Screw seal and lubrication
10895309 ยท 2021-01-19
Assignee
Inventors
Cpc classification
F16H57/0497
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H25/2204
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H25/2418
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16H25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H25/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Disclosed herein is a screw assembly comprising an internal re-circulating path for re-circulating lubricant fluid between a threaded screw shaft and seals provided at the ends of the screw assembly via internal chambers provided within the seals and passages formed within the nut. Also disclosed are seals for use within such assemblies.
Claims
1. A screw assembly comprising: a screw shaft having a helical thread profile; and a nut for mounting around said screw shaft; the screw assembly further comprising a first seal and a second seal, wherein each of said first seal and said second seal independently comprises a seal, the seal comprising: a seal body having an inner surface for mounting onto and sealing against a screw shaft; an internal chamber formed within said seal body, wherein one or more openings are provided on said inner surface to allow lubricant material to transfer between said inner surface and said internal chamber; and one or more external ports provided on a radial surface and/or an outer surface of said seal body for transferring lubricant material into or out of said internal chamber of said seal body; wherein respective external ports (27A, 27B) of said first and second seals (26A, 26B) are aligned with respective passages extending through said screw assembly to provide a re-circulating path for re-circulating lubricant material within said screw assembly.
2. The screw assembly of claim 1, wherein said passages are formed within said nut such that said re-circulating path extends from the first seal (26A) through the passage formed within the nut to the second seal.
3. The screw assembly of claim 1, wherein said first seal (26A) is disposed at a first end of said screw assembly and wherein said second seal (26B) is disposed at a second, opposite end of said screw assembly.
4. The screw assembly of claim 1, wherein a rotation of said screw shaft relative to the first and second seals in a clockwise direction causes lubricant material to flow around said re-circulating path in a first direction and wherein rotation of said screw shaft relative to the first and second seals in an anti-clockwise direction causes lubricant material to flow around said re-circulating path in a second, opposite direction.
5. The screw assembly of claim 1, wherein said screw assembly is a ballscrew assembly comprising a plurality of ball bearings received within the thread profile of said screw shaft and wherein said nut radially confines said ball bearings within the ballscrew assembly.
6. An aircraft comprising: the screw assembly of claim 1.
7. An aircraft control system comprising: the screw assembly of claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Various arrangements and embodiments will now be described, by way of example only, and with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION
(14)
(15) The lubricant material tends to migrate around the helical profile of the shaft 10 in use, i.e. as the shaft rotates within the ballscrew assembly. In order to try to contain the lubricant material, a labyrinth seal 16 may be provided, as shown, having an internal profile that conforms to the helical or threaded outer profile of the shaft 10. However, such seals 16 may not be entirely effective at preventing the natural migration of the lubricant material out of the ballscrew assembly and lubricant material may still escape over time. Thus, the ballscrew assembly must regularly be re-lubricated, during which times the system within which the ballscrew assembly is installed (e.g. an aircraft) may be inoperational.
(16) Thus, according to the present disclosure, a novel sealing design may be provided that offers a path for the lubricating material (e.g. fluid) to be re-directed and re-circulated within the ballscrew assembly via the seals. Thus, the natural migration of the lubricating material may be exploited by providing within the ballscrew assembly a path of lower (e.g. or least) resistance for the lubricant material so that the lubricant material may tend to circulate around the ballscrew assembly (rather than escape) and hence be better contained therein.
(17)
(18) It will be appreciated that the seal body 26 may generally comprise a single internal chamber 30 extending annularly around the seal body 26 (or extending annularly around at least a portion of the seal body 26), with the single internal chamber 30 being in fluid communication with each of the openings 28. However, it will also be appreciated that the seal body 26 may comprise a plurality of individual internal chambers 30, each individual chamber 30 being associated with a respective one or ones of a plurality of openings 28. The skilled person will appreciate that various suitable configurations of openings 28 and internal chambers 30 may be provided. For instance, the number and arrangement or spacing of the openings 28 arranged around the inner surface 24 of the seal 26 may take various suitable configurations other than that depicted in
(19) The openings 28 provided on the inner surface 24 of the seal body 26, however they are arranged, generally allow for fluid communication between the inner surface of the seal 26 and the (or each) interior chamber 30 formed with the seal body 26. Thus, in use, when the seal body 26 is installed onto a ballscrew assembly so that the inner surface 24 seals against the ballscrew shaft 10, lubricant material may be transferred between the shaft 10 and the internal chamber(s) 30 of the seal body via the openings 28.
