Multi-diameter thrust cups

Abstract

Embodiments described herein provide a multi-diameter thrust device that includes one or more thrust cups. Each thrust cup of the one or more thrust cups includes a first axial end hub disposed at a first axial end of the thrust cup; a second axial end hub disposed at a second axial end of the thrust cup; and a plurality of bowsprings. Each bowspring of the plurality of bowsprings includes a first axial end portion coupled to the first axial end hub and a second axial end portion coupled to the second axial end hub. The plurality of bowsprings are disposed circumferentially about a central axis of the multi-diameter thrust device.

1 . A multi-diameter thrust device, comprising:
 one or more thrust cups, each thrust cup of the one or more thrust cups comprising:
 a first axial end hub disposed at a first axial end of the thrust cup, wherein the first axial end of the thrust cup is configured to receive a flow of fluid; 
 a second axial end hub disposed at a second axial end of the thrust cup, wherein the second axial end of the thrust cup is configured to at least partially block the fluid from flowing axially past the second axial end of the thrust cup; and 
 a plurality of bowsprings, each bowspring of the plurality of bowsprings having a first axial end portion coupled to the first axial end hub and a second axial end portion coupled to the second axial end hub, wherein the plurality of bowsprings are disposed circumferentially about a central axis of the multi-diameter thrust device. 
   
     
     
         2 . The multi-diameter thrust device of  claim 1 , comprising a mandrel to which the one or more thrust cups may be secured radially about the mandrel, wherein the mandrel is configured to be used as a housing or a flow line. 
     
     
         3 . The multi-diameter thrust device of  claim 1 , wherein the multi-diameter thrust device comprises a mandrel, and wherein the second axial end hub of each thrust cup of the one or more thrust cups is secured to the mandrel radially about the mandrel. 
     
     
         4 . The multi-diameter thrust device of  claim 3 , wherein the first axial end hub of each thrust cup of the one or more thrust cups is configured to slide axially relative to the mandrel. 
     
     
         5 . The multi-diameter thrust device of  claim 3 , wherein the first axial end hub of each thrust cup of the one or more thrust cups is configured to receive a flow of fluid through a gap formed between the first axial end hub and the mandrel. 
     
     
         6 . The multi-diameter thrust device of  claim 3 , wherein the second axial end hub of each thrust cup of the one or more thrust cups forms a seal against the mandrel. 
     
     
         7 . The multi-diameter thrust device of  claim 1 , wherein the plurality of bowsprings of each thrust cup of the one or more thrust cups are metal bowsprings. 
     
     
         8 . The multi-diameter thrust device of  claim 1 , comprising a plurality of thrust cups disposed in series axially along the multi-diameter thrust device. 
     
     
         9 . The multi-diameter thrust device of  claim 1 , wherein the plurality of bowsprings of each thrust cup of the one or more thrust cups are configured to collapse radially. 
     
     
         10 . The multi-diameter thrust device of  claim 1 , wherein each bowspring of the plurality of bowsprings of each thrust cup of the one or more thrust cups comprises:
 a first main bowspring portion extending axially from the first axial end portion of the bowspring, wherein the first main bowspring portion is configured to be spaced circumferentially apart from first main bowspring portions of adjacent bowsprings of the plurality of bowsprings; and   a second main bowspring portion extending axially from the second axial end portion of the bowspring, wherein the first and second main bowspring portions meet at an intermediate axial location along the multi-diameter thrust device, and wherein the second main bowspring portion is configured to contact main bowspring portions of adjacent bowsprings of the plurality of bowsprings.   
     
     
         11 . The multi-diameter thrust device of  claim 1 , wherein each bowspring of the plurality of bowsprings of each thrust cup of the one or more thrust cups comprises:
 a first main bowspring portion extending axially from the first axial end portion of the bowspring, wherein the first main bowspring portion comprises a slot extending therethrough axially along the first main bowspring portion; and   a second main bowspring portion extending axially from the second axial end portion of the bowspring, wherein the first and second main bowspring portions meet at an intermediate axial location along the multi-diameter thrust device, and wherein the second main bowspring portion does not comprise a slot extending therethrough.   
     
     
         12 . The multi-diameter thrust device of  claim 1 , wherein each bowspring of the plurality of bowsprings of each thrust cup of the one or more thrust cups comprises:
 a first main bowspring portion extending axially from the first axial end portion of the bowspring, wherein the first main bowspring portion is configured to be spaced circumferentially relative to first main bowspring portions of adjacent bowsprings of the plurality of bowsprings; and   a second main bowspring portion extending axially from the second axial end portion of the bowspring, wherein the first and second main bowspring portions meet at an intermediate axial location along the multi-diameter thrust device, and wherein the second main bowspring portion is associated with a plurality of discrete asymmetrical curved fingers extending radially from the second main bowspring portion and at least partially disposed radially within the second main bowspring portion of a neighboring bowspring adjacent each other along the axial length of the second main bowspring portion.   
     
