GB2211908A - Linear actuator - Google Patents

Linear actuator Download PDF

Info

Publication number
GB2211908A
GB2211908A GB8725567A GB8725567A GB2211908A GB 2211908 A GB2211908 A GB 2211908A GB 8725567 A GB8725567 A GB 8725567A GB 8725567 A GB8725567 A GB 8725567A GB 2211908 A GB2211908 A GB 2211908A
Authority
GB
United Kingdom
Prior art keywords
shaft
housing
linear actuator
threaded member
actuator according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB8725567A
Other versions
GB8725567D0 (en
Inventor
Bryan Nigel Victor Parsons
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jaguar Land Rover Ltd
Original Assignee
Jaguar Cars Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Jaguar Cars Ltd filed Critical Jaguar Cars Ltd
Priority to GB8725567A priority Critical patent/GB2211908A/en
Publication of GB8725567D0 publication Critical patent/GB8725567D0/en
Publication of GB2211908A publication Critical patent/GB2211908A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H25/22Screw mechanisms with balls, rollers, or similar members between the co-operating parts; Elements essential to the use of such members
    • F16H25/2285Screw mechanisms with balls, rollers, or similar members between the co-operating parts; Elements essential to the use of such members with rings engaging the screw shaft with the inner perimeter, e.g. using inner rings of a ball bearing
    • F16H25/229Eccentric rings with their axis arranged substantially parallel to the screw shaft axis

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

A linear actuator has a screw threaded shaft 11 mounted so that it is restrained from rotational movement, a housing 13 is mounted for rotation on the shaft 11, a threaded member 20 is rotationally mounted eccentrically of the housing 13, the diameter of the threadform of the threaded member 20 being different from that of the shaft 11 and being arranged to engage the threadform of the shaft 11 on one side thereof, and drive means being provided to rotate the housing 13 so that relative movement between the threads of the shaft 11 and internally threaded member 20 will produce relative axial movement between the shaft 11 and housing 13. <IMAGE>

