Patent GB-1125334-A (GB)
Title: Forward/reverse hydrokinetic transmission device
IPC: F16H61/50
Filed: 1966-03-16
Abstract: 1,125,334. Hydrodynamic forward/reverse transmission. BORG-WARNER CORP. 16 March, 1966 [10 Sept., 1965], No. 11567/66. Heading F2C. A Forward/Reverse hydrodynamic transmission device, particularly for small tractors and powered carts, comprises a selectively brakable flow reversing reactor C between the fluid exit of an input impeller A and the fluid entrance of an output turbine B, the reactor being permitted to rotate freely for forward, fluid coupling, drive of the turbine, or stationed, by a friction brake, to turn the fluid flow peripheral velocity component through approximately 180 degrees for reverse drive of the turbine. The converter element blade contours and torus geometry is such that the stall K- factor (input speed/square root of input torque) does not vary more than 20% in either direction of turbine rotation. The turbine B may be stationed by part braking of the reactor C. As shown, the impeller A comprises a cast shell 10 integral with a hub 17 which is secured, by a roll-pin 53c, to a V-belt sheave 51. The shell 10, together with a part 14 secured thereto, forms a housing surrounding the reactor C and the turbine B. The reactor is secured to one end of a sleeve shaft 41 the other end of which carries a sheet-metal brake disc 63, the latter having deformed fingers 65 keying into grooves in the shaft 41. An output shaft 54 is secured, by a roll-pin 58, to the turbine and, beyond the brake disc 63, to an auxiliary shaft portion 72. The sleeve shaft 41 is journalled on the output shaft 54 by a bush 56. Fluid seals are provided between the housing part 14 and a hardened wear tube 60 cast into the sleeve shaft 41, and between the shafts 41, 54. The brake 62 comprises the disc 63 and a caliper 67 having a brake actuating friction element 68. To prevent turbine creep during idling a brake similar to that 62 may be provided for the output shaft 54, such a brake including a sheet metal disc 69 having deformed fingers 71 keying into grooves in the shaft portion 72. The output shaft 54 is journalled in a recess of the hub 17 by thrust and journal roller bearings 55. The blades 28 of the turbine are shown secured to a turbine shell 24 by integral expanded rivets 28a. With the pump A and turbine B positioned as shown, the outwardly positioned reactor C may be disposed on the right (Fig. 4, not shown) or, as shown, the left of the toroid radial bisecting plane or, Fig. 3 (not shown), so disposed that the fluid entry and exit thereof lie respectively on opposite sides of said plane. In Fig. 6 (not shown), the input, output and brake connections extend on the same side of the device; and in Figs. 7, 8 (not shown), the pump and brake connections extend on the opposite side of the device to the turbine connection. As shown, cooling fins 82 are formed on the pumpattached housing part 14, whereas in Fig. 8 (not shown), smaller fins are formed on the turbineattached housing part, the cooling being aided by a fan connected to an input shaft. In Fig. 8 (not shown), the reactor is stationed by a drum brake. In a further embodiment, a reactorconnected housing may surround the impeller and the turbine. A pressure compensating flexible membrane 90 is provided which communicates on the one hand, through openings 19, with the pressure in the toroidal chamber D and on the other hand with atmospheric pressure in an open auxiliary chamber 95 bounded by a sheet-metal member 94 by which the membrane is locked in place. The device may be filled through an opening in the shell 10.