US2396653A - Hydraulic system - Google Patents

Hydraulic system Download PDF

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Publication number
US2396653A
US2396653A US478989A US47898943A US2396653A US 2396653 A US2396653 A US 2396653A US 478989 A US478989 A US 478989A US 47898943 A US47898943 A US 47898943A US 2396653 A US2396653 A US 2396653A
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United States
Prior art keywords
pressure
valve
line
liquid
air
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Expired - Lifetime
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US478989A
Inventor
Hermanny Heinrich
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Bendix Aviation Corp
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Bendix Aviation Corp
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Publication date
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Priority to US478989A priority Critical patent/US2396653A/en
Priority to US651137A priority patent/US2539134A/en
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Publication of US2396653A publication Critical patent/US2396653A/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/0007—Fluidic connecting means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/17—Coupling arrangements to the indicating device
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0753—Control by change of position or inertia of system
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/2931—Diverse fluid containing pressure systems
    • Y10T137/3115—Gas pressure storage over or displacement of liquid
    • Y10T137/3118—Surge suppression
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7781—With separate connected fluid reactor surface
    • Y10T137/7784—Responsive to change in rate of fluid flow
    • Y10T137/7785—Valve closes in response to excessive flow
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7781—With separate connected fluid reactor surface
    • Y10T137/7784—Responsive to change in rate of fluid flow
    • Y10T137/7787—Expansible chamber subject to differential pressures

Definitions

  • This invention relates to hydraulic systems, and particularly to the control of pressure surges to prevent damage to parts of such a system.
  • An object of the invention is to provide a novel method and means of absorbing a suddenly applied pressure impulse of abnormally great magnitude, such as might result; from an explosion under the surface of a body of water in which is located a vessel, such as a ship or submarine carrying susceptible parts of a hydraulic system.
  • the invention is herein illustrated as applied to the protection of a hydraulic circuit which includes a bellows assembly of a character employed in marine measuring apparatus; but it is to be understood that the invention has broader 1 application and that its scope is defined by the to a bellows assembly 6, divided (by a diaphragm i) into two chambers 8 and 9, the former receiving the pressure (Pltot) conduit ii and the latter receiving the static conduit l2; the index actuating rod is being attached to the diaphragm i for operation of any associated measuring or other apparatus (as in Rydberg Patent No. 1,968,- 539, for example). The inner spaces it and ii are exposed to the pressure of the atmosphere surrounding the unit 5, as is customary.
  • Numeral as designates a rodmeter, as it is termed in the art, having terminal openings as and 20 for the conduits ii and i2, respectively; the said rodmeter it being attached to the hull of the vessel, so that openings i9 and 20 are exposed to the open sea, as are openings 3 and in Fig. 1 oithe Rydberg patent, above identifled.
  • Numerals 2i and 22 designate automatic valve assemblies, and valves 23 and 26 are provided to permit temporary Icy-passing of the valves 2i and 22, respectively, during conditioning and servicing.
  • Air collectors 26 and 2? are provided in the lines ii and i2, respectively; each air collector including a tube (as at 36) projecting externally and adapted to be vented to atmosphere, when desired, by opening of vent valve 3i or 32, as the case may be, and projecting internally sumciently (c1. rev-s8) to insure the trapping of a quantity of air at all times Operation If the pressure increases suddenly due to the 5 explosion of a depth charge, the entrapped air .in collectors 26 and 2'? is compressed by the inrush of water through the SlllibbEl valves 2i and 22.
  • Varying the volume of air trapped in the collectors will vary the amount of water flowing through the snubber valves for a given pressure difference. Changing the distance between each snubber orifice and its valve will determine the time required to eiiectively block the passage.
  • Each valve is slotted at its base, as indicated at 62 in Fig. 3, and each carries a rod or valve stem is to maintain it in seating relationship to its orifice 33.
  • valve means in said line automatically operable to shut off fluid flow by flow resulting from a sudden pressure. surge of redetermined magnitude in said line from said fluid pressure source towards said pressure-responsive device; and resilient liquidcushioning means, disposed in said line between said valve means and said pressure-responsive device, thereby providing for movement of liquid in said line and closure of said valve means in response to said sudden pressure surge, without injuring said pressure-responsive device.
  • resilient cushion means in said line operable to permit a sudden pressure surge in one part of said line without transmitting a corresponding sudden pressure surge to the line adjacent said pressureresponsive device; and valve means in said line asoaecs between said cushion means and said source of variable fluid pressure automatically operable to cut oil fluid flow by flow resulting from a sudden pressure surge of predetermined magnitude in said one part of said line, to thereby prevent sudden pressure surges originating at said source of fluid pressure from being transmitted to said pressure-responsive device.
  • valve means ⁇ operably associated with said conduit means and. automatically operable by flow resulting from hydraulic surges of predetermined magnitude, for cutting off communication between said source oi pressure and said pressure-responsive device for protecting the latter against rupture; and means for adjustably predetermining the closing action of said valve means, comprising air cushion means communicating with said conduit means intermediate said valv mean and said pressure-responsive device and embodying means for selectively varying the volumetric air capacity thereof.
  • hydraulic cushion means operably associated with said conduit means between said source of fluid pressure and said pressure-responsive device for preventing sudden pressure surges from being transmitted undiminished in magnitude from said source of fluid pressure to said pressure-responsive device, comprising chamber means communicating adjacent its bottom with said conduit means and having air vent means adjacent the top thereof, said air vent means being operable to vent enly a portion of the upper part of said chamber, whereby an air cushion of predetermined volume is maintained in said chamber at all times, and pressure-responsive valve means operably associated with said conduit means beitween said source of fluid pressure and said hydrauiic cushion means and automatically operable to shut ofi fluid flow through said conduit means by flow resulting from a sudden pressure surge of predetermined magnitude in said conduit means.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pipe Accessories (AREA)