Description

LINEAR ACTUATOR The present invention relates to linear actuators and in particular to linear actuators of the screw thread type.
Hitherto linear actuators have been provided in which an externally threaded shaft engages an internally threaded member, the velocity ratio, that is the ratio of the number of turns of the driven component to the number of pitch lengths of linear travel of the other component of such systems being 1. It is possible by increasing the diameter of the internally threaded member, so that the threads thereon engage the threads on the shaft member at only one point, to provide a linear actuator with an increased velocity ratio.
Drive is conventionally applied to such actuators by rotation of the shaft. The shaft must consequently be supported in bearings which will run under full load at the drive speed and there will consequently be relatively high frictional losses at these bearings.
According to one aspect of the present invention a linear actuator comprises a screw threaded shaft mounted so that it is restrained from rotational movement, a housing mounted for rotation on said shaft, a threaded member rotationally mounted eccentrically of the housing, the diameter of the threadform of the threaded member being different than that of the shaft and being arranged to engage the threadform of the shaft, and drive means being provided to rotate the housing.
With this arrangement, as the housing is driven so that it rotates relative to the shaft, the threaded member will describe an orbital motion relative to the shaft. As the diameter of the threaded member is different than that of the shaft, the orbital motion will cause the threaded member to rotate relative to the shaft, thus causing relative axial movement. The speed of relative rotation will depend upon the eccentricity of the threaded member, but will generally be much slower than the drive speed.
Consequently while there will still be frictional losses between the threaded member and means for transmitting axial loads to or from the threaded member, these will be at relatively slow speed and will consequently be very much reduced as compared to the losses at the bearings of the shaft in the hitherto known devices.
An embodiment is now described, by way of example only, with reference to the accompanying drawings, in which: Figure 1 is a sectional elevation of a linear actuator in accordance with the present invention; and Figure 2 is an enlarged view of the threadform of the shaft and internally threaded member, shown in Figure 1.
As illustrated in Figure 1 the linear actuator comprises shaft 11 which is non-rotatably mounted in suitable manner. The shaft 11 is provided with an acme type thread 12, which as illustrat-ed in Figure 2 has a profile angle of 290 and flat crests.
A housing 13 is mounted on the shaft 11 by means of a roller bearing 14, the internal race 15 of the roller bearing 14 slidably engaging the flat crests of thread 12.
The bearing 14 is maintained in housing 13 between a shoulder portion 16 and a circlip 17.
An internally threaded member 20 having an acme type thread 21 similar to that of shaft 11 but of larger diameter, is mounted in an eccentric bore 22 in the housing 13 by means of roller bearing 23, so that at one point, the thread 21 thereof engages the thread 12 of the shaft 11.
A load supporting member 25 is slidingly located on the shaft 11 by means of a cylindrical bearing 26 which engages the flat crests of the thread 12. A series of radially inwardly directed angularly spaced pins 27 are provided on the support plate 25 and engage in a circumferential groove 28 in the internally threaded member 20. These pins 27 transfer the thrust between the support member 25 and internally threaded member 20 while permitting relative rotational and eccentric movements therebetween.
A balance weight 30 is provided about the housing 13 to compensate for centrifugal imbalance due to the eccentricity of the internally threaded member 20, bearing 23 and the bore 22 in housing 13. Means (not shown) is also provided to drive the housing 13. Drive of the housing 13 may be achieved, for example, by means of a belt drive from a remote motor or the housing itself may be defined by the rotor of the motor.
When the housing 13 is rotated relative to the shaft 11, if the load applied to the support member 25 is sufficiently low, friction between the threads 12 and 21 will be lower than that of the bearing 23 and the internally threaded member 20 will rotate with the housing 13 giving a drive ratio of 1:1. If however the load applied to support member 25 is such that friction between the threads 12 and 21 is greater than that of the bearing 23, the housing will rotate relative to the internally threaded member 20 and will cause the internally threaded member 20 to describe an orbital motion about the shaft 11. Because of frictional engagement between the threads 12 and 21 and the difference in their diameters, this orbital motion will produce rotation of the internally threaded member 20 with resulting relative axial movement between the internally threaded member 20 and shaft 11.For example, if the diameter ratio of the thread 12 to thread 21 is 3:4, for every orbit of the internally threaded member 20 about the shaft 11, the internally threaded member 20 will rotate by one quarter of a turn and consequently, for four revolutions of the housing 13 the internally threaded member 20 will move one pitch of the screw thread, axially relative to the shaft 11, that is a drive ratio of 1:4.
The device described above will consequently give a linear actuator the drive ratio of which will vary with the load applied.
Various modifications may be made without departing from the invention. For example, rather than having shaft 11 fixed axially and support member 25 and housing 13 etc.
movable axially thereon, the housing 13 and support member 25 may be fixed axially and the shaft 11 movable axially.
Also, while frictional losses occurring between the internally threaded member 20 and support member 25 are very much reduced due to the relatively slow speed of rotation of the internally threaded member 20 when a load is applied, these losses may be reduced even more, by the use of low friction elements. For example, the pins 27 may be replaced by rollers or alternatively roller bearings which are arranged to slide laterally in order to permit eccentric movement of the internally threaded member 20.
For a given nominal diameter of threads 12 and 21, the diameter ratio and hence the drive ratio may be varied, within the limitations of the thread form, by varying the radial overlap of the threads. This may be achieved by providing means for varying the eccentricity of bearing 23 with respect to the housing 13, for example by the interposition of an annular member, the internal diameter of which is eccentric to the external diameter, between the outer face of the bearing 23 and the housing whereby eccentricity of the internally threaded member 20 may be adjusted by rotation of the annular member. Furthermore, while in the embodiment described above, the drive ratio will change from 1:1 to a reduced ratio as a result of the load applied to the support member 25, means may alternatively be provided for locking the bearing 23 so that change in the ratio may be effected as desired.
While in the above embodiment the shaft 11 has an external thread and member 20 an internal thread of larger diameter, the shaft 11 may be tubular with an internal thread and member 20 be mounted within the shaft and have an external thread of smaller diameter.

Claims (13)

1. A linear actuator comprising a screw threaded shaft mounted so that it is restrained from rotational movement, a housing mounted for rotation on said shaft, a threaded member rotationally mounted eccentrically of the housing, the diameter of the threadform of the threaded member being different than that of the shaft and being arranged to engage the threadform of the shaft, and drive means being provided to rotate the housing.
2. A linear actuator according to claim 1 in which the threadforms of the shaft and threaded member have flat crests.
3. A linear actuator according to claim 1 or 2 in which the housing is mounted on the shaft by means of a low friction element which will permit rotation and axial movement of the housing with respect to the shaft.
4. A linear actuator according to any one of claims 1 to 3 in which the threaded member is located in and eccentric bore in the housing by means of a low friction element.
5. A linear actuator according to any one of the preceding claims in which a load supporting member is slidingly mounted on the shaft and is coupled to the threaded member by means which will transmit axial loads while permitting relative rotation and eccentric movement of the threaded member with respect to the support member.
6. A linear actuator according to claim 5 in which a series of angularly spaced radially inwardly extending members are provided on the load supporting member, these members engaging in a circumferential groove in the threaded member.
7. A linear actuator according to any one of the preceding claims in which the housing and support member are movable axially along the shaft.
8. A linear actuator according to any one of claims 1 to 6 in which the housing and support member are fixed axially and the shaft is movable axially with respect thereto.
9. A linear actuator according to any one of the preceding claims in which the drive means comprises a belt or like means by which the housing is driven from a remote motor.
10. A linear actuator according to any one of claims 1 to 8 in which the housing is defined by the rotor of a motor.
11. A linear actuator according to any one of the preceding claims in which the threaded member is mounted with respect to the housing in a manner which will permit adjustment of its eccentricity within the extremes of overlap of the threads of the shaft and threaded member.
12. A linear actuator according to any one of the preceding claims in which means is provided for selectively locking the threaded member rotationally relative to the housing.
13. A linear actuator substantially as described herein with reference to, and as shown in, figures 1 and 2 of the accompanying drawings.
GB8725567A 1987-10-31 1987-10-31 Linear actuator Withdrawn GB2211908A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8725567A GB2211908A (en) 1987-10-31 1987-10-31 Linear actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8725567A GB2211908A (en) 1987-10-31 1987-10-31 Linear actuator

