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

Improvements in variable sweep wing mechanism for aircraft

Info

Publication number
GB1020393A
GB1020393AGB219964AGB219964AGB1020393AGB 1020393 AGB1020393 AGB 1020393AGB 219964 AGB219964 AGB 219964AGB 219964 AGB219964 AGB 219964AGB 1020393 AGB1020393 AGB 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 LtdfiledCriticalBritish Aircraft Corp Operating Ltd
Priority to GB219964ApriorityCriticalpatent/GB1020393A/en
Publication of GB1020393ApublicationCriticalpatent/GB1020393A/en
Expiredlegal-statusCriticalCurrent

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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.
GB219964A1964-01-171964-01-17Improvements in variable sweep wing mechanism for aircraftExpiredGB1020393A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
GB219964AGB1020393A (en)1964-01-171964-01-17Improvements in variable sweep wing mechanism for aircraft

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
GB219964AGB1020393A (en)1964-01-171964-01-17Improvements in variable sweep wing mechanism for aircraft

Publications (1)

Publication NumberPublication Date
GB1020393Atrue GB1020393A (en)1966-02-16

Family

ID=9735334

Family Applications (1)

Application NumberTitlePriority DateFiling Date
GB219964AExpiredGB1020393A (en)1964-01-171964-01-17Improvements in variable sweep wing mechanism for aircraft

Country Status (1)

CountryLink
GB (1)GB1020393A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3565369A (en)*1968-04-181971-02-23British Aircraft Corp LtdAircraft having variable sweep-back wings
CN101767647A (en)*2010-03-022010-07-07北京航空航天大学Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN105620719A (en)*2016-03-162016-06-01舒丹丹Folding-wing unmanned aerial vehicle for municipal garden
CN105667788A (en)*2016-01-122016-06-15林建民Unmanned aerial vehicle
CN107472534A (en)*2016-02-252017-12-15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)*2016-03-302018-02-09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)*2020-04-152020-07-17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 numberPriority datePublication dateAssigneeTitle
US3565369A (en)*1968-04-181971-02-23British Aircraft Corp LtdAircraft having variable sweep-back wings
CN101767647A (en)*2010-03-022010-07-07北京航空航天大学Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN101767647B (en)*2010-03-022013-03-27北京航空航天大学Self-locking 90-degree full-wing variable sweepback transmission mechanism
CN105667788A (en)*2016-01-122016-06-15林建民Unmanned aerial vehicle
CN107472534A (en)*2016-02-252017-12-15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)*2016-03-162016-06-01舒丹丹Folding-wing unmanned aerial vehicle for municipal garden
CN107672807A (en)*2016-03-302018-02-09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)*2016-03-302018-03-20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)*2020-04-152020-07-17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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