US3005573A - Blowout diaphragm - Google Patents
Blowout diaphragm Download PDFInfo
- Publication number
- US3005573A US3005573A US845296A US84529659A US3005573A US 3005573 A US3005573 A US 3005573A US 845296 A US845296 A US 845296A US 84529659 A US84529659 A US 84529659A US 3005573 A US3005573 A US 3005573A
- Authority
- US
- United States
- Prior art keywords
- valve
- diaphragm
- thickness
- hemispherical
- rim
- 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
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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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K17/00—Safety valves; Equalising valves, e.g. pressure relief valves
- F16K17/02—Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side
- F16K17/14—Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side with fracturing member
- F16K17/16—Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side with fracturing member with fracturing diaphragm ; Rupture discs
- F16K17/162—Safety valves; Equalising valves, e.g. pressure relief valves opening on surplus pressure on one side; closing on insufficient pressure on one side with fracturing member with fracturing diaphragm ; Rupture discs of the non reverse-buckling-type
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
- G01M9/04—Details
Definitions
- This invention relates to a valve of the rupturable diaphragm type which is designed to open under a predetermined pressure and which cannot be closed or reused.
- An object of the present invention is to provide a valve of the rupturable diaphragm type which will open instantly from a completely closed position to a completely open position.
- Another object of the present invention is to provide a valve of the rupturable diaphragm type which will completely open at a calculable pressure and remain completely closed until it is subjected to that calculated pressure or a higher pressure.
- Still another object is the provision of a valve having a circular rim and formed with a central hemispherical rupturable diaphragm scored to open along certain predetermined lines, all of the scored sections being retained by the disc upon opening.
- a further object of the invention is the provision of scored sections which vary in thickness along the score mark to insure retention of all the parts of the valve when the valve opens.
- a still further object is the provision of a valve formed with a hemispherical diaphragm scored to be ruptured into spherical quadrants when subjected to a predetermined pressure, the thickness of the diaphragm at the lines of rupture being uniform, the thickness of the metal of the diaphragm varying from the center to the circumference to insure retention of all the parts after rupture.
- FIG. 1 is a perspective view of the valve closed
- FIG. 2 is a perspective view of the valve open
- FIG. 3 is a cross-sectional view along the score lines of a single quadrant.
- FIG. 4 is a plan view of a modification of the valve shown in FIG. 1.
- the diaphragm valve shown on FIG. 1 is hemispherical in shape with a heavy flat integral rim 10.
- the inner wall of the rim continues from the base of the hemisphere in cylindrical form so that the blast enters the hemisphere along a tangential line.
- the valve is stamped or otherwise formed into the hemispherical shape from a flat disc and scored with sections of great circle lines which cross at right angles toeach other and divide the hemispherical I portion into four equal spherical quadrants 12.
- the spherical quadrants When the diaphragm is ruptured the spherical quadrants must not be torn loose from the rim and must open fully so that no part of the quadrants is in the direct path of the blast. Should any part of the quadrants be in the path of the blast, disturbing air currents would be set up in the wind tunnel and the results of the test would not be accurate.
- the entire hemisphere is thicker adjacent the rim and decreases in thickness as it approaches the juncture 14 of the score lines 16.
- the thickness of the metal along the lines on which it is ruptured is the same at the rim as at the juncture of the score lines to make it possible to calculate the bursting pressure and to insure substantially instantaneous rupture, and this uniform thickness is shown at 18.
- FIG. 4 illustrates a modified form of the hemispherical valve.
- the valve shown in this figure is pyramid shaped with a square rim 22.
- the triangular sides 30 of the pyramid are formed similar to the spherical quadrants 12, the metal varying in thickness from the base to the apex.
- the triangular shaped sides open similarly to the quadrants of FIG. 2. This type is generally used with lower pressures and smaller wind tunnels.
