GB620860A - Aircraft wing flap assembly - Google Patents
Aircraft wing flap assemblyInfo
- Publication number
- GB620860A GB620860A GB249647A GB249647A GB620860A GB 620860 A GB620860 A GB 620860A GB 249647 A GB249647 A GB 249647A GB 249647 A GB249647 A GB 249647A GB 620860 A GB620860 A GB 620860A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rods
- rod
- flap
- hydraulic jack
- radius
- 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
- B64C9/32—Air braking surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
- B64C9/323—Air braking surfaces associated with wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
620,860. Wing flaps. MOORE, W. H. Jan. 27, 1947, No. 2496. [Class 4] A flap comprises three or more pivotally interconnected spanwise strips forming an articulated unit pivotally attached along one edge 42 to the wing 1, the flap being raised or lowered by a series of radius rods 15, 16, 17, 18 actuated by a hydraulic jack 6, 7. The rod 6 of the jack carries a cross-piece 9 to which rods 10, 11, 12, 13 are attached. The rod 10 carries a member 31 to which the lower end of the radius rod 15 is pivoted, while the rods 11, 12, 13 carry further members 32, 33, 34 which successively engage blocks 24, 25, 26, to which the rods 16, 17, 18 are pivoted, when the hydraulic jack is extended. Projections at the upper ends of the members 31, 32, 33, 34 engage the rear faces of the radius rods when the flap is fully raised, Fig. 5. Manually operated rack and pinion, or screw drive, may be substituted for the hydraulic jack.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB249647A GB620860A (en) | 1947-01-27 | 1947-01-27 | Aircraft wing flap assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB249647A GB620860A (en) | 1947-01-27 | 1947-01-27 | Aircraft wing flap assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
GB620860A true GB620860A (en) | 1949-03-31 |
Family
ID=9740590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB249647A Expired GB620860A (en) | 1947-01-27 | 1947-01-27 | Aircraft wing flap assembly |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB620860A (en) |
-
1947
- 1947-01-27 GB GB249647A patent/GB620860A/en not_active Expired
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