GB824365A - Improvements in pulsation dampening or surge absorbing apparatus - Google Patents

Improvements in pulsation dampening or surge absorbing apparatus

Info

Publication number
GB824365A
GB824365A GB35844/56A GB3584456A GB824365A GB 824365 A GB824365 A GB 824365A GB 35844/56 A GB35844/56 A GB 35844/56A GB 3584456 A GB3584456 A GB 3584456A GB 824365 A GB824365 A GB 824365A
Authority
GB
United Kingdom
Prior art keywords
sleeve
mandrel
orifices
pressure
lobes
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
GB35844/56A
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.)
Westinghouse Air Brake Co
Original Assignee
Westinghouse Air Brake Co
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 Westinghouse Air Brake Co filed Critical Westinghouse Air Brake Co
Publication of GB824365A publication Critical patent/GB824365A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/04Devices damping pulsations or vibrations in fluids
    • F16L55/045Devices damping pulsations or vibrations in fluids specially adapted to prevent or minimise the effects of water hammer
    • F16L55/05Buffers therefor
    • F16L55/052Pneumatic reservoirs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L55/00Devices or appurtenances for use in, or in connection with, pipes or pipe systems
    • F16L55/04Devices damping pulsations or vibrations in fluids
    • F16L55/045Devices damping pulsations or vibrations in fluids specially adapted to prevent or minimise the effects of water hammer
    • F16L55/05Buffers therefor
    • F16L55/052Pneumatic reservoirs
    • F16L55/053Pneumatic reservoirs the gas in the reservoir being separated from the fluid in the pipe
    • F16L55/054Pneumatic reservoirs the gas in the reservoir being separated from the fluid in the pipe the reservoir being placed in or around the pipe from which it is separated by a sleeve-shaped membrane

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Combined Devices Of Dampers And Springs (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

824,365. Pressure-relieving devices for fluids. WESTINGHOUSE AIR BRAKE CO. Nov. 23, 1956 [Nov. 25, 1955 (2); Dec. 29, 1955; Jan. 30, 1956; Jan. 31, 1956 ; Feb. 27, 1956; March 27, 1956], No. 35844/56. Class 135. A pulsation dampening or surge absorbing apparatus for installation in a conduit conducting fluid comprises a hollow mandrel having a plurality of throttling orifices in its wall and surrounded by an elastic sleeve defining a space between itself and the mandrel, the mandrel or the sleeve being provided with spaced projections disposed within said space and affording a support for the sections of the sleeve intermediate the projections and resilient means being provided externally of the sleeve to restrain radial distention thereof. The cylindrical mandrel 11, Fig. 1, is fitted by screwthreaded ends 6, 7 to a pipe line carrying fluid under pressure. The mandrel 11 has longitudinal rows of orifices 25, 26, 27, 28 and longitudinal lobes 21, 22, 23, 24, Fig. 2. Surrounding the mandrel and abutting the lobes is an elastic sleeve 18 and spaced from the sleeve is a cylindrical casing 10. The outer flanges 19, 20 of the sleeve 18 are clamped between end plates 12, 13 and flanges 47, 48 of the casing 10. A valve 37 may be operated to introduce compressed air into the space 31 and a gauge 34 indicates the pressure of such air which pressure is selected in accordance with the expected value of the pulsations in the pipe line to which the apparatus is attached. The pulsating fluid flows out through the orifices 25, 26, 27, 28 to radially expand the sleeve 18 and during the pressure reduction which follows a surge the air pressure on the sleeve 18 forces it inwardly against the surface of the mandrel. In a second example, Figs. 3 and 4, the mandrel 11 has three longitudinal lobes and is located by pins 66, 67 between the end plates 12, 13 which have threaded bores 70, 71. The compressed air is introduced by the bore 64 to force the sleeve away from the casing wall, grooves 77 being provided to facilitate this movement. The bolts 76 hold the assembly together. In another example, Fig. 5, the lobes are formed by rods 80 of semi-circular cross-section spot-welded to the mandrel 11. The orifices 84 in the mandrel open into annular grooves 85. The casing 10 is formed by a central section 86 and two end sections 87, 88 welded thereto. Cupshaped members 82, 83 which locate the rods 80 are held in the flanges 12, 13. In another similar example, Fig. 9, the rods 93 are of arcuate cross-section and they are aligned with the orifices 84 and are provided with slots 94. In another example, Fig. 12, the mandrel 11 is tubular and the sleeve 18 has inwardly projecting ribs 140, 141, 142, 143 which abut the mandrel between the orifices 112, 113, 114, 115. The tops of the ribs may be curved or, as shown, flat. The sleeve 18 may be longitudinally corrugated, Fig. 19. In another example, Fig. 14, the sleeve 18 is annularly corrugated, the inner ribs resting on the mandrel 11. The sleeve may comprise two separate sleeves, Fig. 17, the inner one of a material having a high resistance to chemical action by the fluid and the outer one of a material having a high elasticity and strength. A lubricant, e.g. graphite, or a reinforcing sleeve, e.g. of nylon, may be interposed between the two sleeves.
GB35844/56A 1955-12-29 1956-11-23 Improvements in pulsation dampening or surge absorbing apparatus Expired GB824365A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US824365XA 1955-12-29 1955-12-29