(20) As also shown in
(21) For instance, each (or at least some) of the openings 28 may be shaped to have a first portion 281 that extends substantially radially (e.g. approximately perpendicular to the inner surface of the seal 26 and the thread path of the shaft 10) so that upon rotation of the shaft 10 in a clockwise direction (referring to the configuration shown in
(22) The openings 28 may further comprise a second portion 282 that is generally shaped to promote spreading of the lubricant material from the internal chamber(s) 30 onto the shaft 10 upon rotation of the shaft 10 in the anticlockwise direction (i.e. the opposite direction to that described above, towards the second portion 282). For example, as shown in
(23) Each of the openings 28 may have substantially the same shape. For example, each of the openings 28 may comprise suitably shaped first portions 281 and second portions 282 to allow lubricant material to alternately pass into or out of said internal chamber 30 depending on the direction of rotation. However, in other examples, the inner surface 24 may be provided with a plurality of openings 28 having different shapes. For example, some of the openings 28 may be shaped to promote or allow lubricant material to enter the internal chamber 30 from the inner surface 24 whereas others of the openings 28 may be shaped to promote or allow lubricant material to spread out from the internal chamber 30 onto the inner surface 24. That is, some of the openings 28 may be suitable shaped to substantially only allow fluid to flow in one direction.
(24) The openings 28 may be disposed entirely within the axial extent of the seal body 26 (i.e. between the radial faces 23, as shown e.g. in
(25) The seal body 26 is also provided with a plurality of external ports 27 which allow lubricant material within the internal chamber 30 to exit the seal 26. The external ports 27 generally act to provide a path for fluid to be transferred out of the internal chamber 30 and away from the inner surface 24 of the seal body. The external ports 27 may thus be provided on a radial face 23 of the seal 26 as shown in
(26) An exit port 27 may be provided for each opening 28, as shown in
(27) Thus, a pathway may be defined for the lubricant material to flow from the inner surface 24 of the seal body 26, and hence from the surface of the ballscrew shaft 10, through the opening 28 into the internal chamber 30 and then out of the seal body 26 through the external ports 27 into the passages 40 formed within the ball nut 14, or vice versa (i.e. from the passages 40 onto the inner surface 24 of the seal body 26). In this way, the lubricant material may be re-circulated around the ballscrew assembly via the internal chamber(s) 30 of the seal body 26. Thus, the lubricant material may be re-directed using the openings 28 of the seal body 26 and re-circulated through the ball nut 14.
(28) For instance,
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(30) That is, as shown, the first portion 281A of the first seal 28A is arranged on the opposite side as the first portion 281B of the second seal 28B. Thus, upon rotation of the shaft 10 in the clockwise direction (referring to
(31) Similarly, rotation of the shaft 10 in the opposite i.e. anticlockwise direction reverses the direction of the lubricant material flow around the ballscrew assembly.
(32) Thus, the routing provided by the openings, internal chambers and passages within the ballscrew assembly may offer a re-circulating path of relatively lower resistance for the lubricating material. So, instead of simply trying to prevent lubricant material escaping from the ends of the ballscrew assembly by fighting the natural migration of the lubricant material (e.g. by simply providing a labyrinth seal, as in
(33) The system may generally be filled with lubricant material so that rotation of the shaft 10 drives the lubricant material around the ballscrew assembly along the path of relatively low resistance offered by the re-circulating pathway. This motion may be driven solely by the fluid pressures and the stresses introduced by the shaping of the openings 28. However, it is also contemplated that by appropriately configuring the relative dimensions of, or by suitably tapering any of, the external ports 27 of the seals 26 and the passages 40 within the ball nut, etc., various pressure differentials may be established within the ballscrew assembly to further facilitate the flow of lubricant material around the ballscrew system. Furthermore, although
(34) Although
(35) Also, although not shown in
(36) The seals described herein may be formed from various suitable sealing materials. Typically, the seals may be formed using hard plastics, such as a hard PTFE plastic.
(37) It is envisioned that a seal of the type generally shown in
(38) Although the techniques presented herein have been described with reference to particular embodiments, it will be understood by those skilled in the art that various changes in form and detail may be made without departing from the scope of the invention as set forth in the accompanying claims.
(39) For instance, although an embodiment has been described above by way of example with particular reference to a ballscrew assembly, it will be appreciated that the seals and techniques presented herein may also suitably be applied to various other screw assemblies where it is generally desirable to better contain the lubricant material within the screw assembly e.g. due to the operating environment or for reasons of size and weight. Particularly, it is contemplated that the seals and techniques presented herein may also suitably be applied to other roller screw or lead screw-type assemblies comprising a threaded screw shaft. For example, the seals presented herein may also be used to provide improved lubrication for ACME-type lead screw actuator assemblies.