- a rupturable diaphragm valve comprising a hemispherical body portion of a decreasing thickness and tapering uniformly from the base to the dome, said body portion being divided into segments by score lines of decreasing depth, said score lines decreasing in depth from the base to a common juncture at the dome, the body portion remaining along said score lines being of body portion, said wall being an extension of the inner 7 Wall of the hemispherical body portion at its base, said 5 rim being of a thickness greater than the hemispherical body portion at its greatest thickness.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Safety Valves (AREA)
Description
Oct 1961 v. c. D. DAWSON ETAL 3,005,573
BLOWOUT DIAPHRAGM Filed 001;. 8, 1959 F161. FICA.
VICTOR C.D. DAWSON ARNOLD E. SEIGEL Momma,
INVENTORS United States Patent 0 3,005,573 BLOWOUT DIAPHRAGM Victor C. D. Dawson, Silver Spring, and Arnold E. Seigel,
Chevy Chase, Md, assignors to the United States of America as represented by the Secretary of the Navy Filed Oct. 8, 1959, Ser. No. 845,296 2 Claims. (Cl. 220-89) (Granted under Title 35, U.S. Code (1952), see. 266) The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
This invention relates to a valve of the rupturable diaphragm type which is designed to open under a predetermined pressure and which cannot be closed or reused.
In the study of aerodynamic forces at supersonic speeds, it is the practice to suspend models in a wind tunnel and pass air at very high velocity past the models, taking pictures at the instant the model is bufieted by the air or gaseous medium. One method of obtaining the velocity of gas desired is to explode a mixture of gases in a gun barrel and by means of a rupturable diaphragm type valve admit the explosive gases into the tunnel. In order to be sure the velocity of the gases are as desired, a valve which will change from completely closed to completely open instantly is needed. Also the parts of the valve must not set up currents in the onrushing air which would be different from that encountered by a missile in flight. The valve must be rugged to withstand the high velocity gases passing from the explosive chamber to the wind tunnel and must be designed with no parts which might tear loose so that no solid particles enter the wind tunnel with the onrushing gases.
An object of the present invention is to provide a valve of the rupturable diaphragm type which will open instantly from a completely closed position to a completely open position.
Another object of the present invention is to provide a valve of the rupturable diaphragm type which will completely open at a calculable pressure and remain completely closed until it is subjected to that calculated pressure or a higher pressure.
Still another object is the provision of a valve having a circular rim and formed with a central hemispherical rupturable diaphragm scored to open along certain predetermined lines, all of the scored sections being retained by the disc upon opening.
A further object of the invention is the provision of scored sections which vary in thickness along the score mark to insure retention of all the parts of the valve when the valve opens.
A still further object is the provision of a valve formed with a hemispherical diaphragm scored to be ruptured into spherical quadrants when subjected to a predetermined pressure, the thickness of the diaphragm at the lines of rupture being uniform, the thickness of the metal of the diaphragm varying from the center to the circumference to insure retention of all the parts after rupture.
Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawing wherein:
FIG. 1 is a perspective view of the valve closed;
FIG. 2 is a perspective view of the valve open;
FIG. 3 is a cross-sectional view along the score lines of a single quadrant; and
FIG. 4 is a plan view of a modification of the valve shown in FIG. 1.
Referring to the drawing wherein like parts are designated by like numerals throughout the several figures, the diaphragm valve shown on FIG. 1 is hemispherical in shape with a heavy flat integral rim 10. The inner wall of the rim continues from the base of the hemisphere in cylindrical form so that the blast enters the hemisphere along a tangential line. The valve is stamped or otherwise formed into the hemispherical shape from a flat disc and scored with sections of great circle lines which cross at right angles toeach other and divide the hemispherical I portion into four equal spherical quadrants 12.
