WO2013184790A1 - Interchangeable flow restricting orifice for clamshell coupler - Google Patents

Interchangeable flow restricting orifice for clamshell coupler Download PDF

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Publication number
WO2013184790A1
WO2013184790A1 PCT/US2013/044297 US2013044297W WO2013184790A1 WO 2013184790 A1 WO2013184790 A1 WO 2013184790A1 US 2013044297 W US2013044297 W US 2013044297W WO 2013184790 A1 WO2013184790 A1 WO 2013184790A1
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WO
WIPO (PCT)
Prior art keywords
sleeve
flow
flange
flow restricting
tube
Prior art date
Application number
PCT/US2013/044297
Other languages
French (fr)
Inventor
Frederick James LAWSON
Jay Mack CAUDILL
Jon W. NEAL
Original Assignee
Eaton Corporation
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 Eaton Corporation filed Critical Eaton Corporation
Priority to EP13730986.0A priority Critical patent/EP2917627A1/en
Priority to US14/404,966 priority patent/US10552552B2/en
Priority to CA2872035A priority patent/CA2872035A1/en
Priority to CN201380029801.4A priority patent/CN104769349B/en
Priority to BR112014025591A priority patent/BR112014025591A2/en
Publication of WO2013184790A1 publication Critical patent/WO2013184790A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L23/00—Flanged joints
    • F16L23/006—Attachments
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/13—Architectural design, e.g. computer-aided architectural design [CAAD] related to design of buildings, bridges, landscapes, production plants or roads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00—Influencing flow of fluids
    • F15D1/02—Influencing flow of fluids in pipes or conduits
    • F15D1/025—Influencing flow of fluids in pipes or conduits by means of orifice or throttle elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/02—Energy absorbers; Noise absorbers
    • F16L55/027—Throttle passages
    • F16L55/02709—Throttle passages in the form of perforated plates
    • F16L55/02718—Throttle passages in the form of perforated plates placed transversely

