US3202162A - Normally-closed explosive-actuated valve - Google Patents

Normally-closed explosive-actuated valve Download PDF

Info

Publication number
US3202162A
US3202162A US249953A US24995363A US3202162A US 3202162 A US3202162 A US 3202162A US 249953 A US249953 A US 249953A US 24995363 A US24995363 A US 24995363A US 3202162 A US3202162 A US 3202162A
Authority
US
United States
Prior art keywords
ram
valve body
nipple
recess
port
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
US249953A
Inventor
Hans F Eckardt
John L Marsh
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US249953A priority Critical patent/US3202162A/en
Application granted granted Critical
Publication of US3202162A publication Critical patent/US3202162A/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
    • F16K13/00Other constructional types of cut-off apparatus; Arrangements for cutting-off
    • F16K13/04Other constructional types of cut-off apparatus; Arrangements for cutting-off with a breakable closure member
    • F16K13/06Other constructional types of cut-off apparatus; Arrangements for cutting-off with a breakable closure member constructed to be ruptured by an explosion
    • 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
    • Y10T137/1624Destructible or deformable element controlled
    • Y10T137/1632Destructible element
    • Y10T137/1647Explosive actuation

Definitions

  • An object of the present invention is to provide an explosive-actuated valve which is simple and economical to manufacture yet is highly reliable, effective and eflicient in operation.
  • a further object is to provide an explosive-actuated valve which positively prevents any flow prior to actuation, yet permits unrestricted and turbulence-free straightthrough flow subsequent to actuation.
  • Another object of the invention is to provide an explosive-actuated valve incorporating a combination energyabsorbing and seal or isolation means adapted not only to retard movement of the ram subsequent to the explosion but also to prevent products of the explosion from entering the controlled fluid.
  • Another object of the invention is to provide a valve incorporating a blind nipple element which prevents the pressure of the controlled fluid from entering the explosive element prior to actuation, and which prevents the controlled fluid from causing hydraulic lock prior to actuation.
  • An additional object of the invention is to provide an explosive-actuated valve incorporating means effective to prevent the sheared nipple portion from entering the fluid stream, and to prevent chips and contaminants from entering the fluid stream.
  • FIGURE 1 is a longitudinal sectional view illustrating an explosive-actuated valve constructed in accordance with the present invention
  • FIGURE 2 is a transverse section taken on line 2-2 of FIGURE 1;
  • FIGURE 3 is a longitudinal section corresponding to FIGURE 1 but illustrating the parts in the positions assumed subsequent to actuation;
  • FIGURE 4 is a longitudinal section of a second embodiment wherein both threaded fittings for the fluid conduits are machined integral with the valve body, and wherein the nipple is suitably pressed, shrunk or taperfitted in position.
  • the explosive-actuated valve may be seen to comprise an elongated hollow body 14 an elon gated ram 11 mounted coaxially in body for longitudinal movement therein, and a nipple element 12 having a portion adapted to be sheared ofi' upon movement of the ram longitudinally of the body.
  • Means are provided to create a straight-through flow path for the controlled fluid in response to shearing of nipple 12 subsequent to igniting of the explosive actuator or squib which is indicated at 14.
  • such means includes energy absorbing, stop and sealing portions which perform various functions including pre- 3,262,162 Patented Aug. 24, 1965 vention of contamination. of the controlled fluid by the products of the explosion.
  • the hollow body 10 is closed at one end by a wall 16 and is open and internally threaded at the other end to threadedly receive the explosive actuator or squib 14.
  • One portion 17 of the valve chamber within body 10, adjacent end wall 16, is cylindrical and relatively small in diameter.
  • Chamber portions 17 and 18 are axially spaced from each other and are connected by a tapered or frustoconical portion 19 the wall of which forms part of the energy-absorbing means indicated above, being adapted to absorb energy from ram 11 and also to create a seal.
  • the ram 11 incorporates portions shaped to conform, except as will be described subsequently, to the walls of the smaller-diameter and tapered chamber portions 17 and 19.
