Patent GB-918935-A (GB)
Title: Improvements relating to propeller pitch controlling mechanism
IPC: B64C11/38
Filed: 1961-02-17
Abstract: 918,935. Variable pitch propellers. UNITED AIRCRAFT CORPORATION. Feb. 17, 1961 [Feb. 23, 1960], No. 6005/61. Class 114. A mechanism shown diagrammatically in Fig. 4 for a controllable pitch propeller having blades 14 comprises a pitch changing motor (not shown) controlled by a speed responsive governer 32 (via low and high pitch lines 34, 36 respectively), means 52, 54 locking the blades against pitch reducing movement, speed responsive means 62 independent of said governor and having a normal speed setting controlling the pitch lock means, and manually controlled means by which the blade pitch can be manually selected and the speed responsive means react to a predetermined higher speed setting. The speed responsive means 62 (shown in detail in Fig. 3) comprises a flap valve 78 operable by flyweights 72 against the force of springs 74, 214, 238 to control an orifice 80 to govern the position of a servo valve 82. The pitch lock means comprises teeth 52 on a member splined to the pitch changing mechanism and urged by springs 60 into engagement with fixed teeth 54, the teeth 52 being moved out of engagement by a piston 56 actuated by pressure in a chamber 58. During static condition chamber 58 is void of fluid pressure (being connected via line 92 through valve 82 to drain line 96) hence the pitch lock will be in engagement and furthermore it is impossible to set the blades at a lower pitch since spring pressure urges a pressurizing valve 100 to the right to block flow from governor 32 and low pitch line 34 to low pitch line 43 and the pitch changing mechanism. As the propeller speeds up, pressure increases in lines 34, 121 to shift a valve 84 so that fluid flows via lines 86, 120 to annulus 119, through passage 117 to lines 124, 230 and chamber 106 to urge the spring loaded servo valve 82 to the right, connecting line 86 to line 92 allowing pressure to build up in chamber 58 to move the piston 56 and disengage the pitch lock. When this occurs, pressure in annulus 119 moves valve 100 to the left to connect low pitch lines 34 to the pitch changing mechanism via line 43. Overspeed causes the flyweights 72 to lift the spring loaded valve 78 so that fluid supplied to the chamber 104 in the pitch lock control 62 at a predetermined pressure from the valve 100 via line 124, enters the servo valve 82 and moves it to the left thus connecting chamber 58 and line 92 to the drain line 96 to allow springs 60 to engage the pitch lock. A lever 246 has a first range in which it controls the movement of the propeller between feathering and high pitch, a second in which it places the propeller under governor control and adjusts the governor setting as well as the flow of fuel to the turbine, and a third in which it manually positions the propeller blades, and in which the control 612 is effective. Follow up mechanisms are shown at 249 and 258. Movement of the lever 246 into the third range opens a valve 204 allowing fluid in a pressure line 202 to flow through line 206 to shift the spring loaded plunger 208 of a valve 200 to the right so that pressure fluid is fed through line 216 (Figs. 4 and 3) to the chamber 210 of a piston or plunger 212 to move same to the left, compressing spring 214 to increase the force which must be overcome by the flyweights 72, thereby altering the speed setting of the pitch lock governor 62. Specifications 683,906, 738,624, 754,095 and 886,256 are referred to.