Definitions

  • the present disclosure relates to a system for restricting fluid flow along a fluid path. More particularly, the present disclosure relates to a system of interchangeable orifices for restricting fluid flow along a fluid path.
  • Flow restriction is used to tune a flow of fluid conveyed in systems where full flow capacity is not desired to balance conveyance systems. Examples of where such flow restriction is desirable includes fuel lines for aircraft or land or sea vehicles.
  • temporary methods of creating flow restriction may be used to tune the system to determine a proper restriction orifice size. Once the proper restriction orifice size is determined, a flange containing a permanent flow restriction orifice is designed and used where the flow restriction is required in the system.
  • the temporary components are not qualified for permanent use. For example, in aircraft fuel lines, the temporary components may not be flight qualified.
  • Figures 1 and 2 illustrate a cross-section and a cut-away perspective view, respectively, of a prior art tube assembly 100.
  • the assembly 100 includes a first tube Ti having a first flange Fi adjacent a second tube T 2 having a second flange F 2 .
  • the flanges are surrounded by a sleeve S, and o-rings O or other seals are placed between the first and second flanges Fi, F 2 and the sleeve S to prevent fluid from leaking, and to lock the joint together.
  • a coupler assembly C captures the sleeve and secures the first and second flanges F 1? F 2 together.
  • the coupler assembly C is a clamshell design, having a first and second semi-circular component hingedly connected and configured to be locked in a closed position.
  • the second flange F 2 is configured to receive a removable orifice plate 110 having an orifice with a diameter smaller than the inner diameter of the first and second tubes Ti, T 2 , thereby restricting flow of fluid.
  • the orifice plate 110 is shown as having a single orifice that is substantially circular, it should be understood that a plurality of orifices of different shapes may be employed.
  • the second flange F 2 has a groove and shoulder on the inner diameter to receive the removable orifice plate 110.
  • the tube assembly 100 may be disassembled to allow an operator to remove the orifice plate 110 and replace it with another removable orifice plate having an orifice of a different size. By removing and replacing orifice plates, an operator may test different sized orifices to arrive at a desirable fluid flow, thereby tuning the system.
  • the removable orifice plate 110 contains accommodations for hardware that secures it to the second flange F 2 .
  • a seal 120 is disposed between the second flange F 2 and the removable orifice plate 110 (illustrated here as an o-ring) to prevent flow around the removable orifice plate 110.
  • a retaining wire 130 is employed to hold the removable orifice plate 110 in place.
  • Figure 3 is a cross-section of an exemplary final tube assembly 200 having a restrictive fiange 210.
  • the restrictive flange 210 is custom-made.
  • the restrictive flange may be a flight-qualified component.
  • a system for testing fluid flow includes a first tube, a first flange disposed on an end of the first tube, a second tube, and a second flange disposed on an end of the second tube.
  • the second flange is adjacent the first flange.
  • a flow restricting sleeve surrounds the first flange and the second flange.
  • the flow restricting sleeve has an inner surface and an outer surface, with a web extending from the inner surface and defining an orifice. The web extends between the first flange and the second flange.
  • a coupler assembly surrounds the flow restricting sleeve.
  • Figure 1 is a cross-section of a prior art tube assembly 100
  • Figure 2 is a cut-away perspective view of the prior art tube assembly 100
  • Figure 3 is a cross-section of an exemplary final tube assembly 200
  • Figure 4 is a perspective view of a prior art sleeve S for a tube assembly
  • Figure 5 is a perspective view of one embodiment of a flow restricting sleeve 300 for a tube assembly
  • Figure 6 is a cross-section of one embodiment of a tube assembly 400 having the flow restricting sleeve 300;
  • Figure 7 is a cut-away perspective view of the tube assembly 400;
  • Figure 8 is a front view of the prior art final tube assembly 200; and
  • Figure 9 is a front view of the tube assembly 400.
  • Figure 4 is a perspective view of a prior art sleeve S for a tube assembly.
  • the prior art sleeve S has an inner diameter and an outer diameter, and a plurality of ribs R on an outer surface configured to receive the coupler assembly.
  • ribs may be configured differently or omitted entirely.
  • the prior art sleeve may have different surface finishes.
  • FIG. 5 is a perspective view of one embodiment of a flow restricting sleeve 300 for a tube assembly.
  • the flow restricting sleeve 300 has substantially the same outer diameter and inner diameter of the sleeve S of an existing tube assembly.