When the diaphragm is ruptured the spherical quadrants must not be torn loose from the rim and must open fully so that no part of the quadrants is in the direct path of the blast. Should any part of the quadrants be in the path of the blast, disturbing air currents would be set up in the wind tunnel and the results of the test would not be accurate. The entire hemisphere is thicker adjacent the rim and decreases in thickness as it approaches the juncture 14 of the score lines 16. The thickness of the metal along the lines on which it is ruptured is the same at the rim as at the juncture of the score lines to make it possible to calculate the bursting pressure and to insure substantially instantaneous rupture, and this uniform thickness is shown at 18. The difference in thickness is clearly shown in the depth of the score lines, being deeper at 20 adjacent the rim than at 14-, the juncture of the score lines. This carefully designed rupturable diaphragm will assume the position shown in dashed outline in FIG. 3 when subjected to a pressure of approximately 60,000 psi, from any suitable source such as, for example, a gas gun. The valve is used between an explosion chamber and a wind tunnel. A mixture of gases under pressures approximately 8,000 psi are ignited and the resultant explosion ruptures the diaphragm as shown in FIG. 2, to permit the gas to enter the wind tunnel.
FIG. 4 illustrates a modified form of the hemispherical valve. The valve shown in this figure is pyramid shaped with a square rim 22. The triangular sides 30 of the pyramid are formed similar to the spherical quadrants 12, the metal varying in thickness from the base to the apex. The triangular shaped sides open similarly to the quadrants of FIG. 2. This type is generally used with lower pressures and smaller wind tunnels.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed as new and desired to be secured by Letters Patent of the United States is:
1. A rupturable diaphragm valve comprising a hemispherical body portion of a decreasing thickness and tapering uniformly from the base to the dome, said body portion being divided into segments by score lines of decreasing depth, said score lines decreasing in depth from the base to a common juncture at the dome, the body portion remaining along said score lines being of body portion, said wall being an extension of the inner 7 Wall of the hemispherical body portion at its base, said 5 rim being of a thickness greater than the hemispherical body portion at its greatest thickness.
2. A rupturable diaphragm valve according to claim 1 wherein the score lines divide the hemispherical body portion into quadrants.
UNITED STATES PATENTS Greengrass Sept. 14, 1897 Killen Oct. 4, 1938 Cofirnan Oct. 27, 1953 Paxton et al Sept. 13, 1960 FOREIGN PATENTS Great Britain May 15, 1957
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US845296A US3005573A (en) | 1959-10-08 | 1959-10-08 | Blowout diaphragm |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US845296A US3005573A (en) | 1959-10-08 | 1959-10-08 | Blowout diaphragm |
Publications (1)
Publication Number | Publication Date |
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US3005573A true US3005573A (en) | 1961-10-24 |
Family
ID=25294897
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US845296A Expired - Lifetime US3005573A (en) | 1959-10-08 | 1959-10-08 | Blowout diaphragm |
Country Status (1)
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US (1) | US3005573A (en) |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3109553A (en) * | 1961-07-17 | 1963-11-05 | Fike Metal Prod Corp | Rupture disc unit |
US3116747A (en) * | 1961-06-05 | 1964-01-07 | Torrington Co | Unitary rupturable check valve |
