| 摘要 |
<p>1,246,119. Change-speed control. CESSNA AIRCRAFT CO. 11 Sept., 1968 [23 Oct., 1967], No. 43134/68. Heading F2D. An infinitely variable transmission having its ratio changed by a fluid pressure servomotor is followed by a stepped change-speed gear, and the rate at which fluid is supplied to the servomotor is controlled in accordance with the ratio established in the change-speed gear. In operation a selected ratio is established in the stepped gear and the output speed is then increased by increasing the ratio of the infinitely variable transmission from zero or a minimum value to its maximum value, and the rate at which this is carried out is adjusted in accordance with the ratio established in the stepped gear to give, for example, constant acceleration, the output speed increasing from zero to a maximum of, say, 4 miles an hour in 4 seconds when first gear is established in the stepped gear, and the output speed increasing from zero to 12 miles an hour in 12 seconds when the second gear is established. As shown the infinitely variable transmission is of the hydrostatic type comprising a variable displacement swash-plate pump driving a variable (or fixed) displacement swash-plate motor, The pump and motor swash plates are controlled by double-acting servomotors 25, 26 controlled by a displacement control 27 to which liquid is supplied by a pump 30 at a rate determined by a valve 20. The valve 20 is linked to the gear lever of a stepped gear 16, and when first gear is established in the gear 16 the valve 20 is in the position shown giving relatively unrestricted flow to the displacement control 27 so that when a change of displacement is demanded by the control 27 the servos respond quickly. When second gear is established, the valve 20 is shifted rightwardly and flow to the control 27 is limited to that through a slot 48 in the valve so that the response is slower. In third gear the valve 20 is shifted to the left and flow passes through a smaller slot 49 to give a still slower response. The valve 20 need not be in the supply line to the control 27, it could be in the exhaust line 58 from the control 27, or individual valves 20 could be positioned in the supply lines 56, 60 or in the return lines 57, 61 between the control 27 and the servomotors. Various embodiments of the valve 20 are described, for example the valve spool may co-operate with different size passages provided in the valve housing, and the size of the passages may be adjustable by means of needle valves, or a rotary valve may be substituted for the axially slidable one described. In other modifications the hydrostatic transmission is replaced by expanding pulley gearing. In one form of expanding pulley gearing a driving pulley has one flange adjusted by a fluid pressure servomotor and a driven pulley has a spring biased flange. In another embodiment two adjustable pulleys are mounted on a common axis and co-operative respectively driving and driven pulleys, the axis of the adjustable pulley being respectively shiftable towards the driving and driven pulleys by a fluid pressure servomotor to change the ratio.</p> |
