SHRINK DISC CONNECTION FOR SURFACE PUMP THRUST CARRYING SHAFTS
20170248151 · 2017-08-31
Assignee
Inventors
- Andrew Michael Nelson (Oklahoma City, OK, US)
- Michael David CAMPBELL (Oklahoma City, OK, US)
- Johnathan Edward Peterson (Oklahoma City, OK, US)
Cpc classification
F04D13/021
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D29/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A shaft coupling for connecting a first shaft to a second shaft includes a first hub that has a shaft sleeve that fits over a portion of the first shaft. The first hub also includes a connection flange connected to the shaft sleeve. The shaft coupling further includes a compression fitting that fits over the shaft sleeve to apply a compressive force to the shaft sleeve and first shaft. The shaft coupling further includes a second hub that is connected to the second shaft and to the first hub.
Claims
1. A horizontal pumping system comprising: a suction chamber connected, wherein the suction chamber includes a stub shaft; a thrust chamber, wherein the thrust chamber includes a thrust chamber shaft that delivers torque to the stub shaft; and a shaft coupling connecting the thrust chamber shaft to the stub shaft, wherein the shaft coupling comprises: a thrust shaft hub, wherein the thrust shaft hub is connected to the stub shaft and to the thrust chamber shaft; and a compression fitting, wherein the compression fitting is connected to the thrust shaft hub.
2. The horizontal pumping system of claim 1, wherein the thrust chamber shaft comprises: a hub portion; and a shoulder.
3. The horizontal pumping system of claim 2, wherein the thrust shaft hub comprises: a shaft sleeve, wherein the shaft sleeve fits over the hub portion of the thrust chamber shaft; and a connection flange connected to the shaft sleeve.
4. The horizontal pumping system of claim 3, wherein the compression fitting surrounds an exterior of the shaft sleeve.
5. The horizontal pumping system of claim 4, wherein the compression fitting applies a compressive force to the shaft sleeve to lock the thrust shaft hub to the thrust chamber shaft.
6. The horizontal pumping system of claim 4, wherein the compression fitting is a shrink disc.
7. The horizontal pumping system of claim 6, wherein the compression fitting comprises: a first outer ring; a second outer ring; and an inner ring, wherein the inner ring is reduced in diameter when the first outer ring and the second outer ring are approximated.
8. The horizontal pumping system of claim 7, wherein the stub shaft includes a stub shaft hub that is attached to the connection flange of the thrust shaft hub.
9. A shaft coupling for connecting a thrust chamber shaft to a stub shaft, wherein the shaft coupling comprises: a thrust shaft hub, wherein the thrust shaft hub is connected to the stub shaft and to the thrust chamber shaft; and a compression fitting, wherein the compression fitting is connected to the thrust shaft hub.
10. The shaft coupling of claim 9, wherein the thrust chamber shaft comprises: a hub portion; and a shoulder.
11. The shaft coupling of claim 10, wherein the thrust shaft hub comprises: a shaft sleeve, wherein the shaft sleeve fits over the hub portion of the thrust chamber shaft; and a connection flange connected to the shaft sleeve.
12. The shaft coupling of claim 11, wherein the compression fitting surrounds an exterior of the shaft sleeve.
13. The shaft coupling of claim 12, wherein the compression fitting applies a compressive force to the shaft sleeve to lock the thrust shaft hub to the thrust chamber shaft.
14. The shaft coupling of claim 13, wherein the compression fitting is a shrink disc.
15. The shaft coupling of claim 13, wherein the compression fitting comprises: a first outer ring; a second outer ring; and an inner ring, wherein the inner ring is reduced in diameter when the first outer ring and the second outer ring are approximated.
16. The shaft coupling of claim 15, wherein the stub shaft includes a stub shaft hub that is attached to the connection flange of the thrust shaft hub.
