GB2471408B - Leading edge element of aircraft, method for manufacturing one, wing and stabilizer - Google Patents

Leading edge element of aircraft, method for manufacturing one, wing and stabilizer

Info

Publication number
GB2471408B
GB2471408B GB1015661A GB201015661A GB2471408B GB 2471408 B GB2471408 B GB 2471408B GB 1015661 A GB1015661 A GB 1015661A GB 201015661 A GB201015661 A GB 201015661A GB 2471408 B GB2471408 B GB 2471408B
Authority
GB
United Kingdom
Prior art keywords
wing
aircraft
stabilizer
manufacturing
leading edge
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 - Fee Related
Application number
GB1015661A
Other versions
GB201015661D0 (en
GB2471408A (en
Inventor
Juha Maekelae
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.)
Patria Aerostructures Oy
Original Assignee
Patria Aerostructures Oy
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 Patria Aerostructures Oy filed Critical Patria Aerostructures Oy
Priority to GB1015661A priority Critical patent/GB2471408B/en
Priority claimed from GB1014846.8A external-priority patent/GB2470524B/en
Publication of GB201015661D0 publication Critical patent/GB201015661D0/en
Publication of GB2471408A publication Critical patent/GB2471408A/en
Application granted granted Critical
Publication of GB2471408B publication Critical patent/GB2471408B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
GB1015661A 2009-03-12 2009-03-12 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer Expired - Fee Related GB2471408B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1015661A GB2471408B (en) 2009-03-12 2009-03-12 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1015661A GB2471408B (en) 2009-03-12 2009-03-12 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer
GB1014846.8A GB2470524B (en) 2008-03-13 2009-03-12 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer

Publications (3)

Publication Number Publication Date
GB201015661D0 GB201015661D0 (en) 2010-10-27
GB2471408A GB2471408A (en) 2010-12-29
GB2471408B true GB2471408B (en) 2011-03-09

Family

ID=43065459

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1015661A Expired - Fee Related GB2471408B (en) 2009-03-12 2009-03-12 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer

Country Status (1)

Country Link
GB (1) GB2471408B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201120707D0 (en) 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
FR2993857B1 (en) 2012-07-26 2015-03-27 Airbus Operations Sas DEVICE FOR PROTECTING A LONGERON STRUCTURE BEFORE A CENTRAL AIRCRAFT WING BOX AND AT LEAST ONE EQUIPMENT LOCATED IN THE SAME
ES2764122T3 (en) * 2016-12-02 2020-06-02 Airbus Operations Sl Integration of the leading edge of an aircraft stabilizer with the torsion box and the fuselage
US11046420B2 (en) 2019-10-23 2021-06-29 The Boeing Company Trailing edge flap having a waffle grid interior structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB339132A (en) * 1928-12-20 1930-12-04 Nieuport Astra Improvements in or relating to airplane construction
JP2003291895A (en) * 2002-04-05 2003-10-15 Japan Aircraft Mfg Co Ltd Aircraft wing leading edge and method of manufacturing the same
EP2130762A2 (en) * 2008-05-06 2009-12-09 Alenia Aeronautica S.P.A. Wing and empennage leading edge structure made of thermoplastic material with a stiffened double-shell configuration
EP2196391A2 (en) * 2008-12-15 2010-06-16 EMBRAER - Empresa Brasileira de Aeronáutica S.A. Impact resistant aircraft leading edge structures and aircraft including the same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB339132A (en) * 1928-12-20 1930-12-04 Nieuport Astra Improvements in or relating to airplane construction
JP2003291895A (en) * 2002-04-05 2003-10-15 Japan Aircraft Mfg Co Ltd Aircraft wing leading edge and method of manufacturing the same
EP2130762A2 (en) * 2008-05-06 2009-12-09 Alenia Aeronautica S.P.A. Wing and empennage leading edge structure made of thermoplastic material with a stiffened double-shell configuration
EP2196391A2 (en) * 2008-12-15 2010-06-16 EMBRAER - Empresa Brasileira de Aeronáutica S.A. Impact resistant aircraft leading edge structures and aircraft including the same

Also Published As

Publication number Publication date
GB201015661D0 (en) 2010-10-27
GB2471408A (en) 2010-12-29

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20190312