Publications (2)

Publication Number Publication Date
GB8725567D0 GB8725567D0 (en) 1987-12-02
GB2211908A true GB2211908A (en) 1989-07-12

Family

ID=10626242

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8725567A Withdrawn GB2211908A (en) 1987-10-31 1987-10-31 Linear actuator

Country Status (1)

Country Link
GB (1) GB2211908A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19515093A1 (en) * 1995-04-25 1996-10-31 Schaeffler Waelzlager Kg Spiral gearing with threaded spindle with ring nut housing for roller bearings
EP1801457A1 (en) * 2004-09-16 2007-06-27 Scientific Technologies Ltd. Method and device for power transmission with load-sensing thrust amplifying mechanism
WO2007110769A1 (en) * 2006-03-24 2007-10-04 Ares Engineering S.R.L. Device for converting a rotary motion into a linear motion
EP1884684A2 (en) * 2006-08-03 2008-02-06 LuK Lamellen und Kupplungsbau Beteiligungs KG Transmission system for transforming a rotary movement into a linear movement

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0024043A2 (en) * 1979-08-09 1981-02-18 Mikko Antero Laakko Apparatus for converting rotary motion to linear motion

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0024043A2 (en) * 1979-08-09 1981-02-18 Mikko Antero Laakko Apparatus for converting rotary motion to linear motion

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19515093A1 (en) * 1995-04-25 1996-10-31 Schaeffler Waelzlager Kg Spiral gearing with threaded spindle with ring nut housing for roller bearings
EP1801457A1 (en) * 2004-09-16 2007-06-27 Scientific Technologies Ltd. Method and device for power transmission with load-sensing thrust amplifying mechanism
EP1801457A4 (en) * 2004-09-16 2008-01-16 Scient Technologies Ltd Method and device for power transmission with load-sensing thrust amplifying mechanism
US7584678B2 (en) 2004-09-16 2009-09-08 Scientific Technologies Ltd. Power transmission method and device having load sensing thrust augmentation mechanism
WO2007110769A1 (en) * 2006-03-24 2007-10-04 Ares Engineering S.R.L. Device for converting a rotary motion into a linear motion
EP1884684A2 (en) * 2006-08-03 2008-02-06 LuK Lamellen und Kupplungsbau Beteiligungs KG Transmission system for transforming a rotary movement into a linear movement
EP1884684B1 (en) * 2006-08-03 2013-06-12 Schaeffler Technologies AG & Co. KG Transmission system for transforming a rotary movement into a linear movement

Also Published As

Publication number Publication date
GB8725567D0 (en) 1987-12-02

Similar Documents

Publication Publication Date Title
US4576057A (en) Anti-friction nut/screw drive
NL1009197C2 (en) Screw actuator, and caliper with such a screw actuator.
US4744261A (en) Ball coupled compound traction drive
US4487091A (en) Speed reducer and method for reducing blacklash
US4794810A (en) Linear actuator
US3295385A (en) Automatic anti-friction dual ratio motion converter
CN1040789C (en) Strok mechanism, especially used in piston pump
US2886986A (en) Infinitely variable friction drive
US5189927A (en) Variable ratio drive transmission
EP1339602B1 (en) Roller screw actuator
US3081639A (en) Feed mechanism
GB2211908A (en) Linear actuator
EP0006082A2 (en) Apparatus for translating rotary movement to rectilinear movement
EP0107485A1 (en) Motion transmitting devices
US4478100A (en) Automatic transmission
US3469463A (en) Frictional drive speed changer
US5795259A (en) Continuously variable transmission
EP0024043A2 (en) Apparatus for converting rotary motion to linear motion
JP3278469B2 (en) Gear type continuously variable transmission
SU1796810A1 (en) Planet screw-nut gear
RU2735979C1 (en) Linear electric drive
US11421765B2 (en) Actuating mechanism with a planetary roller screw mechanism
RU2766637C1 (en) Drive structure
SU926406A1 (en) Screw pair with rolling friction
SU570745A1 (en) Screw nut co-operating system

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)