[go: up one dir, main page]

US3477464A - Surge cut-off device for pressure sensing units - Google Patents

Surge cut-off device for pressure sensing units Download PDF

Info

Publication number
US3477464A
US3477464A US665910A US3477464DA US3477464A US 3477464 A US3477464 A US 3477464A US 665910 A US665910 A US 665910A US 3477464D A US3477464D A US 3477464DA US 3477464 A US3477464 A US 3477464A
Authority
US
United States
Prior art keywords
pressure
annular space
ring
surge
passage
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 - Lifetime
Application number
US665910A
Inventor
John J Ryan
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.)
H AND R DEV CO Inc
Original Assignee
H AND R DEV CO Inc
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 H AND R DEV CO Inc filed Critical H AND R DEV CO Inc
Application granted granted Critical
Publication of US3477464A publication Critical patent/US3477464A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K17/00Safety valves; Equalising valves, e.g. pressure relief valves
    • F16K17/02Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side
    • F16K17/04Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side spring-loaded
    • F16K17/0466Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side spring-loaded with a special seating surface
    • 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
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K15/00Check valves
    • F16K15/14Check valves with flexible valve members
    • F16K15/141Check valves with flexible valve members the closure elements not being fixed to the valve body
    • F16K15/142Check valves with flexible valve members the closure elements not being fixed to the valve body the closure elements being shaped as solids of revolution, e.g. toroidal or cylindrical rings
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S116/00Signals and indicators
    • Y10S116/42Oil filter
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7837Direct response valves [i.e., check valve type]
    • Y10T137/7869Biased open

Definitions

  • the present invention relates to a surge cut-off device for fluid pressure sensing units and more particularly to such a device employing a resilient O-ring which is distorted by surges in pressure to block the passage of thefluid under pressure.
  • Another object of the invention is to provide a surge cut-ofi device for fluid pressure systems wherein surges in pressure are blocked and kept from the pressure sensingunit while gradual increases in pressure are measured.
  • the surge cut-off device comprises a housing having a pressure chamber and an annular space surrounding the pressure chamber.
  • One end of the annular space is provided with a conical surface and there are passage means between the pressure chamber and the annular space, and further passage means between the conical end of the annular space and the exterior of the housing for connection to a source of pressure.
  • a resilient O-ring is positioned within the annular space between the two passage means. There is a predetermined clearance between the O-riug and a surface of the annular space so as to permit a predetermined flow rate of fluid between the first and second passages.
  • the O-ring is of suflicient resiliency so as to be movable or distortable to block the passage between the annular space and the pressure chamber when a surge of fluid pressure is received in the annular chamber from the pressure source.
  • the housing may be made of two concentric tubular 3,477,464 Patented Nov. 11, 1969 members formed to define the annular space therebetween.
  • the O-ring may be positioned in a shallow groove formed in the inner surface of the annular space.
  • FIG. 1 is a longitudinal sectional view of the surge cut-off device of the present invention
  • FIG. 2 is a portion of the view in FIG. 1 in enlarged scale and showing the position of the O-ring within the annular space between the two passages;
  • FIG. 3 is a view similar to FIG. 2 but showing the O-ring in distorted position in response to a surge of pressure into the annular space.
  • the surge cut-ofl? device is indicated generally at 1 and comprises a housing 2 formed of an outer tubular member 3 and an inner tubular member 4 which are fixed with respect to each other in the position shown in FIG. 1.
  • Outer tubular member 3 has a smaller internal diameter portion 5 and a larger internal diameter portion 6, the inner tubular member 4 having corresponding smaller diameter portion 7 and larger diameter portion 8.
  • the two diameter portions 5 and 6 of the outer tubular member are interconnected by a conical surface 9. When the tubular members are positioned as shown in FIG. 1, there is defined therebetween an annular space 10.
  • An inclined passage 11 is formed in the inner tubular member to provide communication between the annular space 10 and a pressure chamber 12 located within the inner tubular member.
  • a second passage 13 is provided in the outer tubular member to communicate between the conical portion of the annular space and the exterior of the cut-off device. The passage 13 is adapted for connection to a source of fluid pressure.
  • annular space 10 Positioned in annular space 10 are two resilient 0- rings 14 and 15 made of natural or synthetic rubber or a suitable plastic material.
  • the O-ring 14 is positioned at the upper end of the annular space as viewed in FIG. 1 and is above the opening to passage 11.
  • O-ring 15 is positioned in a shallow groove 16 formed in the inner tubular member 4. When O-ring 15 is seated in the groove 16, a clearance is provided between the outer edge of O-ring 15 and the adjacent wall defining annular space 10. In this manner, the fluid under pressure entering annular space 10 to passage 13 passes around O-ring 15 and enters passage 11 to flow into the pressure chamber 12. A specific clearance is maintained around O-ring 15 so as to permit a predetermined flow rate to the pressure chamber 12.
  • the O-ring 15 When a surge of fluid pressure enters through passage 13, the O-ring 15 is immediately distorted or moved upwardly against O-ring 15 so as to close the entrance to passage 11 in the inner tubular member as shown in FIG. 3. Upon decay of this surge in pressure, the O-ring will revert to its original position as shown in FIG. 2 and will permit the flow of fluid into the passage 11.
  • the O-ring 16 When the O-ring 16 is in the closed or blocking position, it becomes a selfenergizing seal for the duration of this surge in pressure. Most surges in pressure are relatively short in nature so that the O-ring will almost immediately revert to its original position.
  • the present invention discloses a surge cut-01f device which prevents actuation of pressure sensing units by momentary surges or pressure waves in fluid pressure systems while permitting actuation of pressure sensing units by normal changes in pressure.
  • An outstanding advantage of the present invention is its simplicity of structure and, as a result, its low cost due to ease of manufacture. Furthermore, the structure of this device has a considerable flexibility so as to adapt this device for a large number of different applications. Also, the device is insensitive to minor system contamination.
  • a surge cut-off device for fluid pressure sensing units comprising a housing having a pressure chamber therein and an annular space surrounding said pressure chamber, there being a conical surface at one end of said annular space, first passage means between said pressure chamber and said annular space and second passage means between said conical end of said annular space and the exterior of the housing for connection to a source of pressure, a resilient O-ring Within said annular space between said first and second passage means, there being a predetermined clearance between the outer surface of said O-ring and the adjacent surface of said annular space to permit a predetermined flow rate of fluid between said first and second passage means, at least a portion of said O-ring being movable to block said first passage means upon a surge of fiuid pressure in said second passage means, said housing comprising an outer tubular member having larger and smaller internal diameter portions with said conical surface interconnecting said two diameter portions, and an inner tubular member closed at one end and defining a pressure chamber having a first outer diameter portion corresponding to said smaller internal diameter portion and a second
  • a surge cut-01f device as claimed in claim 1 additionally including a groove in the first outer diameter portion of said inner tubular member, said O-ring being seated therein.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Measuring Fluid Pressure (AREA)