17. A shaft coupling for connecting a first shaft to a second shaft, wherein the shaft coupling comprises: a first hub, wherein the first hub comprises: a shaft sleeve, wherein the shaft sleeve fits over a portion of the first shaft; and a connection flange connected to the shaft sleeve; a compression fitting, wherein the compression fitting fits over the shaft sleeve to apply a compressive force to the shaft sleeve and first shaft; and a second hub, wherein the second hub is connected to the second shaft and to the first hub.
18. The shaft coupling of claim 17, wherein the second hub is non-removably connected to the second shaft.
19. The shaft coupling of claim 19, wherein the first hub is removably connected to the first shaft.
20. The shaft coupling of claim 18, wherein the compression fitting comprises: a first outer ring; a second outer ring; and an inner ring, wherein the inner ring is reduced in diameter when the first outer ring and the second outer ring are approximated.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009]
[0010]
[0011]
[0012]
[0013]
[0014]
[0015]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0016] In accordance with a preferred embodiment of the present invention,
[0017] Turning to
[0018] Turning to
[0019] Turning to
[0020] Turning to
[0021] During assembly, the compression fitting 120 is loosened and placed over the shaft sleeve 128 of the thrust shaft hub 118. The thrust shaft hub 118 is then placed over the hub portion 122 of the thrust chamber shaft 110. The thrust shaft hub 118 is the loaded onto the thrust chamber shaft 110 until the shaft sleeve 128 abuts the shoulder 124. In a particularly preferred embodiment, the inner diameter of the shaft sleeve 128 is nominally a slight clearance fit to the outer diameter of the hub portion 122 of the thrust chamber shaft 110. To install the thrust shaft hub 118 onto the thrust chamber shaft 110, an assembly press (not shown) can be threaded onto the end of the thrust chamber shaft 110 and tightened to apply a force against the connection flange 126 of thrust shaft hub 118, bringing the axial face 129 into contact with the shoulder 124 of the thrust chamber shaft 110.
[0022] Once the thrust shaft hub 118 has been completely loaded onto the thrust chamber shaft 110, the compression fitting 120 is tightened to lock the thrust shaft hub 118 onto the thrust chamber shaft 110. In a particularly preferred embodiment, the compression fitting 120 is engaged by tightening compression fitting fasteners 142 to approximate the first outer ring 136 and second outer ring 138. As the first outer ring 136 and second outer ring 138 are drawn together, the inner ring 140 contracts and applies a locking compressive force to the shaft sleeve 128 and hub portion 122 of the thrust chamber shaft 110. The assembly press is removed following complete tightening of the compression fitting 120.
[0023] Next, the stub shaft 112 is connected to the thrust chamber shaft 110 by connecting the stub shaft hub 132 to the connection flange 126 of the thrust shaft hub 118. Fastener bores 130 are aligned with fastener bores 134 and fasteners 146 are tightened to lock the stub shaft 112 to the thrust chamber shaft 110. In this way, thrust generated by the pump 106 is carried through the stub shaft 112, through the shaft coupling 114 and into the thrust chamber shaft 110 via the shoulder 124. Torque is transferred from the thrust chamber shaft 110 to the stub shaft 112 through the coupling 114. The compression fitting 120 locks the thrust shaft hub 118 to the thrust chamber shaft 110 without the use of a splined or keyed connection between the thrust chamber shaft 110 and the thrust shaft hub 118. The use of the shaft coupling 114 presents a novel and improved way of connecting the stub shaft 112 to the thrust chamber shaft 110 that will find particular utility in high power applications.
[0024] It is to be understood that even though numerous characteristics and advantages of various embodiments of the present invention have been set forth in the foregoing description, together with details of the structure and functions of various embodiments of the invention, this disclosure is illustrative only, and changes may be made in detail, especially in matters of structure and arrangement of parts within the principles of the present invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed. It will be appreciated by those skilled in the art that the teachings of the present invention can be applied to other systems without departing from the scope and spirit of the present invention. As an example, the shaft coupling 114 can be used to connect any a first shaft to any corresponding second shaft.