Seal
10962116 ยท 2021-03-30
Assignee
Inventors
- George Edmond (Yatton, GB)
- Simon Ennor (Clevedon, GB)
- Jonathan Robins (Clevedon, GB)
- Paul Bowles (North Somerset, GB)
- Pawel Kwasniewski (Olawa, PL)
Cpc classification
F16K37/0066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K41/046
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/3232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16J15/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K41/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/3232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16J15/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A rotary seal comprises a seal element comprising a disc-shaped body having a first axial side and an opposed second axial side. The seal element further comprises a radially inner central circular opening for receiving a rotary shaft, the opening having an inner periphery for sealing engagement with the shaft. A radially outer rim portion of the seal element comprises an axially facing annular sealing surface provided on the first axial side for sealing engagement in use with an opposed axially facing sealing surface of an adjacent first static housing and an axially facing pocket provided on the second axial side and having an axially facing surface for receiving, in use, an annular elastomeric biasing element. At least one drainage passage is formed through the outer rim portion from an inlet on the second axial side to an outlet on a radially outer portion of the rim portion.
Claims
1. A rotary sealing arrangement comprising: a first static housing comprising a first axially facing sealing surface; a second static housing comprising a second axially facing surface; a rotary shaft extending axially through the first and second static housings; a rotary seal arranged between the first and second static housings, the rotary seal comprising a seal element comprising a disc-shaped body having a first axial side and an opposed second axial side, the seal element further comprising: a radially inner central circular opening for receiving the rotary shaft, the opening having an inner periphery directly engaging the shaft; a radially outer rim portion, the radially outer rim portion having: an axially facing annular sealing surface provided on the first axial side for sealing engagement with the axially facing sealing surface of the first static housing; an axially facing pocket provided on the second axial side and having an axially facing surface; and at least one drainage passage formed through the outer rim portion from an inlet on the second axial side to an outlet on a radially outer portion of the rim portion to provide a fluid drainage path P through the rim portion by passing the axially facing pocket, the rotary sealing arrangement further comprising an annular elastomeric biasing element received in the pocket; and wherein: the inner periphery of the seal element forms a dynamic seal with the shaft; and the annular elastomeric biasing element is axially compressed between the axially facing surface of the pocket and the axially facing surface of the second housing thereby biasing the axially facing annular sealing surface of the rim portion of the seal element into sealing engagement with the first axially facing sealing surface of the first static housing.
2. A rotary sealing arrangement as claimed in claim 1, the rotary seal comprising a plurality of drainage passages arranged circumferentially therearound.
3. A rotary sealing arrangement as claimed in claim 2, the rotary seal comprising at least four drainage passages arranged circumferentially therearound.
4. A rotary sealing arrangement as claimed in claim 2, wherein the drainage passages are circumferentially equi-spaced around the seal element.
5. A rotary sealing arrangement as claimed in claim 1, wherein said axially facing pocket comprises a radially inner, axially extending lip.
6. A rotary sealing arrangement as claimed in claim 5, wherein the drainage passage inlet is formed at the base of the axially extending lip.
7. A rotary sealing arrangement as claimed in claim 1, wherein the axially facing annular sealing surface comprises an annular groove formed therearound.
8. A rotary sealing arrangement as claimed in claim 1, wherein the at least one drainage passage extends at an angle () to a radial direction (R).
9. A rotary sealing arrangement as claimed in claim 1, wherein said seal body is made from Polytetrafluoroethylene (PTFE) or a PTFE based material.
10. A rotary sealing arrangement as claimed in claim 1, comprising a first additional seal between the first static housing and the shaft and a second additional seal between the second static housing and the shaft, the seal element being arranged between the first and second additional seals.
11. A rotary sealing arrangement as claimed in claim 1, comprising a clamping element for clamping the first static housing to the second static housing, thereby compressing said annular elastomeric biasing element.
12. A rotary actuator system comprising: a rotary actuator, a rotary valve element; and a rotary sealing arrangement as claim 1, wherein the rotary valve element is coupled to the rotary shaft and further comprising an annular elastomeric biasing element received in the pocket; wherein: the rotary shaft is driven by the rotary actuator; and the rotary actuator comprises the first static housing, the rotary valve comprises the second static housing and the seal element engages the rotary shaft.
13. A rotary actuator system as claimed in claim 12, wherein said rotary valve element is a butterfly valve.
14. An aircraft air conditioning system comprising a rotary actuator system as claimed in claim 12 for controlling flow of air therein.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1) An embodiment of the disclosure will now be described by way of example only with reference to the accompanying drawings in which:
(2)
(3)
(4)
DETAILED DESCRIPTION
(5) With reference to
(6) The rotary shaft 8 in this embodiment is connected at its other end to a valve element 12 of a valve 13. In this embodiment, the valve element 12 is a butterfly valve element which is received in a duct 14 to control the flow of fluid through the duct 14. The duct 14 may, for example, be part of an aircraft air conditioning system, the butterfly valve element 12 controlling the flow of air through the duct 14. The valve element 12 is supported in a second static, valve housing 16 which may, for example, be integrated with a wall of the duct 14. In certain embodiments, the rotary shaft 8 may form a part of the valve assembly and project therefrom for engagement with the actuator 4 as discussed above.