Description

J. J. RYAN Nov. 11, 1969 Filed Sept. 6, 1967 FROM PRESSURE SOURCE FIG-.2
United States Patent US. Cl. 137--517 4 Claims ABSTRACT OF THE DISCLOSURE A surge cut-0E device having a resilient O-ring positioned in an annular chamber communicating with a source of pressure and with a pressure chamber within the device and a predetermined clearance past the resilient O-ring so that a surge of fluid pressure will move the O-ring to block the passage communicating with the pressure chamber Within the device.
The present invention relates to a surge cut-off device for fluid pressure sensing units and more particularly to such a device employing a resilient O-ring which is distorted by surges in pressure to block the passage of thefluid under pressure.
The measurement of pressure in fluid systems has been carried out by many forms of gauges, regulators, differential indicators, and the like. These devices have been so highly developed that they can indicate accurately the pressure in the systems at all times. However, in many instances when the pressure changes in a system, the change is not gradual but is accompanied by a surge in pressure. Thus, for a brief instant the pressure surges to an extremely high value and just as rapidly decreases to the level of the pressure change. In many applications it is not necessary to determine the surge in pressure and, indeed, in some applications the pressure surges are undesirable and may adversely afiect the pressure indication. While various forms of surge cut-01f devices have been incorporated in pressure measuring devices, the cutoff devices generally are complex in structure and cumbersome in operation. Furthermore, these cut-ofi devices may add considerably to the cost of the pressure indicating device because of their complicated structures.
It is therefore an object of the present invention to provide an improved surge cut-off device for pressure sensing units.
Another object of the invention is to provide a surge cut-ofi device for fluid pressure systems wherein surges in pressure are blocked and kept from the pressure sensingunit while gradual increases in pressure are measured.
In one aspect of the invention, the surge cut-off device comprises a housing having a pressure chamber and an annular space surrounding the pressure chamber. One end of the annular space is provided with a conical surface and there are passage means between the pressure chamber and the annular space, and further passage means between the conical end of the annular space and the exterior of the housing for connection to a source of pressure. A resilient O-ring is positioned within the annular space between the two passage means. There is a predetermined clearance between the O-riug and a surface of the annular space so as to permit a predetermined flow rate of fluid between the first and second passages. The O-ring is of suflicient resiliency so as to be movable or distortable to block the passage between the annular space and the pressure chamber when a surge of fluid pressure is received in the annular chamber from the pressure source.
The housing may be made of two concentric tubular 3,477,464 Patented Nov. 11, 1969 members formed to define the annular space therebetween. The O-ring may be positioned in a shallow groove formed in the inner surface of the annular space.
Other objects, advantages and features of the invention will become apparent from the following description when taken in conjunction with the accompanying drawings, which, are merely exemplary.
In the drawings:
FIG. 1 is a longitudinal sectional view of the surge cut-off device of the present invention;
FIG. 2 is a portion of the view in FIG. 1 in enlarged scale and showing the position of the O-ring within the annular space between the two passages; and
FIG. 3 is a view similar to FIG. 2 but showing the O-ring in distorted position in response to a surge of pressure into the annular space.
Referring to the drawings wherein like reference symbols indicate the same parts throughout the various views, a specific embodiment of the invention will be described in detail.
As may be seen in FIG. 1, the surge cut-ofl? device is indicated generally at 1 and comprises a housing 2 formed of an outer tubular member 3 and an inner tubular member 4 which are fixed with respect to each other in the position shown in FIG. 1.
Outer tubular member 3 has a smaller internal diameter portion 5 and a larger internal diameter portion 6, the inner tubular member 4 having corresponding smaller diameter portion 7 and larger diameter portion 8. The two diameter portions 5 and 6 of the outer tubular member are interconnected by a conical surface 9. When the tubular members are positioned as shown in FIG. 1, there is defined therebetween an annular space 10.
