Differential drive linear actuator

• US 5,865,272 A
• Filed: 11/22/1996
• Issued: 02/02/1999
• Est. Priority Date: 08/03/1994
• Status: Expired due to Fees

• Current Assignee: Rotork Controls Limited (Rotork PLC)
• Original Assignee: Rotork Controls Limited (Rotork PLC)
• Inventors: Sanders, Peter G., Wiggins, Christopher R.
• Primary Examiner(s): Marmor, Charles A.
• Assistant Examiner(s): GRABOW, TROY E
• Application Number:
  US08/750,226
• Time in Patent Office: 802 Days
• Field of Search: 74/424.8 VA, 74/89.15, 185/40 R, 251/69, 251/71, 251/129.11, 251/129.12
• US Class Current: 185/40.00R
• CPC Class Codes: F16H 2025/2065 Manual back-up means for overriding motor control, e.g. hand operation in case of failure
• CPC Class Codes: F16H 2025/2068 Means for returning linear actuator to zero position, e.g. upon occurrence of failure by using a spring
• CPC Class Codes: F16H 2025/2075 Coaxial drive motors
• CPC Class Codes: F16H 2025/2081 Parallel arrangement of drive motor to screw axis
• CPC Class Codes: F16H 25/2018 with both screw and nut being driven, i.e. screw and nut are both rotating
• CPC Class Codes: F16H 25/2204 with balls
• CPC Class Codes: F16K 31/047 characterised by mechanical means between the motor and the valve, e.g. lost motion means reducing backlash, clutches, brakes or return means F16K31/043 takes precedence
• CPC Class Codes: G01N 2800/52 Predicting or monitoring the response to treatment, e.g. for selection of therapy based on assay results in personalised medicine; Prognosis
• CPC Class Codes: Y10T 74/18608 Single input split into two intermediate outputs that are subsequently superposed into a single output
• CPC Class Codes: Y10T 74/1864 Shaft and nut driven

Abstract

A linear actuator having an output shaft having a pair of driven wheels mounted thereon. One of the driven wheels is rotatably mounted in a fixed plane and has a drive nut for an associated thread on the output shaft. The other drive wheel is rotatably fixed to the output shaft. An input shaft is in side-by-side relationship with the output shaft and adapted to be rotated by a suitable power source. The input shaft provides a drive wheel for each of the driven wheels, with the ratio between each drive and driven wheel set being chosen to rotate the driven wheels at different speeds in the same rotational direction and thereby produce a controlled axial movement of the output shaft in a direction depending upon the relative rotation of the driven wheels. The other driven wheel and the drive wheel of its set are in the form of meshing helical gear wheels. A fail-safe arrangement is provided and has a clutch between the drive wheels of the input shaft, a back-drive for the output shaft, and biasing means for effecting a back-drive. The arrangement is such that the meshing helical gears impart an axial force to engage the clutch only while power is supplied, and the biasing means are operative to back-drive the output shaft to a fail-safe position when the power is terminated.

Claims

1. A linear actuator comprising an output shaft having a pair of driven wheels mounted thereon, one of said pair of driven wheels being rotatably mounted in a fixed plane and having a drive nut for an associated thread on said output shaft, the other of said pair of driven wheels being rotatably fixed to said output shaft, and an input shaft in side-by-side relationship with said output shaft, said input shaft being adapted to be rotated by a suitable power source, said input shaft providing a drive wheel for each of said driven wheels, the ratio between each drive and driven wheel set being chosen to rotate the driven wheels at different speeds in the same rotational direction to produce a controlled axial movement of said output shaft in a direction depending upon the relative rotation of said driven wheels, wherein said other driven wheel and the drive wheel of its set are in the form of meshing helical gear wheels, and wherein a fail-safe arrangement is provided comprising a clutch between the drive wheels of the input shaft, a back-drive for said output shaft, and biasing means for effecting a back-drive, the arrangement being such that the meshing helical gears impart an axial force to engage the clutch only while power is supplied and the biasing means are operative to back-drive the output shaft to a fail-safe position when the power is terminated.

2. An actuator according to claim 1, wherein an electromagnet or other suitable force applying means is provided and adapted to maintain the clutch in engagement when power is terminated.

3. An actuator according to claim 1, wherein said other driven wheel is axially fixed on said output shaft, whereby the speed difference between the driven wheels will cause this wheel and hence the output shaft to move axially towards or away from said one driven wheel depending upon the relative rotation of said driven wheels.

4. An actuator according to claim 1, wherein said other driven wheel is also in a fixed plane, and wherein said output shaft is axially movable relative to this driven wheel via an axially extending key/keyway arrangement, whereby the speed difference between the driven wheels will cause movement of the output shaft in an axial direction depending upon the relative rotation of the two driven wheels.

5. An actuator according to claim 1, wherein the input and output shafts are parallel and the speed difference is achieved by using different tooth sizes/numbers for each drive/driven wheel set.

6. An actuator according to claim 1, wherein the back drive comprises a recirculating ball nut, or other low friction contact device, between the drive nut and associate thread to facilitate the action of the biasing means.

7. An actuator according to claim 1, for use in deep underwater applications, wherein the biasing means comprise a piston/cylinder arrangement in which the cylinder is maintained at a controlled pressure substantially lower than the surrounding water pressure to produce a continuous biasing force.

8. An actuator according to claim 1, wherein said power source comprises a motor with a hollow drive spindle in axial alignment with the output shaft for accommodating axial movement of said output shaft.

9. An actuator according to claim 1, for undersea application where a remote operating vehicle (R.O.V.) is provided in case of breakdown, wherein an auxiliary drive shaft is provided which is connected at one end to the drive end of the actuator output shaft, the other end being adapted to be coupled to the drive of the R.O.V., an auxiliary output shaft is provided at the output end of said actuator output shaft, and a thrust bearing is provided which in normal operation is arranged to maintain the actuator output shaft and the auxiliary drive shaft in the event of a breakdown providing a force which overcomes the biasing means to disengage the thrust bearing and permit independent R.O.V. operation of said auxiliary output shaft.

10. An actuator according to claim 9, wherein said thrust bearing is positioned between the output end of said actuator output shaft and said auxiliary output shaft, and the thrust bearing is in separable halves which are normally held in driving engagement by said biasing means, and the force provided by connection of said R.O.V. causing said halves to separate.