  • the ram also includes, relatively adjacent the squib 14-, a short cylindrical portion which corresponds in diameter to chamber portion 18.
  • Such larger-diameter ram portion is provided with an O-ring seal 21 which slides sealingly on the wall of chamber portion 18 to create an initial seal preventing contamination of the controlled fluid by propellant gases.
  • the inner end of ram 11, in chamber portion 17, is machined flat to provide a surface 22 lying in a plane parallel to the ram axis and spaced a short distance thereabove.
  • the ram portion relatively adjacent end wall 16 is formed with a cylindrical recess 23 the axis of which is perpendicular to fiat surface 22 and intersects the ram axis.
  • a port or passage 24 is formed through the flattened ram portion a short distance from recess 23, such port being cylindrical and having an axis which is perpendicular to surface 22 and intersects the axis of the ram.
  • the port or passage 24 forms a part of the previously-indicated means for creating the straight-through fluid flow path in response to shearing of the end of nipple element 12.
  • Nipple element 12 is shown in FIGURES 1 and 2 as being suitably threaded into body it in such manner that its axis intersects that of ram 11.
  • the outer portion of the nipple element, which forms the inlet to the valve, is shown as being suitably threaded to receive a connector conduit (not shown).
  • the valve inlet (and also the valve outlet) may be constructed as a flared tube fitting, flareless tube fitting, internally-threaded boss, internally or externally-threaded pipe thread or manifold, etc.
  • a wrench-hold portion 26 is formed on the nipple and is adapted to seat on an O-ring 27, the latter being suitably seated in the valve body around the nipple for prevention of leakage from the valve chamber.
  • nipple 12 comprises a relatively thickwalled tubular portion 28 extending to the plane of flat surface 22, and a coaxial and relatively thin-Walled tubular portion 29 disposed in recess 23 and having a closed or blind end wall 31.
  • An external shoulder or stress riser 32 is formed at the junction of the thick-walled and thinwalled tubular portions 28 and 29, in the plane of flat surface 22., and performs important functions to be described hereinafter.
  • the valve body 10 is formed integrally with an outlet portion 33 which may correspond to the outer portion of nipple 12. It is emphasized that outlet portion 33 is formed with a straight passage which is coaxial with the passage or chamber in nipple 12, and has the same diameter.
  • the port or passage 24 through ram 11 also has the same diameter, so that subsequent to actuation of the valve (FIGURE 3) these three passages will combine to create a single unrestricted straight-through flow passage between the valve inlet and valve outlet.
  • the explosive element or squib 14 may be of any suitable construction known to the art, and may contain a solid propellant such as is used in rocketry.
  • the explosive may be electrically or mechanically ignited.
  • a suitable O-ring 34 is provided to prevent leakage of gas around the squib 14.
  • the distance between the axis of recess 23 and that of port or passage 24 corresponds to the distance between the end wall 16 and the inner end of ram 10, so that port 24 will be precisely aligned with the inlet and outlet passages subsequent to actuation (FIGURE 3).
  • This distance is substantially greater, however, than the distance between the tapered portion of ram 11 and the wall of tapered portion 19 of the valve chamber. It follows that substantially before the inner end of the ram contacts the wall 16, the tapered portion of the ram will engage the tapered wall of the valve chamber to commence dissipation of the energy created by the explosion. The ram is then deformed into such shape that it creates a secondary seal preventing leakage of gases to the flow path. Such deformation is facilitated by the presence of an axial bore 36 formed in the outer end of the ram.
  • valve is readily assembled by merely inserting the ram 11 into the valve chamber and so positioning the ram that recess 23 is opposite and coaxial with the internally-threaded valve-body opening for nipple 12.
  • Nipple 12 is then threadedly inserted into the valve body, in such manner that its inner end portion 29 enters the recess 23 as shown in FIGURES 1 and 2.
  • Assembly is then completed by threading the squib 14 into the open end of the valve body. Suitable conduits are then connected to the outer portion of nipple 12 and to valve outlet 33.