  • the flow restricting sleeve 300 further includes ribs R that are substantially the same as the ribs R of the sleeve S of an existing tube assembly. Therefore, the flow restricting sleeve 300 may be employed in place of the sleeve S of an existing tube assembly. It should be understood that additional features or finishes may be employed on the inner or outer surface of the flow restricting sleeve 300 to match such features on an existing sleeve S.
  • the flow restricting sleeve 300 may be configured for any tube assembly.
  • the flow restricting sleeve 300 can be captured by a coupler assembly C in the same manner as a flight-qualified sleeve, and provide the same seal across the sleeves.
  • the flow restricting sleeve 300 further includes a web 310 having an orifice 320.
  • the web 310 is positioned halfway along the axis of the sleeve 300.
  • the web may be off-center.
  • the orifice 320 is substantially circular. In alternative embodiments (not shown), the orifice may be oval, square, triangular, or any geometric shape. In other alternative embodiments (not shown), the web may include two or more orifices.
  • the orifice 320 is machined.
  • a plurality of flow restricting sleeves 300 may be provided, wherein each flow restricting sleeve has an orifice of a different size.
  • at least one flow restricting sleeve is provided without an orifice. Such a sleeve would allow an operator to create an orifice of any desired size, such as by drilling or punching the web.
  • Figures 6 and 7 illustrate a cross-section and a cutaway perspective view, respectively, of one embodiment of a tube assembly 400 including the flow restricting sleeve 300.
  • the assembly 400 includes a first tube Ti having a first flange 410 adjacent a second tube T 2 having a second flange 420.
  • the first flange 410 is substantially the same as the second flange 420.
  • the first flange 410 is spaced from the second flange 420 by a gap having a length 1.
  • the flanges 410, 420 are surrounded by the sleeve 300, such that the web 310 extends through the gap between the first flange 410 and the second flange 420. Accordingly, the web 310 has a thickness of less than 1.
  • O-rings O or other seals are placed between the first and second flanges 410, 420 and the sleeve S to prevent fluid from leaking, and to lock the joint together.
  • a coupler assembly C captures the sleeve and secures the first and second flanges 410, 420 together.
  • the coupler assembly C is a clamshell design, having first and second semi-circular components that are hingedly connected and configured to be locked in a closed position.
  • an operator may test different flow restricting sleeves, with each flow restricting sleeve having a different orifice configuration.
  • the coupler assembly C is removed, and the flow restricting sleeve 300 containing one specific size of orifice is removed.
  • a flow restricting sleeve containing a different size of orifice is then put in place, and the coupler assembly C is reassembled over the sleeve and flanges 410, 420. This process may be repeated multiple times until the operator achieves a desired fluid flow.
  • the operator may remove the flow restricting sleeve 300 in the manner described above.
  • the operator may then remove one of the flanges 410, 420 and replace it with a unitary flange and orifice plate having an orifice with the desired dimensions, such as in the exemplary final tube assembly 200 illustrated in Figure 3.
  • the unitary flange and orifice plate may be a flight-qualified component.
  • the restricting sleeve 300 may be constructed of a material having a color different from that of a flight-qualified component.
  • the flow restricting sleeve 300 is colored red via a dyed aluminum anodizing process during manufacture. The color red is used to indicate components that are not to be used for flight.
  • the flow restricting sleeve 300 may use other colors, or other visual indicia to indicate that the sleeve is not a flight-qualified component.
  • Figure 8 is a front view of the prior art final tube assembly 200.
  • Figure 9 is a front view of the tube assembly 400.
  • the coupler assembly C that captures the sleeve contains inspection holes H in its perimeter that are used to visually verify that a sleeve is installed.
  • an inspector can see through the inspection holes H that the sleeve S is a flight-qualified component having a first color. Should a flow restricting sleeve 300 be inadvertently left in a tube assembly, an inspector can see the second color through the inspection holes H, indicating that a non-flight component is present.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Computational Mathematics (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Evolutionary Computation (AREA)
  • Architecture (AREA)
  • Measuring Volume Flow (AREA)
  • Pipe Accessories (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