(7) The actuator system 2 further comprises a sealing arrangement 20 arranged between the actuator housing 6 and the housing 16. The sealing arrangement 20 comprises a seal element 22 and an annular elastomeric biasing element 24.
(8) As shown in more detail in
(9) The seal body 26 further comprises a radially outer rim portion 36. The radially outward rim portion 36 has an axially facing annular sealing surface 38 provided on the first axial side 28 of the seal body for sealing engagement with an axially facing annular surface 40 of the adjacent first static housing 6. The axially facing annular sealing surface 38 of the seal element 22 is arranged generally perpendicularly to the axis of rotation A of the rotary shaft 8 and of the central opening 32 of the seal body 26. The axially facing surface 40 of the first static housing is also arranged perpendicularly to the axis of rotation A. The axially facing annular sealing surface 38 of the seal element 22 further comprises an annular groove 42 which extends in a circumferential direction around the axially facing annular surface 38. The purpose of this groove 42 will be described further below.
(10) The radially outer rim portion 36 also comprises, on the second side 30 of the seal body 26, an axially facing pocket 44 comprising a radially inner, axially extending lip 46 and a radially extending axially facing surface 48. As can be seen in
(11) The seal body 26 further comprises at least one drainage passage 50 formed through the outer rim portion 36 from an inlet 52 on the second axial side of the seal body 26 to an outlet 54 on a radially outer portion 56 of the rim portion 36. As will be described further below with reference to
(12) In this embodiment, a plurality, for example four, drainage passages 50 may be provided. Of course more or fewer drainage passages 50 may be provided. The drainage passages 50 may be circumferentially equi-spaced about the seal body 26, although other arrangements of drainage passages 50 may be used. Providing a plurality of drainage passages 50 will help ensure that there is no pooling of liquid around the seal inner circumference in any potential actuator or valve orientation.
(13) In this embodiment, the drainage passages 50 extend in a direction R having a component from the second axial side 30 of the seal body 26 towards the first axial side of the seal body 26. Thus, as shown in
(14) In this embodiment, the inlets 52 of the drainage passages 50 are formed at the base of the lip 46 defining the pocket 44. The outlets 54 of the drainage passages 50 are formed in a sloping radially outer surface 58 of the rim portion 36. Other configurations of drainage passages are of course possible, as long as they provide the necessary bypass passage P. For example, the radially outer surface 58 may not be sloped in other embodiments and the drainage passages 50 may extend parallel to the radial direction R.
(15) The seal body 26 may be a one-piece body. The seal body 26 may, for example, be constructed from a relatively low friction material such as PTFE. This will provide a relatively low friction sealing interface between the inner surface 34 of the central opening 32 and the shaft 8. In other embodiments, the seal body 26 may be made in more than one part example of different materials.
(16) As discussed above and as can be seen in
(17) As further illustrated in
(18) Operation of the above system will now be described.
(19) As briefly mentioned above, in certain circumstances, fluid, for example condensed water may attempt to flow from the duct 14 along the shaft 8 between the first and second housings 6, 16 and into the rotary actuator 4. The additional seals 70, 72, may themselves prevent some flow of fluid, but in the event of the water freezing and thawing, the seals 70, 72 may remain at least partially frozen due to the thermal mass around them, even after the water has thawed which may lead to the effectiveness of the seal being compromised which in turn means that water may penetrate the first static housing 6 and possibly adversely interfere with components of the actuator such as electronic components 10. The sealing arrangement 20 of the present disclosure is intended to mitigate such problems and reduce significantly or avoid penetration of water into the first static housing 6.
(20) As will be seen from
(21) Ingress of water from the outer circumferential surface 56 of the seal element 32 into the first static housing 6 is prevented by the sealing engagement between the between the axially facing annular sealing surface 38 provided on the first axial side 28 of the seal body 32 and the opposed surface 40 of the adjacent first static housing 6. To improve the seal between these 2 components, grease may be provided in the grooves 42 in the axially facing annular sealing surface 38 of the seal element 32. This seal will, normally, be a static seal, since the friction between the opposed surfaces 38, 40 will generally be sufficient to prevent rotation of the sealing element 22 due to its interaction with the rotating shaft 8 at the inner central opening 32.
(22) It will be understood that the description above is of an exemplary embodiment of the disclosure and that modifications may be made thereto without departing from the scope of the disclosure. For example, while the seal element has been described in the context of a rotary valve actuator, an air conditioning system, it may be used in other applications in which water or fluid requires removal from the system.
(23) It will also be understood that, in the disclosed embodiment, the radially inner lip 46 of the pocket 44 is circumferentially continuous. However, this is not essential and the lip (46) may be formed with a plurality of circumferentially spaced sections which will still locate the biasing element 24 radially. Yet further embodiments, the pocket 44 may be formed as a groove in the second side 30 of the rim portion 36. The axially facing surface 48 of the pocket 44 may not be planar as illustrated but may be curved, provided it includes an axially facing portion.
(24) Thus, it will be seen that embodiments of the disclosure provide an advantageous arrangement which will reduce or prevent ingress of moisture to sensitive electronic components in a rotary actuator. The disclosed embodiment has no moving parts and is therefore potentially highly reliable. The system may easily be provided with mistake proofing features to avoid installation of the seal element in an incorrect orientation. The disclosure can be applied to new installations or as a retrofit to existing installations. It may easily be installed using standard tools and fasteners and may easily be adapted to various applications by suitable sizing.