Abstract:
An improved high torque rotary abutment motor is provided that is capable of producing ultra high pressures, while still remaining light weight an reliably efficient. The rotary abutment motor is provided with a body and rotor are sealed in the axial direction with two face spring seals compensating for tolerance and wearing gap. In such a configuration, increasing pressures create increasing force of sealing, thereby allowing operational pressures in excess of what is currently available today.

Description:
BACKGROUND OF THE INVENTION 
       [0001]    1. Field of the Invention 
         [0002]    The present invention relates generally to hydraulic motors and, more particularly, to a low speed, high torque hydraulic motor. 
         [0003]    2. Description of the Related Art 
         [0004]    Hydraulic motors are actuators (like hydraulic cylinders) that simply convert hydraulic pressure into rotary movement. Even though the construction is similar, motors differ from pumps in that they are ““pushed”” into rotation by the already active fluid. A hydraulic motor converts hydraulic energy into rotating motion by being pushed by hydraulic fluid. A hydraulic motor is rated by displacement, torque, speed and pressure limits. Further, they are classified as HSLT (High speed/Low torque), LSHT (Low speed/High torque) or Limited Rotation (Torque Actuators). Typical hydraulic motors (actually called a rotary hydraulic actuator) use some form of surface area to receive hydraulic fluid, which cause a shaft to spin, which is connected to various equipment driven by that hydraulic motor. The surface that is ““pushed”” may be rectangular in nature, as in gear, vane and rotary abutment motors, or circular in nature as in rotary and axial piston motors. 
         [0005]    Commercially, there are available only several practical designs for low speed, high torque applications. Eaton Corporation Hydraulic Division developed a derivative called the Geroler™, which consists of an inner and outer rotor. The inner rotor has N teeth, and the outer rotor has N+1 teeth. One rotor is located off-center and both rotors rotate. During part of the assembly&#39;s rotation cycle, the area between the inner and outer rotor increases, creating a vacuum. This vacuum creates suction, and hence, this part of the cycle is where the intake is located. Then, the area between the rotors decreases, causing compression. During this compression period, fluids can be pumped, or compressed (if they are gaseous fluids). The Eaton Geroler™ design essentially uses bearing rollers instead of lobes on the ring to increase the mechanical efficiency. Greater efficiency comes at the price of greater manufacturing complexity and extreme fit tolerances involving single digit micrometers. Gerotor pumps are generally designed using a trochoidal inner rotor and an outer rotor formed by a circle with intersecting circular arcs. Although this design works well and is simple to define it does create gaps between the inner and outer rotor when the tooth of the inner rotor rotates into the pocket of the outer rotor. This gap seals during rotation causing inefficiency, noise and wear due to the pump attempting to compress the trapped and incompressible fluid in the gap. A Gerotor can also function as a motor. High pressure gas enters the intake area and pushes against the inner and outer rotors, causing both to rotate as the area between the inner and outer rotor increases. During the compression period, the exhaust is pumped out. 
         [0006]    However, due to sealing limitations such commercially available hydraulic motors generally maintain a continuous pressure of around 3000 psi, while tolerating only intermittent pressure spikes in excess of that. Nowherein is there available a high torque hydraulic motor that is capable of producing ultra high pressures at speeds ranging from low to high, while still remaining light weight an reliably efficient. 
         [0007]    Consequently, a need has therefore been felt for an improved but less complex high pressure, high torque hydraulic motor. 
       SUMMARY OF THE INVENTION 
       [0008]    It is therefore an object of the present invention to provide an improved rotary abutment motor. 
         [0009]    It is a feature of the present invention to provide increased power density, and thereby greater efficiency, by providing an improved rotary abutment motor designed to hold pressure exceeding 10,000 PSI [700 BAR] while maintaining a low coefficient of friction −0.06-0.07, that will provide a long dependable service life, excellent leakage control. 