US3195769A (en) * | 1961-08-31 | 1965-07-20 | Gerald A Miller | Burst diaphragm and method of making same |
US3257026A (en) * | 1964-07-17 | 1966-06-21 | Taylor Glenn | High pressure quick opening valve |
US3272381A (en) * | 1964-03-25 | 1966-09-13 | Continental Can Co | Can end for easy opening beverage cans |
US3356257A (en) * | 1965-09-16 | 1967-12-05 | Midwest Consultants Inc | Safety plug for pressure vessels |
US3363801A (en) * | 1965-12-20 | 1968-01-16 | Fike Metal Prod Corp | Rupture disc assembly |
DE1261365B (en) * | 1964-05-02 | 1968-02-15 | Karl Erb Dipl Ing | Foil safety valve |
US3463351A (en) * | 1967-02-06 | 1969-08-26 | Black Sivalls & Bryson Inc | Safety pressure relief device |
US3484817A (en) * | 1967-11-07 | 1969-12-16 | Black Swalls & Bryson Inc | Safety pressure relief device |
US3834580A (en) * | 1972-09-25 | 1974-09-10 | Black Sivalls & Bryson Inc | Safety pressure relief device |
FR2538494A1 (en) * | 1982-12-27 | 1984-06-29 | Bs & B Safety Systems Ltd | RECESSED BREAK DISC DEVICE |
US4498368A (en) * | 1983-10-06 | 1985-02-12 | The United States Of America As Representedby The Secretary Of The Navy | Frangible fly through diaphragm for missile launch canister |
US4597505A (en) * | 1984-04-09 | 1986-07-01 | Continental Disc Corporation | Rupture disc with selectively positioned initial buckling |
US4669626A (en) * | 1983-09-20 | 1987-06-02 | Continental Disc Corporation | Rupture disc with selectively positioned initial buckling |
US4745521A (en) * | 1985-10-31 | 1988-05-17 | Icotron S.A. Industria De Componentes Electronicos | Explosion proof safety valve for a condenser |
US4759460A (en) * | 1983-09-20 | 1988-07-26 | Continental Disc Corporation | Rupture disc system |
US4787180A (en) * | 1988-01-29 | 1988-11-29 | Bs&B Safety Systems, Inc. | Vibration resistant rupturable pressure relief member |
US4795051A (en) * | 1982-05-24 | 1989-01-03 | Rs&B Safety Systems, Inc. | Rupturable fluid pressure relief apparatus and manufacturing method |
US4838447A (en) * | 1987-06-29 | 1989-06-13 | Bs&B Safety Systems, Inc. | Pressure relief device with conical reverse buckling disc |
EP0442199A2 (en) * | 1990-02-12 | 1991-08-21 | BS & B SAFETY SYSTEMS, INC. | Low pressure non-fragmenting rupture disks |
WO2012149612A1 (en) * | 2011-05-02 | 2012-11-08 | Dispack-Projects Nv | Fixation of a fitting on a container |
CN104634197A (en) * | 2013-11-08 | 2015-05-20 | 北京天高智机技术开发公司 | Rupture membrane |
WO2018035372A1 (en) * | 2016-08-19 | 2018-02-22 | Continental Disc Corporation | Inlet support structure for a tension acting rupture disc |
CN110701415A (en) * | 2019-11-13 | 2020-01-17 | 中水北方勘测设计研究有限责任公司 | Water passing device capable of keeping flow stable |
US11156417B2 (en) * | 2017-02-02 | 2021-10-26 | Nexter Systems | Cap for duct for ejecting cartridges and turret including a duct for ejecting cartridges obturated by such a cap |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US589944A (en) * | 1897-09-14 | Safety | ||
US2131809A (en) * | 1935-01-26 | 1938-10-04 | Dan J Killen | Valve |
US2656950A (en) * | 1950-08-23 | 1953-10-27 | Black Sivalls & Bryson Inc | Safety pressure device |
GB774812A (en) * | 1954-08-30 | 1957-05-15 | Johnson Matthey Co Ltd | Improvements in and relating to vacuum supports for pressure releasing devices |
US2952383A (en) * | 1959-09-04 | 1960-09-13 | Pure Carbon Company Inc | Carbon rupture disk |
-
1959
- 1959-10-08 US US845296A patent/US3005573A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US589944A (en) * | 1897-09-14 | Safety | ||
US2131809A (en) * | 1935-01-26 | 1938-10-04 | Dan J Killen | Valve |
US2656950A (en) * | 1950-08-23 | 1953-10-27 | Black Sivalls & Bryson Inc | Safety pressure device |