A system for testing fluid flow includes a first tube Tl, a first flange 410 disposed on an end of the first tube, a second tube 12, and a second flange 420 disposed on an end of the second tube. The second flange is adjacent the first flange. A flow restricting sleeve 300 surrounds the first flange and the second flange. The flow restricting sleeve has an inner surface and an outer surface, with a web 310 extending from the inner surface and defining an orifice. The web extends between the first flange and the second flange. A coupler assembly C surrounds the flow restricting sleeve.

Description

INTERCHANGEABLE FLOW RESTRICTING ORIFICE FOR
CLAMSHELL COUPLER
RELATED APPLICATIONS
[0001] This application claims priority to U.S. Provisional Application No. 61/655,988, filed June 5, 2012, and entitled Interchangeable Flow Restricting Orifice for Claimshell Coupler.
FIELD OF INVENTION
[0002] The present disclosure relates to a system for restricting fluid flow along a fluid path. More particularly, the present disclosure relates to a system of interchangeable orifices for restricting fluid flow along a fluid path.
BACKGROUND
[0003] Flow restriction is used to tune a flow of fluid conveyed in systems where full flow capacity is not desired to balance conveyance systems. Examples of where such flow restriction is desirable includes fuel lines for aircraft or land or sea vehicles. In designing a fluid flow system, temporary methods of creating flow restriction may be used to tune the system to determine a proper restriction orifice size. Once the proper restriction orifice size is determined, a flange containing a permanent flow restriction orifice is designed and used where the flow restriction is required in the system. In some known instances, the temporary components are not qualified for permanent use. For example, in aircraft fuel lines, the temporary components may not be flight qualified.
[0004] Figures 1 and 2 illustrate a cross-section and a cut-away perspective view, respectively, of a prior art tube assembly 100. The assembly 100 includes a first tube Ti having a first flange Fi adjacent a second tube T2 having a second flange F2. The flanges are surrounded by a sleeve S, and o-rings O or other seals are placed between the first and second flanges Fi, F2 and the sleeve S to prevent fluid from leaking, and to lock the joint together. A coupler assembly C captures the sleeve and secures the first and second flanges F1? F2 together. In one embodiment, the coupler assembly C is a clamshell design, having a first and second semi-circular component hingedly connected and configured to be locked in a closed position.
[0005] In the illustrated prior art embodiment, the second flange F2 is configured to receive a removable orifice plate 110 having an orifice with a diameter smaller than the inner diameter of the first and second tubes Ti, T2, thereby restricting flow of fluid. Although the orifice plate 110 is shown as having a single orifice that is substantially circular, it should be understood that a plurality of orifices of different shapes may be employed.
[0006] The second flange F2 has a groove and shoulder on the inner diameter to receive the removable orifice plate 110. The tube assembly 100 may be disassembled to allow an operator to remove the orifice plate 110 and replace it with another removable orifice plate having an orifice of a different size. By removing and replacing orifice plates, an operator may test different sized orifices to arrive at a desirable fluid flow, thereby tuning the system.
[0007] In the illustrated embodiment, the removable orifice plate 110 contains accommodations for hardware that secures it to the second flange F2. A seal 120 is disposed between the second flange F2 and the removable orifice plate 110 (illustrated here as an o-ring) to prevent flow around the removable orifice plate 110. Additionally, a retaining wire 130 is employed to hold the removable orifice plate 110 in place.
[0008] After an operator determines a desirable orifice size, the operator may remove the second flange F2 and the removable orifice plate 110 and replace it with a unitary flange and orifice plate. Figure 3 is a cross-section of an exemplary final tube assembly 200 having a restrictive fiange 210. In one embodiment, the restrictive flange 210 is custom-made. When used in an aircraft application, the restrictive flange may be a flight-qualified component.
SUMMARY OF THE INVENTION