  • nipple 12 Since the nipple 12 is blind and is of integral construction, there is no possibility of leakage from the valve inlet to the outlet 33, to squib 14 or to the small-diameter portion 17 of the valve chamber. This eliminates all possibility of interaction between the controlled fluid and the explosive, and also eliminates the possibility of hydraulic lock due to the presence of controlled fluid in the valve chamber.
  • the engagement between the tapered portions of the valve body and ram provides a secondary seal which is highly effective to prevent gases from entering the controlled fluid after the gas pressure between the ram and the squib becomes so great that O-ring 21 is no longer effective to prevent leakage.
  • FIGURE 4 EMBQDIMENT OF FIGURE 4
  • the embodiment of FIGURE 4 is identical with that of FIGURES 1-3, except as will be described subsequently.
  • Corresponding reference numerals have been employed to denote corresponding parts, certain reference numerals in FIGURE 4 being followed by the letter a.
  • the threaded fitting for the inlet conduit is machined integral with the valve body 1%, as shown at 37.
  • the nipple 12a is then pressed, shrunk or taper-fitted into the portion 37 of the valve body and in such manner that its blind inner end enters the recess 23 as in the case of the previous embodiment.
  • an annular groove 33 is provided in the inner end portion of the nipple, at flat surface of the ram. Such groove augments the action of the stress riser in insuring a clean fracture of the nipple.
  • the present invention may also be incorporated in a tandem valve having two or more sets of inlet and outlet passages in axial alignment (respectively) with each other.
  • the ram incorporates a recess 23 and port 24 for each coaxial set of inlet and outlet passages.
  • the valve body and the ram incorporate cooperating tapered portions not only between the single squib and the adjacent coaxial valve passages but also between adjacent sets of coaxial passages. Such tapered portions between the adjacent sets of coaxial valve passages serve to isolate the controlled fluids from each other, in addition to absorbing the energy created by the explosion. Suitable O-rings may also be provided between adjacent sets of valve passages.
  • a normally-closed explosive-actuated valve comprising an elongated hollow valve body having a closed end and an open end, the interior wall of said body be- 1ng a relatively small-diameter cylinder adjacent said closed end and a relatively large-diameter cylinder adjacent said open end, said large-diameter and small-diameter cylindrical walls being axially spaced from each other and being connected by a frustoconical wall, an elongated one-piece ram mounted axially of said valve body for longitudinal movement therein, said ram-having an inner portion which is disposed radially-inwardly of said small-diameter cylindrical wall when the valve is in open condition, positive stop means provided in said valve body to stop movement of said ram at a predetermined point relatively adjacent said closed end, said ram also having a tapered portion corresponding generally to said frustoconical wall of said valve body and disposed to come into forceful engagement therewith prior to engagement of said ram with said positive stop means, said inner portion
  • sealing means are provided in the outer end portion of said ram between said squib and said tapered portion of said ram.
  • a normally-closed explosive-actuated valve comprising an elongated hollow valve body having a closed end and an open end, the valve chamber defined by said body having a relatively small-diameter cylindrical wall adjacent said closed end and a relatively large-diameter cylindrical wall adjacent said open end, said cylindrical walls being coaxial, said large-diameter and small-diameter walls being axially spaced from each other and being connected by frustoconical wall, an elongated one-piece ram mounted axially of said valve body for longitudinal movement therein, positive stop means provided in said valve body to stop movement of said ram at a predetermined point relatively adjacent said closed end, said ram having a tapered portion corresponding generally to said frustoconical wall of ,said valve body and disposed to come into forceful engagement theerwith prior to engagement of said ram with said positive stop means, said ram also having an inner portion which is disposed radiallyinwardly of said small-diameter cylindrical wall when the'valve is in open

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Safety Valves (AREA)

Description

H. F. ECKARDT ETAL 3,202,162
NORMALLY-CLOSED EXPLOSIVE-ACTUATED VALVE Aug. 24, 1965 Original Filed May 9, 1960 67 I J 2] Q6 l J9 5] 10 34 K 54 I j JGH/V 4. M425 1 INVENTORS.
