GB273745A - Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes - Google Patents
Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanesInfo
- Publication number
- GB273745A GB273745A GB17544/27A GB1754427A GB273745A GB 273745 A GB273745 A GB 273745A GB 17544/27 A GB17544/27 A GB 17544/27A GB 1754427 A GB1754427 A GB 1754427A GB 273745 A GB273745 A GB 273745A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- spider
- spring
- pivoted
- releases
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
- B64C27/021—Rotor or rotor head construction
- B64C27/026—Devices for converting a fixed wing into an autorotation rotor and viceversa
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pivots And Pivotal Connections (AREA)
- Hinge Accessories (AREA)
Abstract
273,745. Ehmig, V., and Hofmann, F. July 1, 1926, [Convention date]. Helicopters; stopping way. - An aeroplane has a series of planes normally housed in a recess in one of the m a i n planes but adapted to be released to form a rotary retarding surface above the machine. In the case of a biplane additional surfaces are housed in the lower plane and hinge upwards into the air stream when released. Fig. 3 shows the machine after planes 7, 8 have been withdrawn from a recess 5 in the upper plane of a biplane to form a rotary retarding device, and after planes 9 have been permitted to rise against stops on the plane bracing. A streamlined central tube 3, Fig. 7, is secured to a frame 14 pivoted to the aircraft at 15 and having a pin 16 at its forward end normally locked at the lower end of a slot 17 on the aircraft frame by a hook 51. Two pairs of planes 7, 8 have central ribs pivoted respectively to two rings 12, 13 rotating about ball bearings provided on the central column. A spider 20 capable of sliding within the column has parts extending through slots 21 and carries ball races for the two rings 23, 26 carrying links 25, 27 which are pivoted to the central ribs of the planes 7, 8. Half-way slots are formed in the planes as shown in Fig. 10 to permit the passage of the links 25, 27. The spider has two projections 32 normally engaged by pivoted hooks 33, but when a cam 36 is moved by the pilot, the lower ends of the hooks are drawn together by a spring 45 to release the projections 32, and the spider 20 is raised by a spring 19 to raise the planes 7, 8. Simultaneously a spring 28 swings the pairs of planes into a position at right-angles to one another. Another cam 43 releases the hook 51 to enable the frame 14 to swing upwards until the pin 16 engages pawls 60 at the top of the slot 17 and simultaneously another hook 52 releases a spring-influenced lever 54 to turn a shaft 56 which releases the planes 9. Portions of the planes as shown at 8b, Fig. 10, may be given an inclination by varying the length of struts 61 to cause the planes 7, 8 to rotate. A screw 63 enables the spider 20 to be forced into its normal position again.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR273745X | 1926-07-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB273745A true GB273745A (en) | 1928-06-21 |
Family
ID=8886157
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB17544/27A Expired GB273745A (en) | 1926-07-01 | 1927-07-01 | Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB273745A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103523199A (en) * | 2013-09-29 | 2014-01-22 | 郭献民 | Novel tubular-structure electric unmanned helicopter |
-
1927
- 1927-07-01 GB GB17544/27A patent/GB273745A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103523199A (en) * | 2013-09-29 | 2014-01-22 | 郭献民 | Novel tubular-structure electric unmanned helicopter |
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