An inclined passage 11 is formed in the inner tubular member to provide communication between the annular space 10 and a pressure chamber 12 located within the inner tubular member. A second passage 13 is provided in the outer tubular member to communicate between the conical portion of the annular space and the exterior of the cut-off device. The passage 13 is adapted for connection to a source of fluid pressure.
Positioned in annular space 10 are two resilient 0- rings 14 and 15 made of natural or synthetic rubber or a suitable plastic material. The O-ring 14 is positioned at the upper end of the annular space as viewed in FIG. 1 and is above the opening to passage 11. O-ring 15 is positioned in a shallow groove 16 formed in the inner tubular member 4. When O-ring 15 is seated in the groove 16, a clearance is provided between the outer edge of O-ring 15 and the adjacent wall defining annular space 10. In this manner, the fluid under pressure entering annular space 10 to passage 13 passes around O-ring 15 and enters passage 11 to flow into the pressure chamber 12. A specific clearance is maintained around O-ring 15 so as to permit a predetermined flow rate to the pressure chamber 12.
When a surge of fluid pressure enters through passage 13, the O-ring 15 is immediately distorted or moved upwardly against O-ring 15 so as to close the entrance to passage 11 in the inner tubular member as shown in FIG. 3. Upon decay of this surge in pressure, the O-ring will revert to its original position as shown in FIG. 2 and will permit the flow of fluid into the passage 11.
When the O-ring 16 is in the closed or blocking position, it becomes a selfenergizing seal for the duration of this surge in pressure. Most surges in pressure are relatively short in nature so that the O-ring will almost immediately revert to its original position.
Thus, it can be seen that the present invention discloses a surge cut-01f device which prevents actuation of pressure sensing units by momentary surges or pressure waves in fluid pressure systems while permitting actuation of pressure sensing units by normal changes in pressure. An outstanding advantage of the present invention is its simplicity of structure and, as a result, its low cost due to ease of manufacture. Furthermore, the structure of this device has a considerable flexibility so as to adapt this device for a large number of different applications. Also, the device is insensitive to minor system contamination.
What is claimed is:
1. A surge cut-off device for fluid pressure sensing units comprising a housing having a pressure chamber therein and an annular space surrounding said pressure chamber, there being a conical surface at one end of said annular space, first passage means between said pressure chamber and said annular space and second passage means between said conical end of said annular space and the exterior of the housing for connection to a source of pressure, a resilient O-ring Within said annular space between said first and second passage means, there being a predetermined clearance between the outer surface of said O-ring and the adjacent surface of said annular space to permit a predetermined flow rate of fluid between said first and second passage means, at least a portion of said O-ring being movable to block said first passage means upon a surge of fiuid pressure in said second passage means, said housing comprising an outer tubular member having larger and smaller internal diameter portions with said conical surface interconnecting said two diameter portions, and an inner tubular member closed at one end and defining a pressure chamber having a first outer diameter portion corresponding to said smaller internal diameter portion and a second outer diameter portion corresponding to said larger diameter portion, said annular space being defined between said inner and outer tubular members.
2. A surge cut-01f device as claimed in claim 1 additionally including a groove in the first outer diameter portion of said inner tubular member, said O-ring being seated therein.
3. A surge cut-off device as claimed in claim 1, further comprising a second resilient O-ring at the other end of said annular space and on the other side of said first passage means.
4. A surge cut-01f device as claimed in claim 1 wherein said first passage means is inclined away from said second passage means.
References Cited UNITED STATES PATENTS 2,703,558 3/1955 Wilcox 137525 X 3,122,352 2/1964- Anderson et a1. l37-525 X 3,216,451 11/1965 Smallpeice 137-5l7 X WILLIAM F. ODEA, Primary Examiner DAVID J. ZOBKIW, Assistant Examiner US. Cl. X.R.
US665910A 1967-09-06 1967-09-06 Surge cut-off device for pressure sensing units Expired - Lifetime US3477464A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US66591067A 1967-09-06 1967-09-06