ATTOPA/E'K Hans F. Eclrardt, 18161 Allegheny Drive,
United States Patent Oflfice 3,202,162 NORMALLY-'CL'0SED EXPLQSIVE-ACTUATED VALVE Santa Ana, 628 Arbolado Drive, Fuller- May 9, 249,953
Calif and John L. Marsh, ton, Calif. Continuation of application Ser. No. 27,870, 1960. This application Jan. 7,1963, Ser. No.
Claims. (Cl. 137-68) This invention relates to an explosive-actuated valve of the normally-closed type. This application is a continuation of our co-pending patent application Serial Number 27,870, filed May 9, 1960, for Normally-Closed Explosive- Actuated Valve, and since abandoned.
An object of the present invention is to provide an explosive-actuated valve which is simple and economical to manufacture yet is highly reliable, effective and eflicient in operation.
A further object is to provide an explosive-actuated valve which positively prevents any flow prior to actuation, yet permits unrestricted and turbulence-free straightthrough flow subsequent to actuation.
Another object of the invention is to provide an explosive-actuated valve incorporating a combination energyabsorbing and seal or isolation means adapted not only to retard movement of the ram subsequent to the explosion but also to prevent products of the explosion from entering the controlled fluid.
Another object of the invention is to provide a valve incorporating a blind nipple element which prevents the pressure of the controlled fluid from entering the explosive element prior to actuation, and which prevents the controlled fluid from causing hydraulic lock prior to actuation.
An additional object of the invention is to provide an explosive-actuated valve incorporating means effective to prevent the sheared nipple portion from entering the fluid stream, and to prevent chips and contaminants from entering the fluid stream.
These and other objects and advantages of the invention will be more fully set forth in the following specification and claims, considered in connection with the attached drawing to which they relate.
In the drawing:
FIGURE 1 is a longitudinal sectional view illustrating an explosive-actuated valve constructed in accordance with the present invention;
FIGURE 2 is a transverse section taken on line 2-2 of FIGURE 1;
FIGURE 3 is a longitudinal section corresponding to FIGURE 1 but illustrating the parts in the positions assumed subsequent to actuation; and
FIGURE 4 is a longitudinal section of a second embodiment wherein both threaded fittings for the fluid conduits are machined integral with the valve body, and wherein the nipple is suitably pressed, shrunk or taperfitted in position.
Referring first to the embodiment shown in FIGURES 1-3 of the drawing, the explosive-actuated valve may be seen to comprise an elongated hollow body 14 an elon gated ram 11 mounted coaxially in body for longitudinal movement therein, and a nipple element 12 having a portion adapted to be sheared ofi' upon movement of the ram longitudinally of the body. Means are provided to create a straight-through flow path for the controlled fluid in response to shearing of nipple 12 subsequent to igniting of the explosive actuator or squib which is indicated at 14. As will be described in detail subsequently, such means includes energy absorbing, stop and sealing portions which perform various functions including pre- 3,262,162 Patented Aug. 24, 1965 vention of contamination. of the controlled fluid by the products of the explosion. i
The hollow body 10 is closed at one end by a wall 16 and is open and internally threaded at the other end to threadedly receive the explosive actuator or squib 14. One portion 17 of the valve chamber within body 10, adjacent end wall 16, is cylindrical and relatively small in diameter. Another and coaxial chamber portion, numbered 18 and located adjacent squib 14, is also cylindrical but has a somewhat larger diameter. Chamber portions 17 and 18 are axially spaced from each other and are connected by a tapered or frustoconical portion 19 the wall of which forms part of the energy-absorbing means indicated above, being adapted to absorb energy from ram 11 and also to create a seal.
The ram 11 incorporates portions shaped to conform, except as will be described subsequently, to the walls of the smaller-diameter and tapered chamber portions 17 and 19. The ram also includes, relatively adjacent the squib 14-, a short cylindrical portion which corresponds in diameter to chamber portion 18. Such larger-diameter ram portion is provided with an O-ring seal 21 which slides sealingly on the wall of chamber portion 18 to create an initial seal preventing contamination of the controlled fluid by propellant gases.
