GB2138756B - Wing leading edge slat - Google Patents

Wing leading edge slat

Info

Publication number
GB2138756B
GB2138756B GB08311294A GB8311294A GB2138756B GB 2138756 B GB2138756 B GB 2138756B GB 08311294 A GB08311294 A GB 08311294A GB 8311294 A GB8311294 A GB 8311294A GB 2138756 B GB2138756 B GB 2138756B
Authority
GB
United Kingdom
Prior art keywords
leading edge
wing leading
edge slat
slat
wing
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
GB08311294A
Other versions
GB2138756A (en
GB8311294D0 (en
Inventor
Arthur Evans
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to GB08311294A priority Critical patent/GB2138756B/en
Publication of GB8311294D0 publication Critical patent/GB8311294D0/en
Publication of GB2138756A publication Critical patent/GB2138756A/en
Application granted granted Critical
Publication of GB2138756B publication Critical patent/GB2138756B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • Y02T50/10—Drag reduction
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Blinds (AREA)
GB08311294A 1983-04-26 1983-04-26 Wing leading edge slat Expired GB2138756B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08311294A GB2138756B (en) 1983-04-26 1983-04-26 Wing leading edge slat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08311294A GB2138756B (en) 1983-04-26 1983-04-26 Wing leading edge slat

Publications (3)

Publication Number Publication Date
GB8311294D0 GB8311294D0 (en) 1983-06-02
GB2138756A GB2138756A (en) 1984-10-31
GB2138756B true GB2138756B (en) 1986-07-16

Family

ID=10541687

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08311294A Expired GB2138756B (en) 1983-04-26 1983-04-26 Wing leading edge slat

Country Status (1)

Country Link
GB (1) GB2138756B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3683140B1 (en) 2019-01-18 2022-10-12 Asco Industries NV Slat for an aircraft wing, method for manufacturing such a slat

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9703683D0 (en) * 1997-02-21 1997-04-09 Broadbent Michael C Interconnection system for slat/flap deployment
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
US6802475B2 (en) 2002-07-04 2004-10-12 Smiths Wolverhampton Limited Flight surface actuator
GB0215522D0 (en) * 2002-07-04 2002-08-14 Smiths Wolverhampton Ltd Flight surface actuator
DE102007020870A1 (en) * 2007-05-04 2008-11-13 Airbus Deutschland Gmbh High-lift system on the wing of an aircraft
TR201910783T4 (en) 2015-06-18 2019-08-21 Bae Systems Plc Aircraft wing system.
ES2746872T3 (en) 2015-06-18 2020-03-09 Bae Systems Plc Wing system of an aircraft
EP3378760A1 (en) 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
EP3378762A1 (en) * 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3683140B1 (en) 2019-01-18 2022-10-12 Asco Industries NV Slat for an aircraft wing, method for manufacturing such a slat

Also Published As

Publication number Publication date
GB2138756A (en) 1984-10-31
GB8311294D0 (en) 1983-06-02

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Legal Events

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