Publications (1)

Publication Number Publication Date
US3477464A true US3477464A (en) 1969-11-11

Family

ID=24672055

Family Applications (1)

Application Number Title Priority Date Filing Date
US665910A Expired - Lifetime US3477464A (en) 1967-09-06 1967-09-06 Surge cut-off device for pressure sensing units

Country Status (1)

Country Link
US (1) US3477464A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3646906A (en) * 1968-02-01 1972-03-07 Purolator Products Inc Pressure indicator and surge control device
US3680594A (en) * 1970-06-12 1972-08-01 Mts System Corp Servovalve with accumulator means on drain cavities
US4480729A (en) * 1979-10-03 1984-11-06 P. L. Porter Company Anti-surge valve for hydraulic locking device
US4637000A (en) * 1985-06-21 1987-01-13 Western Geophysical Co. Of America Depth transducer protective assembly
US5284060A (en) * 1989-03-20 1994-02-08 Martinez Donald G Pressure/control gage
US6651698B1 (en) * 2002-05-31 2003-11-25 Wilkes & Mclean Ltd. Suppressor for manifold fluid line

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703558A (en) * 1951-08-30 1955-03-08 Modern Products Inc Pressure return cylinder and piston unit
US3122352A (en) * 1961-07-10 1964-02-25 Acf Ind Inc Spherical plug valve having pressurized seats including body pressure relief means
US3216451A (en) * 1963-10-07 1965-11-09 Martonair Ltd Annular sealing ring control valve

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2703558A (en) * 1951-08-30 1955-03-08 Modern Products Inc Pressure return cylinder and piston unit
US3122352A (en) * 1961-07-10 1964-02-25 Acf Ind Inc Spherical plug valve having pressurized seats including body pressure relief means
US3216451A (en) * 1963-10-07 1965-11-09 Martonair Ltd Annular sealing ring control valve

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3646906A (en) * 1968-02-01 1972-03-07 Purolator Products Inc Pressure indicator and surge control device
US3680594A (en) * 1970-06-12 1972-08-01 Mts System Corp Servovalve with accumulator means on drain cavities
US4480729A (en) * 1979-10-03 1984-11-06 P. L. Porter Company Anti-surge valve for hydraulic locking device
US4637000A (en) * 1985-06-21 1987-01-13 Western Geophysical Co. Of America Depth transducer protective assembly
US5284060A (en) * 1989-03-20 1994-02-08 Martinez Donald G Pressure/control gage
US6651698B1 (en) * 2002-05-31 2003-11-25 Wilkes & Mclean Ltd. Suppressor for manifold fluid line

Similar Documents

Publication Publication Date Title
US3131716A (en) Flow control valves
US2948296A (en) Variable constant flow device
US3742970A (en) Flow-sensitive sensing and shut-off device
EP3276311B1 (en) Balancing valve for adjusting the distribution of fluids in multiple pipes
GB2040406A (en) Flow-indicating check valves
US3633618A (en) Valved manifold for gauging a plurality of fluid pressures
US4254664A (en) Flow meters
US3759098A (en) Apparatus for determining fluid flow in a conduit
US2827008A (en) Flow indicator
US3477464A (en) Surge cut-off device for pressure sensing units
US3403556A (en) Flow measuring device
US4257452A (en) Biased open direct response valve with damping means
US3969923A (en) Leak detector
US3210987A (en) Pneumatic measuring circuit
US5549277A (en) Fluid flow controller and meter
US4424716A (en) Hydraulic flowmeter
US5827978A (en) Flow transducer
US3633612A (en) Flow indicator and valve
US3646906A (en) Pressure indicator and surge control device
CA1151893A (en) Device for detecting rate of change in pressure
US3037384A (en) Multi-range fluid flow measuring apparatus
US2583384A (en) Flow regulator
US2846871A (en) Air gage apparatus
US3799107A (en) Positive fluid flow indicator
US5458007A (en) Bi-directional flow indicator