Hydraulic radial piston device with improved pressure transition mechanism

A hydraulic radial piston device comprising:

• a housing having a hydraulic fluid inlet and a hydraulic fluid outlet;
• a pintle shaft fixed within the housing, the pintle shaft having an outer circumferential surface defining a fluid inlet section, a fluid precompression section, a fluid outlet section, and a fluid decompression section, the pintle shaft including a pintle inlet defined in the fluid inlet section and a pintle outlet defined in the fluid outlet section, the pintle inlet being in fluid communication with the hydraulic fluid inlet, and the pintle outlet being in fluid communication with the hydraulic fluid outlet;
• a rotor mounted on the pintle shaft and configured to rotate relative to the pintle shaft about a rotor axis of rotation, the rotor axis of rotation extending through a length of the pintle shaft, the rotor defining a plurality of radially oriented cylinders and a plurality of rotor fluid ports, each of the plurality of rotor fluid ports being in fluid communication with at least one of the plurality of radially oriented cylinders and moving on the outer circumferential surface of the pintle shaft to pass the fluid inlet section, the fluid precompression section, the fluid outlet section, and the fluid decompression section as the rotor rotates relative to the pintle shaft about the rotor axis of rotation;
• a plurality of pistons received in the plurality of radially oriented cylinders, respectively;
• a thrust ring disposed about the rotor and having a thrust ring axis of rotation, the thrust ring being in contact with the plurality of pistons and configured to rotate about the thrust ring axis of rotation as the rotor rotates relative to the pintle shaft about the rotor axis of rotation;
• and
• a ring displacement driver operable to displace the thrust ring through a range of movement within the housing between a first position in which the radial piston device provides a minimum displacement of hydraulic fluid per each rotation of the rotor and a second position in which the radial piston device provides a maximum displacement of hydraulic fluid per each rotation of the rotor,
• wherein, when the each of the plurality of rotor fluid ports passes the fluid inlet section, each of the plurality of rotor fluid ports is in fluid communication with the pintle inlet at the fluid inlet section to draw hydraulic fluid into one or more cylinders associated with the rotor fluid port through the pintle inlet;
• wherein, when the each of the plurality of rotor fluid ports passes the fluid precompression section, each of the plurality of rotor fluid ports is closed to trap and compress the hydraulic fluid within the cylinders at the fluid precompression section;
• wherein, when the each of the plurality of rotor fluid ports passes the fluid outlet section, the each of the plurality of rotor fluid ports is in fluid communication with the pintle outlet at the fluid outlet section to discharge the hydraulic fluid from the cylinders through the pintle outlet;
• and
• wherein, when the each of the plurality of rotor fluid ports passes the fluid decompression section, the each of the plurality of rotor fluid ports is closed to decompress the cylinders at the fluid decompression section,
• wherein an eccentricity reference line defined through the rotor axis of rotation and the thrust ring axis of rotation rotates about the rotor axis of rotation as the thrust ring is moved through the range of movement such that the thrust ring axis of rotation remains in offset relation relative to the rotor axis of rotation to provide a consistent precompression stroke distance and a consistent decompression stroke distance of each of the plurality of pistons regardless of a position of the thrust ring in the range of movement of the thrust ring within the housing, thereby providing a smooth pressure transition in the each of the plurality of radially oriented cylinders,
• wherein adjustment of a position of the thrust ring along the range of movement adjusts a volume of hydraulic fluid displaced by the radial piston device for each rotation of the rotor by moving the thrust ring axis of rotation further from the rotor axis of rotation as the thrust ring is moved toward the second position so as to increase a stroke length of the pistons within the cylinders, and by moving the thrust ring axis of rotation closer to the rotor axis of rotation as the thrust ring is moved toward the first position so as to decrease a stroke length of the pistons within the cylinders.

A hydraulic radial piston device comprising:

• a housing having a hydraulic fluid inlet and a hydraulic fluid outlet;
• a pintle shaft fixed within the housing, the pintle shaft defining a pintle inlet and a pintle outlet, the pintle inlet being in fluid communication with the hydraulic fluid inlet, and the pintle outlet being in fluid communication with the hydraulic fluid outlet;
• a rotor mounted on the pintle shaft and configured to rotate relative to the pintle shaft about a rotor axis of rotation, the rotor axis of rotation extending through a length of the pintle shaft, the rotor defining a plurality of radially oriented cylinders and a plurality of rotor fluid ports, each of the plurality of rotor fluid ports being in fluid communication with at least one of the plurality of radially oriented cylinders and being alternatively in fluid communication with either the pintle inlet or the pintle outlet as the rotor rotates relative to the pintle shaft about the rotor axis of rotation;
• a plurality of pistons received in the plurality of radially oriented cylinders, respectively;
• a thrust ring disposed about the rotor and having a thrust ring axis of rotation, the thrust ring being in contact with the plurality of pistons and configured to rotate about the thrust ring axis of rotation as the rotor rotates relative to the pintle shaft about the rotor axis of rotation;
• and
• a ring displacement driver configured to displace the thrust ring into different positions within the housing between a first position in which the radial piston device is in a minimum displacement operation and a second position in which the radial piston device is in a maximum displacement operation, to produce different flow rates of the hydraulic fluid, wherein, when the thrust ring is in a position other than the minimum displacement position, the ring displacement driver displaces the thrust ring to offset the thrust ring axis of rotation from the rotor axis of rotation such that each of the plurality of pistons radially reciprocates within the associated cylinder and repeatedly passes through a cycle of a fluid inlet stage, a compression stage, a fluid outlet stage, and a decompression stage as the rotor rotates relative to the pintle shaft about the rotor axis of rotation, wherein, in the fluid inlet stage, the associated piston extends within the associated cylinder to draw a hydraulic fluid from the pintle inlet into a chamber defined within the associated cylinder when the associated rotor fluid port is in fluid communication with the pintle inlet;
• in the compression stage, the associated piston retracts within the associated cylinder to compress the hydraulic fluid within the chamber as the associated rotor fluid port slides on an outer surface of the pintle shaft from the pintle inlet to the pintle outlet;
• in the fluid outlet stage, the associated piston continues to retract within the associated cylinder to discharge the hydraulic fluid from the chamber to the pintle outlet when the associated rotor fluid port is in fluid communication with the pintle outlet;
• and, in the decompression stage, the associated piston extends within the associated cylinder to decompress the hydraulic fluid as the associated rotor fluid port slides on the outer surface of the pintle shaft from the pintle outlet to the pintle inlet;
• wherein the ring displacement driver operates to maintain the thrust ring in offset relation from the pintle shaft such that each of an amount of precompression stoke performed by each of the plurality of pistons retracting in the precompression stage and an amount of decompression stroke performed by the each of the plurality of pistons extending in the decompression stage is maintained to be consistent regardless of a position of the thrust ring offset from the pintle shaft, thereby providing a smooth pressure transition in the each of the plurality of radially oriented cylinders.