Description

March 19, 1946.
H. HERMANNY HYDRAULIC SYSTEM Filed March 12, 1945 IN VEN TOR Patented Mar. 19, 1946 HYDRAC SYSTEM vllilelnrich Hermanny, Valley Stream, N. EL, assignor to Bendix Aviation Corporation, Bendix, N. .li.,'a corporation of Delaware Application March 12, 1943, Serial No. 478,989
8 Claims.
This invention relates to hydraulic systems, and particularly to the control of pressure surges to prevent damage to parts of such a system.
An object of the invention is to provide a novel method and means of absorbing a suddenly applied pressure impulse of abnormally great magnitude, such as might result; from an explosion under the surface of a body of water in which is located a vessel, such as a ship or submarine carrying susceptible parts of a hydraulic system.
The invention is herein illustrated as applied to the protection of a hydraulic circuit which includes a bellows assembly of a character employed in marine measuring apparatus; but it is to be understood that the invention has broader 1 application and that its scope is defined by the to a bellows assembly 6, divided (by a diaphragm i) into two chambers 8 and 9, the former receiving the pressure (Pltot) conduit ii and the latter receiving the static conduit l2; the index actuating rod is being attached to the diaphragm i for operation of any associated measuring or other apparatus (as in Rydberg Patent No. 1,968,- 539, for example). The inner spaces it and ii are exposed to the pressure of the atmosphere surrounding the unit 5, as is customary.
Numeral as designates a rodmeter, as it is termed in the art, having terminal openings as and 20 for the conduits ii and i2, respectively; the said rodmeter it being attached to the hull of the vessel, so that openings i9 and 20 are exposed to the open sea, as are openings 3 and in Fig. 1 oithe Rydberg patent, above identifled. Numerals 2i and 22 designate automatic valve assemblies, and valves 23 and 26 are provided to permit temporary Icy-passing of the valves 2i and 22, respectively, during conditioning and servicing.
Air collectors 26 and 2? are provided in the lines ii and i2, respectively; each air collector including a tube (as at 36) projecting externally and adapted to be vented to atmosphere, when desired, by opening of vent valve 3i or 32, as the case may be, and projecting internally sumciently (c1. rev-s8) to insure the trapping of a quantity of air at all times Operation If the pressure increases suddenly due to the 5 explosion of a depth charge, the entrapped air .in collectors 26 and 2'? is compressed by the inrush of water through the SlllibbEl valves 2i and 22. The piston it of each valve rises and closes ofi its upper orifice, thus blocking the iurther passage of water before the pressure applied has increased sufficiently to injure the bellows assembly 6. As soon as the pressure subsides, the pistons will drop due to gravity and the system will again be safe for normal operation.
Varying the volume of air trapped in the collectors will vary the amount of water flowing through the snubber valves for a given pressure difference. Changing the distance between each snubber orifice and its valve will determine the time required to eiiectively block the passage.
These values can be determined experimentally and so fixed that normal changes in pressure due to diving or acceleration of the vessel will not actuate the snubbers, but any sudden increase will move the pistons ii to the cut-on ositions.
' Each valve is slotted at its base, as indicated at 62 in Fig. 3, and each carries a rod or valve stem is to maintain it in seating relationship to its orifice 33.
What is claimed is:
1. A protective system including, in combination with'liquid-filled line embodying a unit to be protected, pressure surge limiting means in= eluding a valve movable to shut off communication with said unit by flow resulting from sudden pressure surge application, and means located in said line between said valve and said unit for cushioning the shock of the sudden pressure surge application as said valve is moving to the shut-off position, said last-named means includinga vessel in which air is trapped at one end and liquid is admissible at the other end to compress said air in response to a pressure rise at the point of liquid admission.
