GB279470A - Improvements in and relating to flying machines, helicopters and the like - Google Patents
Improvements in and relating to flying machines, helicopters and the likeInfo
- Publication number
- GB279470A GB279470A GB27896/27A GB2789627A GB279470A GB 279470 A GB279470 A GB 279470A GB 27896/27 A GB27896/27 A GB 27896/27A GB 2789627 A GB2789627 A GB 2789627A GB 279470 A GB279470 A GB 279470A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- rod
- sleeve
- blades
- ring
- 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
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
- B64C5/16—Stabilising surfaces adjustable about spanwise axes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/17—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
279,470. Perrin, E. A. Oct. 22, 1926, [Convention date]. . Screw and like propellers.-A helicopter supported by a single screw is provided with means for cyclically varying the pitch of the screw blades and means for varying the pitch of the screw as a whole. The blades of the propeller are pivoted about a tubular cross-piece 81 on a tubular shaft 54 which is surrounded near its lower end by a sleeve 59 carrying pawls 56 engaging a ratchet on a casing integral with a gear wheel 53 in mesh with a gear wheel 52 on the engine shaft. The sleeve 59 has a ring 60 notches to receive the ends of two levers 66 pivoted about a belt 67 extending through the shaft 54 and the lower ends of the levers engage inclined slots 68 in a sleeve 69 which can slide without relative rotation upon the shaft 54. When. this sleeve 69 is moved by a hand-lever 72 the sleeve 59 is turned relatively to the shaft 54 and this motion is transmitted to a tubular shaft 74 by means of a bolt 73 extending through oval holes in the shaft 54. The upper end of the shaft 74 carries a bail having cranked portions entering a ring 76 which carries arm 77 connected by short links to the under surfaces of the screw blades, so that the rotary movement of the shaft 74 is transmitted to the ring 76 and the pitch of the blades is varied equally. A joystick M is connected bv a link 141 to arm ML on a cross shaft having a lever 119 which moves a rod MLV connected through levers 131, 132 and rod OT to mechanism for moving a, frame 145, Fig. 13. This frame carries rollers 144 bearing on the ring 76 whereby the ring is displaced to cause a cyclical and opposite variation of the pitch of the screw blades which is a maximum as the blades pass through the transverse plane of the machine. This frame is also displaced through a, conection to the upper end of' the lever 131 when the hand-wheel 109 is turned, but at the, same time the bell crank 115 moves the rod MLV nearer to or further from the pivot of the lever 119 so that at high speeds the rod MLV is not movable by the joy-stick M. Lateral movements of the joystick M are transmitted through a rod 140, arm MT, and rod OL to arms 148, Fig. 13, connected to a sleeve 149 through which rods on the frame 145 can slide when moved by the rod OT. Movement of the rod OL moves the frame in a direction at right angles to that caused by the rod OT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR279470X | 1926-10-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB279470A true GB279470A (en) | 1928-04-19 |
Family
ID=8886668
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27896/27A Expired GB279470A (en) | 1926-10-22 | 1927-10-20 | Improvements in and relating to flying machines, helicopters and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB279470A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2249770A (en) * | 1990-11-19 | 1992-05-20 | Thomas Thomson Gardner | Helicopter downdraught controls |
-
1927
- 1927-10-20 GB GB27896/27A patent/GB279470A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2249770A (en) * | 1990-11-19 | 1992-05-20 | Thomas Thomson Gardner | Helicopter downdraught controls |
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