GB2545325B - An airframe for an air vehicle - Google Patents

An airframe for an air vehicle

Info

Publication number
GB2545325B
GB2545325B GB1618791.6A GB201618791A GB2545325B GB 2545325 B GB2545325 B GB 2545325B GB 201618791 A GB201618791 A GB 201618791A GB 2545325 B GB2545325 B GB 2545325B
Authority
GB
United Kingdom
Prior art keywords
airframe
air vehicle
vehicle
air
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.)
Active
Application number
GB1618791.6A
Other versions
GB2545325A (en
Inventor
James Price Howard
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Publication of GB2545325A publication Critical patent/GB2545325A/en
Application granted granted Critical
Publication of GB2545325B publication Critical patent/GB2545325B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
GB1618791.6A 2015-11-13 2016-11-08 An airframe for an air vehicle Active GB2545325B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1520030.6A GB201520030D0 (en) 2015-11-13 2015-11-13 An airframe for a air vehicle

Publications (2)

Publication Number Publication Date
GB2545325A GB2545325A (en) 2017-06-14
GB2545325B true GB2545325B (en) 2018-09-05

Family

ID=55132732

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB1520030.6A Ceased GB201520030D0 (en) 2015-11-13 2015-11-13 An airframe for a air vehicle
GB1618791.6A Active GB2545325B (en) 2015-11-13 2016-11-08 An airframe for an air vehicle

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB1520030.6A Ceased GB201520030D0 (en) 2015-11-13 2015-11-13 An airframe for a air vehicle

Country Status (1)

Country Link
GB (2) GB201520030D0 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3934845A (en) * 1975-03-17 1976-01-27 Northrop Corporation Gun bay pressure relief device
US20110265300A1 (en) * 2008-11-05 2011-11-03 Rolf Bense Device for temporarily fixing in position two fuselage sections to be joined
US20130020438A1 (en) * 2011-07-18 2013-01-24 The Boeing Company Flexible Truss Frame and Method of Making the Same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3934845A (en) * 1975-03-17 1976-01-27 Northrop Corporation Gun bay pressure relief device
US20110265300A1 (en) * 2008-11-05 2011-11-03 Rolf Bense Device for temporarily fixing in position two fuselage sections to be joined
US20130020438A1 (en) * 2011-07-18 2013-01-24 The Boeing Company Flexible Truss Frame and Method of Making the Same

Also Published As

Publication number Publication date
GB201520030D0 (en) 2015-12-30
GB2545325A (en) 2017-06-14

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