2. In a hydraulic system, in combination with a pressure responsive element and a liquid-filled conduit leading thereto, means in said conduit to cut 0d flow therethrough in response to flow resulting from pressure surge, and means located in said line between said cut-off means and said unit including an air-cushioned liquid container coactlng with said cut-oil means to thereby provide for movement of liquid in said conduit and movement of said cut-off means to the cut-0d position.
3. In a hydraulic system having a liquid-filled line leading from a source of variable fluid pressure to a pressure-responsive device, valve means in said line automatically operable to shut off fluid flow by flow resulting from a sudden pressure. surge of redetermined magnitude in said line from said fluid pressure source towards said pressure-responsive device; and resilient liquidcushioning means, disposed in said line between said valve means and said pressure-responsive device, thereby providing for movement of liquid in said line and closure of said valve means in response to said sudden pressure surge, without injuring said pressure-responsive device.
4. In a hydraulic system having a liquid-filled line leading from a source of variable fluid pressure to a pressure-responsive device, resilient cushion means in said line operable to permit a sudden pressure surge in one part of said line without transmitting a corresponding sudden pressure surge to the line adjacent said pressureresponsive device; and valve means in said line asoaecs between said cushion means and said source of variable fluid pressure automatically operable to cut oil fluid flow by flow resulting from a sudden pressure surge of predetermined magnitude in said one part of said line, to thereby prevent sudden pressure surges originating at said source of fluid pressure from being transmitted to said pressure-responsive device.
5. The hydraulic apparatus defined in claim 4. wherein said valv means is operable to cut ofl liquid flow only in the direction of said pressureresponsive device. 4
6. The hydraulic apparatus defined in claim 4, wherein said line leading from said source of fluid pressure to said pressure-responsive device is normally completely'fllled with liquid, and said resilient liquid cushion means comprises a side branch in said line leading to a closed chamber partially filled with liquid and defining an air' cushion.
7. In a hydraulic apparatus having condui means leading from a source oi variable fluid pressure to a pressure-responsive device and mirmaliy completely filled with liquid, valve means\ operably associated with said conduit means and. automatically operable by flow resulting from hydraulic surges of predetermined magnitude, for cutting off communication between said source oi pressure and said pressure-responsive device for protecting the latter against rupture; and means for adjustably predetermining the closing action of said valve means, comprising air cushion means communicating with said conduit means intermediate said valv mean and said pressure-responsive device and embodying means for selectively varying the volumetric air capacity thereof.
8. In a hydraulic system of the type embodying conduit means leading from a source of variable fluid pressure to a pressure-responsive device, hydraulic cushion means operably associated with said conduit means between said source of fluid pressure and said pressure-responsive device for preventing sudden pressure surges from being transmitted undiminished in magnitude from said source of fluid pressure to said pressure-responsive device, comprising chamber means communicating adjacent its bottom with said conduit means and having air vent means adjacent the top thereof, said air vent means being operable to vent enly a portion of the upper part of said chamber, whereby an air cushion of predetermined volume is maintained in said chamber at all times, and pressure-responsive valve means operably associated with said conduit means beitween said source of fluid pressure and said hydrauiic cushion means and automatically operable to shut ofi fluid flow through said conduit means by flow resulting from a sudden pressure surge of predetermined magnitude in said conduit means.
HEINRICH HERMANNY.
US478989A 1943-03-12 1943-03-12 Hydraulic system Expired - Lifetime US2396653A (en)