[0009] A system for testing fluid flow includes a first tube, a first flange disposed on an end of the first tube, a second tube, and a second flange disposed on an end of the second tube. The second flange is adjacent the first flange. A flow restricting sleeve surrounds the first flange and the second flange. The flow restricting sleeve has an inner surface and an outer surface, with a web extending from the inner surface and defining an orifice. The web extends between the first flange and the second flange. A coupler assembly surrounds the flow restricting sleeve.
BRIEF DESCRIPTION OF DRAWINGS
[0010] The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate various example systems and components that illustrate various example embodiments of aspects of the invention. It will be appreciated that the illustrated element boundaries represent one example of the boundaries. One of ordinary skill in the art will appreciate that one element may be designed as multiple elements or that multiple elements may be designed as one element. An element shown as an internal component of another element may be implemented as an external component and vice versa. The drawings may not be to scale and the proportion of certain elements may be exaggerated for the purpose of illustration.
[0011] Figure 1 is a cross-section of a prior art tube assembly 100;
[0012] Figure 2 is a cut-away perspective view of the prior art tube assembly 100;
[0013] Figure 3 is a cross-section of an exemplary final tube assembly 200;
[0014] Figure 4 is a perspective view of a prior art sleeve S for a tube assembly; [0015] Figure 5 is a perspective view of one embodiment of a flow restricting sleeve 300 for a tube assembly;
[0016] Figure 6 is a cross-section of one embodiment of a tube assembly 400 having the flow restricting sleeve 300;
[0017] Figure 7 is a cut-away perspective view of the tube assembly 400; [0018] Figure 8 is a front view of the prior art final tube assembly 200; and [0019] Figure 9 is a front view of the tube assembly 400. DETAILED DESCRIPTION
[0020] Figure 4 is a perspective view of a prior art sleeve S for a tube assembly. The prior art sleeve S has an inner diameter and an outer diameter, and a plurality of ribs R on an outer surface configured to receive the coupler assembly. In alternative embodiments, ribs may be configured differently or omitted entirely. In another alternative embodiment, the prior art sleeve may have different surface finishes.
[0021] Figure 5 is a perspective view of one embodiment of a flow restricting sleeve 300 for a tube assembly. The flow restricting sleeve 300 has substantially the same outer diameter and inner diameter of the sleeve S of an existing tube assembly. The flow restricting sleeve 300 further includes ribs R that are substantially the same as the ribs R of the sleeve S of an existing tube assembly. Therefore, the flow restricting sleeve 300 may be employed in place of the sleeve S of an existing tube assembly. It should be understood that additional features or finishes may be employed on the inner or outer surface of the flow restricting sleeve 300 to match such features on an existing sleeve S. In other words, the flow restricting sleeve 300 may be configured for any tube assembly. By having the same shape and finish, the flow restricting sleeve 300 can be captured by a coupler assembly C in the same manner as a flight-qualified sleeve, and provide the same seal across the sleeves.
[0022] The flow restricting sleeve 300 further includes a web 310 having an orifice 320. In the illustrated embodiment, the web 310 is positioned halfway along the axis of the sleeve 300. In an alternative embodiment (not shown), the web may be off-center.
[0023] In the illustrated embodiment, the orifice 320 is substantially circular. In alternative embodiments (not shown), the orifice may be oval, square, triangular, or any geometric shape. In other alternative embodiments (not shown), the web may include two or more orifices.
[0024] In one known embodiment, the orifice 320 is machined. A plurality of flow restricting sleeves 300 may be provided, wherein each flow restricting sleeve has an orifice of a different size. In one known embodiment, at least one flow restricting sleeve is provided without an orifice. Such a sleeve would allow an operator to create an orifice of any desired size, such as by drilling or punching the web.
[0025] Figures 6 and 7 illustrate a cross-section and a cutaway perspective view, respectively, of one embodiment of a tube assembly 400 including the flow restricting sleeve 300. The assembly 400 includes a first tube Ti having a first flange 410 adjacent a second tube T2 having a second flange 420. The first flange 410 is substantially the same as the second flange 420. The first flange 410 is spaced from the second flange 420 by a gap having a length 1.
