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 aircraftInfo
- 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
Links
Classifications
-
- 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
-
- 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
- B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
-
- 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)
- 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.
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)
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 |
-
1927
- 1927-01-25 GB GB2210/27A patent/GB289517A/en not_active Expired
Cited By (4)
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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