701491.1A
Other versions
GB2559181A (en
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.)
Airbus Operations Ltd
Original Assignee
Airbus Operations Ltd
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 Airbus Operations Ltd filed Critical Airbus Operations Ltd
Priority to GB1701491.1A priority Critical patent/GB2559181A/en
Publication of GB201701491D0 publication Critical patent/GB201701491D0/en
Publication of GB2559181A publication Critical patent/GB2559181A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • F16B11/008—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing of tubular elements or rods in coaxial engagement
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
GB1701491.1A 2017-01-30 2017-01-30 Space frame structure for an aircraft Withdrawn GB2559181A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1701491.1A GB2559181A (en) 2017-01-30 2017-01-30 Space frame structure for an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1701491.1A GB2559181A (en) 2017-01-30 2017-01-30 Space frame structure for an aircraft

Publications (2)

Publication Number Publication Date
GB201701491D0 true GB201701491D0 (en) 2017-03-15
GB2559181A GB2559181A (en) 2018-08-01

Family

ID=58462826

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1701491.1A Withdrawn GB2559181A (en) 2017-01-30 2017-01-30 Space frame structure for an aircraft

Country Status (1)

Country Link
GB (1) GB2559181A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018160780A1 (en) * 2017-03-01 2018-09-07 Ford Global Technologies, Llc Method of assembly for 3d printed vehicle architecture, joints

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4041599A (en) * 1976-04-14 1977-08-16 Union Carbide Corporation Method of concentric bonding of a rod in a tubular shaft
GB2012649A (en) * 1977-12-22 1979-08-01 Gkn Transmissions Ltd Tubular shaft and universal joint assembly
US4352584A (en) * 1978-10-24 1982-10-05 Union Carbide Corporation Method of producing a joint capable of transmitting high torque
DE102004001386B3 (en) * 2004-01-09 2005-07-21 Universität Kassel Method for creating a plug connection by means of adhesive injection, as well as a male member and a hollow joining member therefor
FR3006726B1 (en) * 2013-06-05 2015-06-19 Hutchinson ROD, ITS MANUFACTURING METHOD AND AERONAUTICAL FLOOR STRUCTURE INCORPORATING IT.

Also Published As

Publication number Publication date
GB2559181A (en) 2018-08-01

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)