[0026] The flanges 410, 420 are surrounded by the sleeve 300, such that the web 310 extends through the gap between the first flange 410 and the second flange 420. Accordingly, the web 310 has a thickness of less than 1. O-rings O or other seals are placed between the first and second flanges 410, 420 and the sleeve S to prevent fluid from leaking, and to lock the joint together. A coupler assembly C captures the sleeve and secures the first and second flanges 410, 420 together. In one embodiment, the coupler assembly C is a clamshell design, having first and second semi-circular components that are hingedly connected and configured to be locked in a closed position.
[0027] During testing, an operator may test different flow restricting sleeves, with each flow restricting sleeve having a different orifice configuration. To swap one flow restricting sleeve 300 with another during flow testing, the coupler assembly C is removed, and the flow restricting sleeve 300 containing one specific size of orifice is removed. A flow restricting sleeve containing a different size of orifice is then put in place, and the coupler assembly C is reassembled over the sleeve and flanges 410, 420. This process may be repeated multiple times until the operator achieves a desired fluid flow.
[0028] After an operator determines a desirable orifice size, the operator may remove the flow restricting sleeve 300 in the manner described above. The operator may then remove one of the flanges 410, 420 and replace it with a unitary flange and orifice plate having an orifice with the desired dimensions, such as in the exemplary final tube assembly 200 illustrated in Figure 3. When used in an aircraft application, the unitary flange and orifice plate may be a flight-qualified component.
[0029] In one embodiment, the restricting sleeve 300 may be constructed of a material having a color different from that of a flight-qualified component. In one particular embodiment, the flow restricting sleeve 300 is colored red via a dyed aluminum anodizing process during manufacture. The color red is used to indicate components that are not to be used for flight. In alternative embodiments (not shown), the flow restricting sleeve 300 may use other colors, or other visual indicia to indicate that the sleeve is not a flight-qualified component. [0030] Figure 8 is a front view of the prior art final tube assembly 200. For comparison, Figure 9 is a front view of the tube assembly 400. In both assemblies, the coupler assembly C that captures the sleeve contains inspection holes H in its perimeter that are used to visually verify that a sleeve is installed. In the final tube assembly 200, an inspector can see through the inspection holes H that the sleeve S is a flight-qualified component having a first color. Should a flow restricting sleeve 300 be inadvertently left in a tube assembly, an inspector can see the second color through the inspection holes H, indicating that a non-flight component is present.
[0031] To the extent that the term "includes" or "including" is used in the specification or the claims, it is intended to be inclusive in a manner similar to the term "comprising" as that term is interpreted when employed as a transitional word in a claim. Furthermore, to the extent that the term "or" is employed (e.g., A or B) it is intended to mean "A or B or both." When the applicants intend to indicate "only A or B but not both" then the term "only A or B but not both" will be employed. Thus, use of the term "or" herein is the inclusive, and not the exclusive use. See, Bryan A. Garner, A Dictionary of Modern Legal Usage 624 (2d. Ed. 1995). Also, to the extent that the terms "in" or "into" are used in the specification or the claims, it is intended to additionally mean "on" or "onto." Furthermore, to the extent the term "connect" is used in the specification or claims, it is intended to mean not only "directly connected to," but also "indirectly connected to" such as connected through another component or components.
[0032] While the present application has been illustrated by the description of embodiments thereof, and while the embodiments have been described in considerable detail, it is not the intention of the applicants to restrict or in any way limit the scope of the appended claims to such detail. Additional advantages and modifications will readily appear to those skilled in the art. Therefore, the application, in its broader aspects, is not limited to the specific details, the representative apparatus and method, and illustrative examples shown and described. Accordingly, departures may be made from such details without departing from the spirit or scope of the applicant's general inventive concept.