The inner end of ram 11, in chamber portion 17, is machined flat to provide a surface 22 lying in a plane parallel to the ram axis and spaced a short distance thereabove. The ram portion relatively adjacent end wall 16 is formed with a cylindrical recess 23 the axis of which is perpendicular to fiat surface 22 and intersects the ram axis. A port or passage 24 is formed through the flattened ram portion a short distance from recess 23, such port being cylindrical and having an axis which is perpendicular to surface 22 and intersects the axis of the ram. The port or passage 24 forms a part of the previously-indicated means for creating the straight-through fluid flow path in response to shearing of the end of nipple element 12.
Nipple element 12 is shown in FIGURES 1 and 2 as being suitably threaded into body it in such manner that its axis intersects that of ram 11. The outer portion of the nipple element, which forms the inlet to the valve, is shown as being suitably threaded to receive a connector conduit (not shown). It is to be understood that the valve inlet (and also the valve outlet) may be constructed as a flared tube fitting, flareless tube fitting, internally-threaded boss, internally or externally-threaded pipe thread or manifold, etc. A wrench-hold portion 26 is formed on the nipple and is adapted to seat on an O-ring 27, the latter being suitably seated in the valve body around the nipple for prevention of leakage from the valve chamber.
The inner end of nipple 12 comprises a relatively thickwalled tubular portion 28 extending to the plane of flat surface 22, and a coaxial and relatively thin-Walled tubular portion 29 disposed in recess 23 and having a closed or blind end wall 31. An external shoulder or stress riser 32 is formed at the junction of the thick-walled and thinwalled tubular portions 28 and 29, in the plane of flat surface 22., and performs important functions to be described hereinafter. The valve body 10 is formed integrally with an outlet portion 33 which may correspond to the outer portion of nipple 12. It is emphasized that outlet portion 33 is formed with a straight passage which is coaxial with the passage or chamber in nipple 12, and has the same diameter. The port or passage 24 through ram 11 also has the same diameter, so that subsequent to actuation of the valve (FIGURE 3) these three passages will combine to create a single unrestricted straight-through flow passage between the valve inlet and valve outlet.
The explosive element or squib 14 may be of any suitable construction known to the art, and may contain a solid propellant such as is used in rocketry. The explosive may be electrically or mechanically ignited. A suitable O-ring 34 is provided to prevent leakage of gas around the squib 14.
The distance between the axis of recess 23 and that of port or passage 24 corresponds to the distance between the end wall 16 and the inner end of ram 10, so that port 24 will be precisely aligned with the inlet and outlet passages subsequent to actuation (FIGURE 3). This distance is substantially greater, however, than the distance between the tapered portion of ram 11 and the wall of tapered portion 19 of the valve chamber. It follows that substantially before the inner end of the ram contacts the wall 16, the tapered portion of the ram will engage the tapered wall of the valve chamber to commence dissipation of the energy created by the explosion. The ram is then deformed into such shape that it creates a secondary seal preventing leakage of gases to the flow path. Such deformation is facilitated by the presence of an axial bore 36 formed in the outer end of the ram.
OPERATION The valve is readily assembled by merely inserting the ram 11 into the valve chamber and so positioning the ram that recess 23 is opposite and coaxial with the internally-threaded valve-body opening for nipple 12. Nipple 12 is then threadedly inserted into the valve body, in such manner that its inner end portion 29 enters the recess 23 as shown in FIGURES 1 and 2. Assembly is then completed by threading the squib 14 into the open end of the valve body. Suitable conduits are then connected to the outer portion of nipple 12 and to valve outlet 33.
Since the nipple 12 is blind and is of integral construction, there is no possibility of leakage from the valve inlet to the outlet 33, to squib 14 or to the small-diameter portion 17 of the valve chamber. This eliminates all possibility of interaction between the controlled fluid and the explosive, and also eliminates the possibility of hydraulic lock due to the presence of controlled fluid in the valve chamber.