         [0010]    Briefly described according to the present invention, a rotary abutment motor is provided with simplicity of design (just 15 parts), in which the body and rotor are sealed in the axial direction with two face spring seals compensating for tolerance and wearing gap. 
         [0011]    An advantage of the present invention is that increasing pressures create increasing force of sealing, thereby allowing operational pressures in excess of what is currently available today. 
         [0012]    Further advantages of the present invention resulting from being able to use ultra high pressures include its compact size, higher reliability due to fewer parts, bidirectional operation and scalable size and performance. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0013]    The advantages and features of the present invention will become better understood with reference to the following more detailed description and claims taken in conjunction with the accompanying drawings, in which like elements are identified with like symbols, and in which: 
           [0014]      FIG. 1  is axial section of a rotary abutment motor according to the preferred embodiment of the present invention; 
           [0015]      FIG. 1A  is a partial detail cross sectional view of the face shaft seal that forms axial seal between shaft and body; 
           [0016]      FIG. 2  is a section B-B thru the joint of the body; 
           [0017]      FIG. 2A  is a partial detail of rotor seal passing cutout in body an equalizing pressure before vane of the shaft and behind; 
           [0018]      FIG. 2B  is a partial detail of star seal passing cutout in the rotor an equalizing pressure before vane of the wing and behind; 
           [0019]      FIG. 3  is a top view showing a schematic representation of timing cams for operation of the rotary abutments and stars in the start of turning; and 
           [0020]      FIG. 4  is a top view showing a schematic representation of timing cams for operation of the rotary abutments and stars in the second (locked) position. 
       
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS 
       [0021]    The best mode for carrying out the invention is presented in terms of its preferred embodiment, herein depicted within the Figures. 
       1. Detailed Description of the Figures 
       [0022]    Referring now to  FIG. 1-4  a rotary abutment type hydraulic motor, generally noted as motor, shows the preferred embodiment of the invention having a housing formed of a housing top  1  and a hosing bottom  2  that serves to contain the fluid and moving parts of the motor. A drive shaft  3  with 2 symmetrical vanes  3 A and  3 B rotably mounted centrally within the housing supports. The drive shaft  3  provides an input/output mechanical interconnection for the power presenting the rotor structure  3 A and  3 B and a cylindrical member which rotates in respect to the housing of the motor. It is anticipated that each rotor vane has rectangular slot for rotor seal and having sealed rotor bolts  6  bolted there through such that each vane member is firmly mated together about rotor seal  15 . This rotor seal  15  forms a seal between the rotor vane  3  ands the interior surface of the housing that forms the fluid passage  1 B and is anticipated as having two separate elements: an inner rubber “O”ring and outer trapezoidal plastic part. It has been found that the use of Zatkoff brand Turcon Glide Ring T seal can be utilized for pressure up to 11600 psi [800 Bar]. In the middle of each seal there are reinforcement metal  14 A for star seal and  15 A for shaft seal longer than cutout in body and shaft to pass cutouts without squeezing-out. Additionally, as shown in grater detail in conjunction with  FIG. 1A , the body and rotor are sealed in the axial direction with a shaft seal  12  that forms a face seal between the outer surface of the shaft  3  such as to provide increased pressure sealing within the fluid passage  1 A,  1 B and between wings. This is accomplished by having an upper ring  12 A pressed into the body, and having a laterally movable lower ring  12 B connected thereto by spring element  12 C brazed to both rings. The high pressure inside the internal cavity  1 B forces against the convexity of the seal. This urging force between the shaft  3  and the pressurized cavity P 1  forces the sides of the seal outward, thereby increasing the sealing pressure and making the seal more effective at higher pressure. 
         [0023]    In this manner, additional later force against the convexity  12 C results from increasing pressure within the fluid passage  1 A. In effect, the pressure within the fluid passage P 1  aids in generating a sealing force. This is opposite of most seal applications in which the sealing member must be strong enough to oppose direct pressure. 