Claims

A flow restricting sleeve of a tube assembly comprising:
an inner surface;
an outer surface;
a web extending from the inner surface.
2. The flow restricting sleeve of claim 1, wherein the web comprises an orifice.
3. The flow restricting sleeve of claim 1, wherein the orifice is circular.
4. The flow restricting sleeve of claim 1, wherein the web is disposed proximate to a center along the axis of the flow restrictive sleeve.
5. The flow restricting sleeve of claim 1, further comprising a plurality of ribs disposed on the outer surface.
6. The flow restricting sleeve of claim 5, wherein the ribs are configured to receive a coupler assembly.
7. The flow restricting sleeve of claim 1, wherein the flow restrictive sleeve is configured to surround a first flange of a first tube and a second flange of a second tube.
8. A system for testing fluid flow comprising:
a first tube;
a first flange disposed on an end of the first tube
a second tube;
a second flange disposed on an end of the second tube, the second flange being adjacent the first flange; and
a flow restricting sleeve comprising an inner surface, an outer surface, and a web extending from the inner surface;
wherein the flow restricting sleeve surrounds the first flange and the second flange; and wherein the web extends between the first flange and the second flange.
9. The system of claim 8, wherein the web comprises an orifice.
10. The system of claim 9, wherein the orifice is circular.
11. The system of claim 8, wherein the flow restricting sleeve further comprises a plurality of ribs disposed on the outer surface.
12. The system of claim 8, further comprising a coupler assembly surrounding the flow restricting sleeve.
13. The system of claim 12, wherein the coupler assembly comprises an inspection hole.
14. The system of claim 8, wherein the web is disposed proximate to a center along the axis of the flow restrictive sleeve.
15. The system of claim 8, further comprising a first seal disposed between the first flange and the flow restricting sleeve, and a second seal disposed between the second flange and the flow restricting sleeve.
16. A method for testing fluid flow comprising:
disposing a first flow restricting sleeve between a first tube and a second tube, the flow restricting sleeve having a web with a an orifice of a first configuration;
testing flow through the first flow restricting sleeve between the first tube and the second tube;
replacing the first flow restricting sleeve with a second flow restricting sleeve having a web with an orifice of a second configuration;
testing the flow through the second flow restricting sleeve between the first tube and the second tube; and selecting one of the first flow restricting sleeve and the second flow restricting sleeve based on the testing of the flow through the first flow restricting sleeve and the flow through the second flow restricting sleeve.
17. The method of claim 16, wherein the step of disposing the first flow restricting sleeve between the first tube and the second tube comprises:
surrounding a first flange of the first tube and a second flange of the second tube with the first flow restrictive sleeve; and
capturing the first flow restrictive sleeve with a coupler assembly.
18. The method of claim 16, further comprising the steps of:
removing the second restricting sleeve;
removing one of the first flange and the second flange; and
disposing, between the first tube and the second tube, a unitary flange and a plate, the plate comprising an orifice having a configuration substantially equal to the configuration of the selected one of the first flow restricting sleeve and the second flow restricting sleeve.
19. The method of claim 16, further comprising the step of coloring the first flow restrictive sleeve red and coloring the second flow restrictive sleeve red.
20. The method of claim 19, further comprising the step of inspecting to identify a final tube assembly comprising one of the first flow restrictive sleeve and the second flow restrictive sleeve.
PCT/US2013/044297 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler WO2013184790A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP13730986.0A EP2917627A1 (en) 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler
US14/404,966 US10552552B2 (en) 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler
CA2872035A CA2872035A1 (en) 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler
CN201380029801.4A CN104769349B (en) 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler
BR112014025591A BR112014025591A2 (en) 2012-06-05 2013-06-05 flow restricting sleeve, fluid flow testing system and method for fluid flow testing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261655988P 2012-06-05 2012-06-05
US61/655,988 2012-06-05

Publications (1)

Publication Number Publication Date
WO2013184790A1 true WO2013184790A1 (en) 2013-12-12

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PCT/US2013/044297 WO2013184790A1 (en) 2012-06-05 2013-06-05 Interchangeable flow restricting orifice for clamshell coupler

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US (1) US10552552B2 (en)
EP (1) EP2917627A1 (en)
CN (1) CN104769349B (en)
BR (1) BR112014025591A2 (en)
CA (1) CA2872035A1 (en)
WO (1) WO2013184790A1 (en)

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US11485556B1 (en) * 2018-02-26 2022-11-01 Vincent Charles Brenner Vessel connector
CA3047289A1 (en) 2019-06-19 2020-12-19 Slurryflo Valve Corporation Flow centralizer for valve assembly
CA3047469A1 (en) 2019-06-20 2020-12-20 Slurryflo Valve Corporation Gate valve
US11691752B2 (en) * 2019-10-15 2023-07-04 The Boeing Company Dual walled tube flexible joint seal systems and methods
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CA2872035A1 (en) 2013-12-12
US10552552B2 (en) 2020-02-04
CN104769349B (en) 2017-05-03
EP2917627A1 (en) 2015-09-16
BR112014025591A2 (en) 2017-07-04
US20160063143A1 (en) 2016-03-03
CN104769349A (en) 2015-07-08

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