GB592368A - Improvements in or relating to arrangements for securing and controlling a movable flap at the trailing edge of an airplane wing - Google Patents
Improvements in or relating to arrangements for securing and controlling a movable flap at the trailing edge of an airplane wingInfo
- Publication number
- GB592368A GB592368A GB11218/45A GB1121845A GB592368A GB 592368 A GB592368 A GB 592368A GB 11218/45 A GB11218/45 A GB 11218/45A GB 1121845 A GB1121845 A GB 1121845A GB 592368 A GB592368 A GB 592368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rod
- flap
- trailing edge
- controlling
- securing
- 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
- 239000000725 suspension Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
592,368. Controlling aircraft. SOC; NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU SUD-OUEST. May 3, 1945, No. 11218. Convention date; Nov. 23, 1944. [Class 4] A flap a; e.g. an aileron, is suspended from the trailing edge of an aeroplane wing by links band h, and is actuated by rods l. n and s connected by bell-crank levers o, p and t to a slidable rod m operated by an electric motor or jack u. The arm of the lever t is longer than the arms of the levers o and p, and the point of connection r of the rod s to the flap is displaced from the suspension axis; so that, on actuation of the rod m, the flap is given a combined rearward and rotational movement. The ends of the link h and rod s are provided with ball-joints ; the link b has a ball-joint at its lower end but is connected to the wing at its upper end by an elongated pivot g,to prevent lateral movement of the flap. The links band h may be adjustable in length and more than one rod s may be provided.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR592368X | 1944-11-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB592368A true GB592368A (en) | 1947-09-16 |
Family
ID=8964762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB11218/45A Expired GB592368A (en) | 1944-11-23 | 1945-05-03 | Improvements in or relating to arrangements for securing and controlling a movable flap at the trailing edge of an airplane wing |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB592368A (en) |
-
1945
- 1945-05-03 GB GB11218/45A patent/GB592368A/en not_active Expired
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