GB774812A (en) * | 1954-08-30 | 1957-05-15 | Johnson Matthey Co Ltd | Improvements in and relating to vacuum supports for pressure releasing devices |
US2952383A (en) * | 1959-09-04 | 1960-09-13 | Pure Carbon Company Inc | Carbon rupture disk |
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3116747A (en) * | 1961-06-05 | 1964-01-07 | Torrington Co | Unitary rupturable check valve |
US3109553A (en) * | 1961-07-17 | 1963-11-05 | Fike Metal Prod Corp | Rupture disc unit |
US3195769A (en) * | 1961-08-31 | 1965-07-20 | Gerald A Miller | Burst diaphragm and method of making same |
US3272381A (en) * | 1964-03-25 | 1966-09-13 | Continental Can Co | Can end for easy opening beverage cans |
DE1261365B (en) * | 1964-05-02 | 1968-02-15 | Karl Erb Dipl Ing | Foil safety valve |
US3257026A (en) * | 1964-07-17 | 1966-06-21 | Taylor Glenn | High pressure quick opening valve |
US3356257A (en) * | 1965-09-16 | 1967-12-05 | Midwest Consultants Inc | Safety plug for pressure vessels |
US3363801A (en) * | 1965-12-20 | 1968-01-16 | Fike Metal Prod Corp | Rupture disc assembly |
US3463351A (en) * | 1967-02-06 | 1969-08-26 | Black Sivalls & Bryson Inc | Safety pressure relief device |
US3484817A (en) * | 1967-11-07 | 1969-12-16 | Black Swalls & Bryson Inc | Safety pressure relief device |
US3834580A (en) * | 1972-09-25 | 1974-09-10 | Black Sivalls & Bryson Inc | Safety pressure relief device |
US4795051A (en) * | 1982-05-24 | 1989-01-03 | Rs&B Safety Systems, Inc. | Rupturable fluid pressure relief apparatus and manufacturing method |
FR2538494A1 (en) * | 1982-12-27 | 1984-06-29 | Bs & B Safety Systems Ltd | RECESSED BREAK DISC DEVICE |
US4669626A (en) * | 1983-09-20 | 1987-06-02 | Continental Disc Corporation | Rupture disc with selectively positioned initial buckling |
US4759460A (en) * | 1983-09-20 | 1988-07-26 | Continental Disc Corporation | Rupture disc system |
US4498368A (en) * | 1983-10-06 | 1985-02-12 | The United States Of America As Representedby The Secretary Of The Navy | Frangible fly through diaphragm for missile launch canister |
US4597505A (en) * | 1984-04-09 | 1986-07-01 | Continental Disc Corporation | Rupture disc with selectively positioned initial buckling |
US4745521A (en) * | 1985-10-31 | 1988-05-17 | Icotron S.A. Industria De Componentes Electronicos | Explosion proof safety valve for a condenser |
US4838447A (en) * | 1987-06-29 | 1989-06-13 | Bs&B Safety Systems, Inc. | Pressure relief device with conical reverse buckling disc |
US4787180A (en) * | 1988-01-29 | 1988-11-29 | Bs&B Safety Systems, Inc. | Vibration resistant rupturable pressure relief member |
EP0442199A2 (en) * | 1990-02-12 | 1991-08-21 | BS & B SAFETY SYSTEMS, INC. | Low pressure non-fragmenting rupture disks |
EP0442199A3 (en) * | 1990-02-12 | 1992-01-02 | Bs & B Safety Systems, Inc. | Low pressure non-fragmenting rupture disks |
WO2012149612A1 (en) * | 2011-05-02 | 2012-11-08 | Dispack-Projects Nv | Fixation of a fitting on a container |
CN104634197A (en) * | 2013-11-08 | 2015-05-20 | 北京天高智机技术开发公司 | Rupture membrane |
WO2018035372A1 (en) * | 2016-08-19 | 2018-02-22 | Continental Disc Corporation | Inlet support structure for a tension acting rupture disc |
US10100942B2 (en) * | 2016-08-19 | 2018-10-16 | Continental Disc Corporation | Inlet support structure for a tension acting rupture disc |
US11156417B2 (en) * | 2017-02-02 | 2021-10-26 | Nexter Systems | Cap for duct for ejecting cartridges and turret including a duct for ejecting cartridges obturated by such a cap |
CN110701415A (en) * | 2019-11-13 | 2020-01-17 | 中水北方勘测设计研究有限责任公司 | Water passing device capable of keeping flow stable |
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