         [0024]    Additionally, the rotor vanes  3 A,  3 B and stars vanes  5 A 1 ,  5 B 1  (in next turn will be next vanes) form the main operative valve for the motor. For this to occur, there a fluid passage  1 A located surrounding the outer circumference of the drive shaft  3 . This fluid passage  1 B is in fluid communication with a first port  16 A and second port  16 B for constant communication in respect thereto. Undercuts placed on both joint surfaces of the upper and lower bodies, and in the middle of the rotor vanes allow for symmetry of the rotor and body. The first fluid passage  1 B is interconnected by a first undercut  1 D and second  1 E placed on the joint surface of the body. The operation of each of four undercuts  3 C will be described in greater detail below. 
         [0025]    A first rotary abutment I and second II are provided as operating symmetrically. For purposes of brevity, only the detailed description of the first rotary abutment I will be provided, it being understood that the second rotary abutment II is formed and operates similarly. The rotary abutment I is formed of a vane  3 B and vane  5 B 1  of the star  5 B. Each rotary abutment I and II rotates in an overlapping concentric fashion over the path of each rotor vane  3 A,  3 B respectively, such incremental progression of each star  5 A,  5 B in series can be implemented in timed fashion’ synchronized to the position of the rotor  3  in order to alternately cause various chambers formed within the internal cavity P 1 , P 2 , P 3 , P 4 .to be pressurized or depressurized. As the rotor vane  3 B passes through the rotation path of the abutment, the star rotates and seal chamber P 1  but vane  3 B passed notch N 1  and seal chamber P 1  release pressure in front of vane  3 B. In this manner, it is anticipated that each rotary abutment I, II can be bidirectional, and completely reversible under load. The absence of the springs and symmetry of the rotor and body can allow smooth, reverse operation. If torque applied to the rotor, and behind the vane  3 B is suction in chamber P 1  and before in passage P 2  is pressure—motor becomes a pump. 
         [0026]    Referring now to  FIGS. 3 and 4 , timing of the sequentially stepped and synchronized rotation of the stars  5 A and  5 B are accomplished though the use of inter-impinging cams. A rotor cam  7  is affixed to and rotates with the main rotor  3  and allows for both synchronization of the movements of each star  5 A,  5 B relative to the rotor  3 , but also provides an urging force as well. A star cam  9   b  affixed to star  5   b  and rotating with the rotary abutment II impinges against the rotor cam  7  preventing rotation until concave timing inset approaches the star cam. A star  9 A start rotates because of pressure vane  9 A, at the same time concave  7 A is passing through cam  9 A and allow to rotate. When the star vane contact surface to vane of the rotor  3 A is become tangent the star cam  9 A is forced by corner of the concave  7 A ( FIG. 4 ) into the next sequential position and again locked in place through impingement. Similarly, the second star cam  9 B functions in the same manner for synchronizing and rotating the second abutment II, and a second timing concave  7 B opposite the first timing concave  7 A functions to allow this sequential procedure continues for each rotary abutment I, II. 
       2. Operation of the Preferred Embodiment 
       [0027]    In operation, the two ports  16 A,  16 B interconnected the motor to a source of high pressure and fluid return, with the direction of rotation of the motor dependent upon which port is pressurized. (motor can also be utilized as a pump by connecting the shaft  3  to a source of power in known manner). By way of example, and not as a limitation, and in connection with FIGURES, as pressurized fluid enters the second port  16 B it pressurized the cavity P 3  between the rotor vane  3 A and vanes of star  5 B of rotary abutment I and rotation is in a clockwise direction and discharge fluid in port  16 A. 
         [0028]    The foregoing descriptions of specific embodiments of the present invention have been presented for purposes of illustration and description. They are not intended to be exhaustive or to limit the invention to the precise forms disclosed, and obviously many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical application, to thereby enable others skilled in the art to best utilize the invention and various embodiments with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the Claims appended hereto and their equivalents. Therefore, the scope of the invention is to be limited only by the following claims.