     
         13 . The multi-diameter thrust device of  claim 1 , wherein each thrust cup of the one or more thrust cups comprises a bladder disposed radially within the plurality of bowsprings of the thrust cup. 
     
     
         14 . The multi-diameter thrust device of  claim 1 , comprising one or more elastomeric swab cups disposed axially relative to the one or more thrust cups along the central axis of the multi-diameter thrust device. 
     
     
         15 . A multi-diameter thrust device, comprising:
 a mandrel configured to be used as a housing or a flow line; and   one or more thrust cups secured to the mandrel radially about the mandrel, each thrust cup of the one or more thrust cups comprising:
 a first axial end hub disposed at a first axial end of the thrust cup, wherein the first axial end hub is configured to slide axially relative to the mandrel; 
 a second axial end hub secured to the mandrel at a second axial end of the thrust cup; and 
 a plurality of bowsprings configured to collapse radially, each bowspring of the plurality of bowsprings having a first axial end portion coupled to the first axial end hub and a second axial end portion coupled to the second axial end hub, wherein the plurality of bowsprings are disposed circumferentially about a central axis of the multi-diameter thrust device; and wherein each bowspring of the plurality of bowsprings comprises:
 a first main bowspring portion extending axially from the first axial end portion of the bowspring, wherein the first main bowspring portion comprises a slot extending therethrough axially along the first main bowspring portion; and 
 a second main bowspring portion extending axially from the second axial end portion of the bowspring, wherein the first and second main bowspring portions meet at an intermediate axial location along the multi-diameter thrust device, and wherein the second main bowspring portion does not comprise a slot extending therethrough; and 
 
 wherein each thrust cup of the one or more thrust cups is configured to receive a flow of fluid at the first axial end of the thrust cup, and to at least partially block the fluid from flowing axially past the second axial end of the thrust cup. 
   
     
     
         16 . The multi-diameter thrust device of  claim 15 , wherein the plurality of bowsprings of each thrust cup of the one or more thrust cups are metal bowsprings. 
     
     
         17 . The multi-diameter thrust device of  claim 15 , comprising a plurality of thrust cups disposed in series axially along the multi-diameter thrust device. 
     
     
         18 . A multi-diameter thrust device, comprising:
 a mandrel configured to be used as a housing or a flow line; and   one or more thrust cups secured to the mandrel radially about the mandrel, each thrust cup of the one or more thrust cups comprising:
 a first axial end hub disposed at a first axial end of the thrust cup, wherein the first axial end hub is configured to slide axially relative to the mandrel; 
 a second axial end hub secured to the mandrel at a second axial end of the thrust cup; and 
 a plurality of bowsprings configured to collapse radially, each bowspring of the plurality of bowsprings having a first axial end portion coupled to the first axial end hub and a second axial end portion coupled to the second axial end hub, wherein the plurality of bowsprings are disposed circumferentially about a central axis of the multi-diameter thrust device; and wherein each bowspring of the plurality of bowsprings comprises:
 a first main bowspring portion extending axially from the first axial end portion of the bowspring, wherein the first main bowspring portion is configured to be spaced circumferentially relative to first main bowspring portions of adjacent bowsprings of the plurality of bowsprings; and 
 a second main bowspring portion extending axially from the second axial end portion of the bowspring, wherein the first and second main bowspring portions meet at an intermediate axial location along the multi-diameter thrust device, and wherein the second main bowspring portion is associated with a plurality of discrete asymmetrical curved fingers extending radially from the second main bowspring portion and at least partially disposed radially within the second main bowspring portion of a neighboring bowspring adjacent each other along the axial length of the second main bowspring portion; and 
 
 wherein each thrust cup of the one or more thrust cups is configured to receive a flow of fluid at the first axial end of the thrust cup, and to at least partially block the fluid from flowing axially past the second axial end of the thrust cup. 
   
     
     
         19 . The multi-diameter thrust device of  claim 18 , wherein the plurality of bowsprings of each thrust cup of the one or more thrust cups are metal bowsprings. 
     
     
         20 . The multi-diameter thrust device of  claim 18 , comprising a plurality of thrust cups disposed in series axially along the multi-diameter thrust device.