GB457454A - Improvements in and relating to aircraft controlling surfaces - Google Patents
Improvements in and relating to aircraft controlling surfacesInfo
- Publication number
- GB457454A GB457454A GB1532835A GB1532835A GB457454A GB 457454 A GB457454 A GB 457454A GB 1532835 A GB1532835 A GB 1532835A GB 1532835 A GB1532835 A GB 1532835A GB 457454 A GB457454 A GB 457454A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spar
- spars
- tail
- shaft
- fuselage
- 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
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/40—Application of doors, windows, wings or fittings thereof for gates
- E05Y2900/402—Application of doors, windows, wings or fittings thereof for gates for cantilever gates
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
457,454. Aircraft tail unit. BAYNES, L. E., 144, Cromwell Road, South Kensington, London. May 25, 1935, Nos. 15328 and 15329. [Class 4] An aircraft tail unit comprises a horizontal cantilever tail plane having a main and a subsidiary spar spaced apart at their roots and converging toward their tips where they are rigidly joined together, the spar roots being attached by quick release joints to the spars of a fixed fin. A fixed fin 4, Fig. 1, is built up on substantially vertical spars 2, 3 upstanding from the tail end of the fuselage 1, Fig. 2. Intermediate of its length spar 2 carries a spar root attachment comprising plates 8 extending outwardly on either side of the spar to engage similar fittings secured to main spar 6 of tail plane 7. Attachment is by upper and lower pairs of pins 9, 11. A similar fitting but providing for one securing pin on each side only, is carried by spar 3 and serves for securing rear spar 12. Spars 12 of the two tail planes are collinear. Elevators 16 are hinged to spars 12 by brackets 21, Fig. 4, embracing brackets 20 on the spars through which passes a torque tube 19. Spar 3 carries a shaft 23 adapted to mate with the ends of torque tubes 19 and to transmit rotation thereto through pins 25 engaging slots 26 formed in the tube ends. Fast on shaft 23 is a lever 27 connected by a substantially vertical link 28 to a bell-crank lever in the tail end of the fuselage and operatively connected to the pilot's elevator control. According to a modification, hinge pin 19 and operating shaft 23 may not be in alignment, a universal joint being incorporated in either or both of them so that they may be brought into local alignment for coupling together. Specification 432,301 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1532835A GB457454A (en) | 1935-05-25 | 1935-05-25 | Improvements in and relating to aircraft controlling surfaces |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1532835A GB457454A (en) | 1935-05-25 | 1935-05-25 | Improvements in and relating to aircraft controlling surfaces |
Publications (1)
Publication Number | Publication Date |
---|---|
GB457454A true GB457454A (en) | 1936-11-25 |
Family
ID=10057145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1532835A Expired GB457454A (en) | 1935-05-25 | 1935-05-25 | Improvements in and relating to aircraft controlling surfaces |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB457454A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
-
1935
- 1935-05-25 GB GB1532835A patent/GB457454A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
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