GB1020393A - Improvements in variable sweep wing mechanism for aircraft - Google Patents

Improvements in variable sweep wing mechanism for aircraft

Info

Publication number
GB1020393A
GB1020393A GB219964A GB219964A GB1020393A GB 1020393 A GB1020393 A GB 1020393A GB 219964 A GB219964 A GB 219964A GB 219964 A GB219964 A GB 219964A GB 1020393 A GB1020393 A GB 1020393A
Authority
GB
United Kingdom
Prior art keywords
aircraft
tracks
carriage
wing
variable
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
GB219964A
Inventor
Charles Frederick Toms
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp Operating Ltd
British Aircraft Corp 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 British Aircraft Corp Operating Ltd, British Aircraft Corp Ltd filed Critical British Aircraft Corp Operating Ltd
Priority to GB219964A priority Critical patent/GB1020393A/en
Publication of GB1020393A publication Critical patent/GB1020393A/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
    • B64C3/40—Varying angle of sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

1,020,393. Variable-geometry aircraft. BRITISH AIRCRAFT CORPORATION (OPERATING) Ltd. Jan. 18, 1965 [Jan. 17, 1964], No. 2199/64. Headings B7G and B7W. [Also in Division F2] In an aircraft having variable-geometry wings, which may be operated in the manner described in Specification 972,268, the wing pivots 2 are carried by a carriage 3, the ends of which engage in longitudinal tracks 4, the sweep angle being determined by wing-mounted pins 6 engaging fixed tracks 7. Each extremity of carriage 3 carries three rollers 10 recessed both in the carriage and in the tracks 4, the rollers being driven before and during wing sweep through gearing 14, 15 and motor 16. In a further embodiment the driving pinions are mounted on splined shafts which extend the length of tracks 4 and are driven in unison through further gearing and a single motor.
GB219964A 1964-01-17 1964-01-17 Improvements in variable sweep wing mechanism for aircraft Expired GB1020393A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB219964A GB1020393A (en) 1964-01-17 1964-01-17 Improvements in variable sweep wing mechanism for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB219964A GB1020393A (en) 1964-01-17 1964-01-17 Improvements in variable sweep wing mechanism for aircraft

Publications (1)

Publication Number Publication Date
GB1020393A true GB1020393A (en) 1966-02-16

Family

ID=9735334

Family Applications (1)

Application Number Title Priority Date Filing Date
GB219964A Expired GB1020393A (en) 1964-01-17 1964-01-17 Improvements in variable sweep wing mechanism for aircraft

Country Status (1)

Country Link
GB (1) GB1020393A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3565369A (en) * 1968-04-18 1971-02-23 British Aircraft Corp Ltd Aircraft having variable sweep-back wings
CN101767647A (en) * 2010-03-02 2010-07-07 北京航空航天大学 Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN105620719A (en) * 2016-03-16 2016-06-01 舒丹丹 Folding-wing unmanned aerial vehicle for municipal garden
CN105667788A (en) * 2016-01-12 2016-06-15 林建民 Unmanned aerial vehicle
CN107472534A (en) * 2016-02-25 2017-12-15 陈国栋 Flying Camera head can freely convert take photo by plane unmanned plane and its method for work of shooting angle
CN107672807A (en) * 2016-03-30 2018-02-09 苏州巴涛信息科技有限公司 A kind of auto-changing wing sweep angle municipal administration afforestation folding wings unmanned plane
CN111422375A (en) * 2020-04-15 2020-07-17 中国飞机强度研究所 Active control method and system for load of vertical constraint point of airplane

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3565369A (en) * 1968-04-18 1971-02-23 British Aircraft Corp Ltd Aircraft having variable sweep-back wings
CN101767647A (en) * 2010-03-02 2010-07-07 北京航空航天大学 Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN101767647B (en) * 2010-03-02 2013-03-27 北京航空航天大学 Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN105667788A (en) * 2016-01-12 2016-06-15 林建民 Unmanned aerial vehicle
CN107472534A (en) * 2016-02-25 2017-12-15 陈国栋 Flying Camera head can freely convert take photo by plane unmanned plane and its method for work of shooting angle
CN105620719A (en) * 2016-03-16 2016-06-01 舒丹丹 Folding-wing unmanned aerial vehicle for municipal garden
CN107672807A (en) * 2016-03-30 2018-02-09 苏州巴涛信息科技有限公司 A kind of auto-changing wing sweep angle municipal administration afforestation folding wings unmanned plane
CN107813922A (en) * 2016-03-30 2018-03-20 苏州巴涛信息科技有限公司 Auto-changing wing sweep angle municipal administration afforestation folding wings unmanned plane
CN111422375A (en) * 2020-04-15 2020-07-17 中国飞机强度研究所 Active control method and system for load of vertical constraint point of airplane

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