GB615919A - Improvements in or relating to fluid flow proportioning valves - Google Patents

Improvements in or relating to fluid flow proportioning valves

Info

Publication number
GB615919A
GB615919A GB11716/46A GB1171646A GB615919A GB 615919 A GB615919 A GB 615919A GB 11716/46 A GB11716/46 A GB 11716/46A GB 1171646 A GB1171646 A GB 1171646A GB 615919 A GB615919 A GB 615919A
Authority
GB
United Kingdom
Prior art keywords
grooves
piston
fluid
line
flow
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB11716/46A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB615919A publication Critical patent/GB615919A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D11/00Control of flow ratio
    • G05D11/003Control of flow ratio using interconnected flow control elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/022Flow-dividers; Priority valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Damping Devices (AREA)
  • Multiple-Way Valves (AREA)

Abstract

615,919. Fluid-actuated valves. BENDIX AVIATION CORPORATION. April 16,1946, No. 11716. Convention date, April 23, 1945. [Class 135] Apparatus for dividing a fluid stream into two, e.g. equal, streams or uniting two streams equally comprises a valve body 10, Fig. 2, having a main line 55 communicating through ports 74, 75, Figs. 3, 5, in a spring-loaded sleeve 58 and ducts 70, 71 with the ends 72, 73 of a cylinder 14 having a piston 15 formed with pairs of grooves 22, 23 and 24, 25 coacting respectively with grooves 16, 17 in the cylinder wall which are in open communication with branch lines 20, 21, Fig. 4. The ports 74, 75 in the sleeve 58 are controlled by a spring- loaded piston 63, the position of which depends upon the pressure in the line 55, and flow from the cylinder ends to the grooves 16, 17 is controlled by spring-loaded check valves 39, Fig. 5, and 49, Fig. 4, and in the reverse direction by check valves 27, 42. Leakage of fluid between the grooves 16 and 17 past the piston 15 is prevented by the fluid pressure in grooves 78, 79 communicating through bores 44, 31 respectively with the cylinder spaces 72, 73. When the apparatus functions to divide into equal parts a fluid stream entering the line 55, the pressure of the fluid presses back the piston 63, Fig. 3, to open the ports 74, 75 through which the fluid flows to the cylinder spaces 72, 73 and thence past the valves 39, 49 and the spaces 22a, Fig. 5, and 25a, Fig. 4, to the grooves 16, 17 and the branch lines 20, 21. If, e.g. the flow through the line 21 becomes too great, the pressure in the cylinder space 73 falls and the piston 15 moves to the right, thus increasing the space 22a and the flow through the groove 16 to the line 20, and reducing the space 25a and the flow through the groove 17 to the line 21. When the apparatus functions to unite the flows entering the valve body through the lines 20, 21, the fluid from these lines flows from the grooves 16, 17 into the grooves 23, 24 and thence past the valves 27, Fig. 4, and 42, Fig. 5, into the spaces 72, 73, and then via the ducts 70, 71 and the ports 74, 75 to the line 55. Differences in flow result in corresponding differences in the pressures in the spaces 72, 73 and movement of the piston to equalize the flow. The valve may be modified to produce unequal flows by making the ports 74, 75 of unequal size, forming the piston 15 with ends of unequal area, or loading one end of the piston by a light spring. Specification 599,012 is referred to.
GB11716/46A 1945-04-23 1946-04-16 Improvements in or relating to fluid flow proportioning valves Expired GB615919A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US615919XA 1945-04-23 1945-04-23

Publications (1)

Publication Number Publication Date
GB615919A true GB615919A (en) 1949-01-13

Family

ID=22036792

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11716/46A Expired GB615919A (en) 1945-04-23 1946-04-16 Improvements in or relating to fluid flow proportioning valves

Country Status (1)

Country Link
GB (1) GB615919A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2521369A (en) * 1944-11-03 1950-09-05 Air Preheater Multifluid heat exchanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2521369A (en) * 1944-11-03 1950-09-05 Air Preheater Multifluid heat exchanger

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