Publications (1)

Publication Number Publication Date
GB824365A true GB824365A (en) 1959-11-25

Family

ID=22171210

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35844/56A Expired GB824365A (en) 1955-12-29 1956-11-23 Improvements in pulsation dampening or surge absorbing apparatus

Country Status (1)

Country Link
GB (1) GB824365A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3387630A (en) * 1965-04-22 1968-06-11 Dow Chemical Co Adjustable pressure reducing device
US4191358A (en) * 1977-04-15 1980-03-04 Luwa Ag Shutoff device
US4234885A (en) * 1979-09-10 1980-11-18 A. B. Dick Company Remote ink valve
DE3210239A1 (en) * 1982-03-20 1983-10-06 Heinz M Naegel Air vessel for compensating flow rate fluctuations in pressure lines of pumps and the like
GB2198478A (en) * 1986-12-08 1988-06-15 Hypro Corp Surge suppressor
US4785841A (en) * 1988-04-05 1988-11-22 Innovac Technology Inc. Bladder valve
GB2234015A (en) * 1986-12-08 1991-01-23 Hypro Corp Surge suppressor
WO2017062396A1 (en) * 2015-10-08 2017-04-13 Shell Oil Company Shock mitigation devices
CN110319303A (en) * 2019-07-15 2019-10-11 郑州工程技术学院 The composite pressure pipe of hydraulic pressure frequent fluctuation impact force can be reduced
US11248731B2 (en) * 2017-10-19 2022-02-15 Khs Gmbh Device and method for aseptic pressure relief

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3387630A (en) * 1965-04-22 1968-06-11 Dow Chemical Co Adjustable pressure reducing device
US4191358A (en) * 1977-04-15 1980-03-04 Luwa Ag Shutoff device
US4234885A (en) * 1979-09-10 1980-11-18 A. B. Dick Company Remote ink valve
FR2464754A1 (en) * 1979-09-10 1981-03-20 Dick Co Ab VALVE CONTROL SYSTEM FOR THE FLOW OF A PRESSURIZED LIQUID TO A HEAD, IN PARTICULAR AN INK JET PRINTING
DE3210239A1 (en) * 1982-03-20 1983-10-06 Heinz M Naegel Air vessel for compensating flow rate fluctuations in pressure lines of pumps and the like
GB2234015B (en) * 1986-12-08 1991-05-22 Hypro Corp Surge suppressor
GB2234015A (en) * 1986-12-08 1991-01-23 Hypro Corp Surge suppressor
GB2198478B (en) * 1986-12-08 1991-05-01 Hypro Corp Surge suppressor
GB2198478A (en) * 1986-12-08 1988-06-15 Hypro Corp Surge suppressor
US4785841A (en) * 1988-04-05 1988-11-22 Innovac Technology Inc. Bladder valve
WO2017062396A1 (en) * 2015-10-08 2017-04-13 Shell Oil Company Shock mitigation devices
US11248731B2 (en) * 2017-10-19 2022-02-15 Khs Gmbh Device and method for aseptic pressure relief
CN110319303A (en) * 2019-07-15 2019-10-11 郑州工程技术学院 The composite pressure pipe of hydraulic pressure frequent fluctuation impact force can be reduced

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