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US651137A US2539134A (en) 1943-03-12 1946-03-01 Hydraulic system

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2592464A (en) * 1948-12-07 1952-04-08 Shell Dev Continuous proportional sampler
US2705020A (en) * 1950-10-26 1955-03-29 Virgil L Frantz Fluid pressure actuated control valve
US2768704A (en) * 1954-07-20 1956-10-30 John T Cronkhite Apparatus for facilitating flow of liquid through gathering pipe lines to a pump supplying a main pressure line
US3094281A (en) * 1961-05-05 1963-06-18 Carl O Myers Boiler top mounting arrangement for pressure relief valves
WO1991005201A1 (en) * 1989-09-29 1991-04-18 Jaromir Tobias Active accumulator vibration absorbing system
US5018698A (en) * 1989-09-29 1991-05-28 Jaromir Tobias Motor vehicle vibration isolation support mounting system
US5101929A (en) * 1989-07-18 1992-04-07 Jaromir Tobias Vibration isolation support mounting system
US5141202A (en) * 1989-09-29 1992-08-25 Jaromir Tobias Active accumulator vibration absorbing support system
US5168703A (en) * 1989-07-18 1992-12-08 Jaromir Tobias Continuously active pressure accumulator power transfer system
US5310017A (en) * 1989-07-18 1994-05-10 Jaromir Tobias Vibration isolation support mounting system

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2592464A (en) * 1948-12-07 1952-04-08 Shell Dev Continuous proportional sampler
US2705020A (en) * 1950-10-26 1955-03-29 Virgil L Frantz Fluid pressure actuated control valve
US2768704A (en) * 1954-07-20 1956-10-30 John T Cronkhite Apparatus for facilitating flow of liquid through gathering pipe lines to a pump supplying a main pressure line
US3094281A (en) * 1961-05-05 1963-06-18 Carl O Myers Boiler top mounting arrangement for pressure relief valves
US5101929A (en) * 1989-07-18 1992-04-07 Jaromir Tobias Vibration isolation support mounting system
US5168703A (en) * 1989-07-18 1992-12-08 Jaromir Tobias Continuously active pressure accumulator power transfer system
US5310017A (en) * 1989-07-18 1994-05-10 Jaromir Tobias Vibration isolation support mounting system
WO1991005201A1 (en) * 1989-09-29 1991-04-18 Jaromir Tobias Active accumulator vibration absorbing system
US5018698A (en) * 1989-09-29 1991-05-28 Jaromir Tobias Motor vehicle vibration isolation support mounting system
US5050835A (en) * 1989-09-29 1991-09-24 Jaromir Tobias Active accumulator vibration absorbing support system
US5141202A (en) * 1989-09-29 1992-08-25 Jaromir Tobias Active accumulator vibration absorbing support system

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