GB289517A - Improvements in or relating to the wings or supporting planes of aircraft - Google Patents

Improvements in or relating to the wings or supporting planes of aircraft

Info

Publication number
GB289517A
GB289517A GB2210/27A GB221027A GB289517A GB 289517 A GB289517 A GB 289517A GB 2210/27 A GB2210/27 A GB 2210/27A GB 221027 A GB221027 A GB 221027A GB 289517 A GB289517 A GB 289517A
Authority
GB
United Kingdom
Prior art keywords
flap
pilot
plane
movement
stop
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
GB2210/27A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2210/27A priority Critical patent/GB289517A/en
Publication of GB289517A publication Critical patent/GB289517A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/28Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/30Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

289,517. Wood, R. M. Jan. 25, 1927. Steering, balancing, and regulating altitude. -A pilot plane 1 is freely pivoted in advance of a main plane 4, so that at small incidences it sets itself as in Fig. 4 in the air stream, adding little to the drag, while at large incidences it rises as in Fig. 3 against a stop 6 to form a slot, which tends to maintain steady air flow over the upper surface. The pilot plane may extend only along the tip of the wing, and the stop 6 may be linked to the aileron. As shown in Fig. 7, downward movement of the aileron 12 from its neutral position lowers the upward limit of the pilot plane in a small degree, while upward movement of the aileron raises the limit in a greater degree. The link control may act in the opposite sense, as shown in Fig. 5. The stop 6 may be linked as in Fig 9 to a freely pivoted rear-flap 20, the movement of which is limited by check-wires 24, 25 or by stops. The flap 20 may be linked to the pilot plane itself, as in Fig. 14, so that as the pilot plane rises the flap is depressed; a slot may thus be opened between the main plane and flap, or the slot may be open in all positions of the flap. Automatic control of the camber of the wing, as in Fig. 14, may be combined with lateral control by enabling the pilot to superimpose a differential movement on the flap 20 of the two wings. Wires 16, 17 Fig. 15, from differentially geared pulleys are connected to the two flaps in such manner that these can only move up or down together while the control column 44 is held stationary, but movement of the column 44 superimposes an upward movement on one flap and a downward movement on the other. The same effect may be obtained by a lever 52, Fig. 17, pivoted on the control column 54 and connected by links to the flaps 33, 34. A pilot plane may be mounted in advance of a symmetrical aerofoil, such as a rudder, in which case it is pivoted one fifth of its chord behind its leading edge and a stop is provided on each side.
GB2210/27A 1927-01-25 1927-01-25 Improvements in or relating to the wings or supporting planes of aircraft Expired GB289517A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2210/27A GB289517A (en) 1927-01-25 1927-01-25 Improvements in or relating to the wings or supporting planes of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2210/27A GB289517A (en) 1927-01-25 1927-01-25 Improvements in or relating to the wings or supporting planes of aircraft

Publications (1)

Publication Number Publication Date
GB289517A true GB289517A (en) 1928-04-25

Family

ID=9735528

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2210/27A Expired GB289517A (en) 1927-01-25 1927-01-25 Improvements in or relating to the wings or supporting planes of aircraft

Country Status (1)

Country Link
GB (1) GB289517A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422296A (en) * 1941-08-22 1947-06-17 Curtiss Wright Corp Slat and flap control system
WO2015190124A1 (en) * 2014-06-13 2015-12-17 独立行政法人宇宙航空研究開発機構 Morphing wing
US9394046B2 (en) 2011-11-16 2016-07-19 Ecological Energy Company Fluid interface device as well as apparati and methods including same

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422296A (en) * 1941-08-22 1947-06-17 Curtiss Wright Corp Slat and flap control system
US9394046B2 (en) 2011-11-16 2016-07-19 Ecological Energy Company Fluid interface device as well as apparati and methods including same
WO2015190124A1 (en) * 2014-06-13 2015-12-17 独立行政法人宇宙航空研究開発機構 Morphing wing
JP2016002790A (en) * 2014-06-13 2016-01-12 国立研究開発法人宇宙航空研究開発機構 Morphing airfoil

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