When the squib or explosive element 14 is electrically or mechanically ignited, the resulting gases are trapped by O- rings 21 and 34 between the outer end of ram 11 and the squib. Ram 11 is then propelled inwardly in an unimpeded manner (except for the resistance caused by the nipple shearing at stress riser 32, to be discussed below) until the tapered ram portion engages the wall of tapered portion 19 of the valve body. Thereafter, as discussed above, the outer portion of the ram is deformed to result in absorbing of the energy created by the explosion. It follows that the engagement of the inner end of the ram with wall 16 will be with insufiicient force to create undesirable effects such as rebound or fracture. Furthermore, and very importantly, the engagement between the tapered portions of the valve body and ram provides a secondary seal which is highly effective to prevent gases from entering the controlled fluid after the gas pressure between the ram and the squib becomes so great that O-ring 21 is no longer effective to prevent leakage.
During the above-described inward shifting of ram 11 from the FIGURE 1 position to the FIGURE 3 position, the inner portion 29 of nipple 12 is sheared off cleanly at the shoulder or stress riser 32, and travels in recess 23 into the chamber portion 17. The resulting close surface contact between flat surface 22 and the inner end of the thick-walled tubular nipple portion 28 results in several important advantages. Such advantages include preventing the ram 11 from rotating about its longitudinal axis, thereby insuring that port 24 will be in perfect axial alignment with the inlet and outlet passages. Another advantage is that contaminants and chips are prevented from entering the fluid stream. The presence of the stress riser or shoulder 32 insures that there will be no bending at the fracture point, but only an extremely clean fracture,
4 EMBQDIMENT OF FIGURE 4 The embodiment of FIGURE 4 is identical with that of FIGURES 1-3, except as will be described subsequently. Corresponding reference numerals have been employed to denote corresponding parts, certain reference numerals in FIGURE 4 being followed by the letter a.
In the construction of FIGURE 4, the threaded fitting for the inlet conduit is machined integral with the valve body 1%, as shown at 37. The nipple 12a is then pressed, shrunk or taper-fitted into the portion 37 of the valve body and in such manner that its blind inner end enters the recess 23 as in the case of the previous embodiment. In accordance with the present embodiment, an annular groove 33 is provided in the inner end portion of the nipple, at flat surface of the ram. Such groove augments the action of the stress riser in insuring a clean fracture of the nipple.
It is to be understood that the present invention may also be incorporated in a tandem valve having two or more sets of inlet and outlet passages in axial alignment (respectively) with each other. In such valves, the ram incorporates a recess 23 and port 24 for each coaxial set of inlet and outlet passages. Furthermore, and very importantly, the valve body and the ram incorporate cooperating tapered portions not only between the single squib and the adjacent coaxial valve passages but also between adjacent sets of coaxial passages. Such tapered portions between the adjacent sets of coaxial valve passages serve to isolate the controlled fluids from each other, in addition to absorbing the energy created by the explosion. Suitable O-rings may also be provided between adjacent sets of valve passages.
Various embodiments of the present invention, in addition to what has been illustrated and described in detail, may be employed without departing from the scope of the accompanying claims. 7
We claim:
1. A normally-closed explosive-actuated valve, comprising an elongated hollow valve body having a closed end and an open end, the interior wall of said body be- 1ng a relatively small-diameter cylinder adjacent said closed end and a relatively large-diameter cylinder adjacent said open end, said large-diameter and small-diameter cylindrical walls being axially spaced from each other and being connected by a frustoconical wall, an elongated one-piece ram mounted axially of said valve body for longitudinal movement therein, said ram-having an inner portion which is disposed radially-inwardly of said small-diameter cylindrical wall when the valve is in open condition, positive stop means provided in said valve body to stop movement of said ram at a predetermined point relatively adjacent said closed end, said ram also having a tapered portion corresponding generally to said frustoconical wall of said valve body and disposed to come into forceful engagement therewith prior to engagement of said ram with said positive stop means, said inner portion of said ram being provided with a flat surface lying in a plane parallel to the axis of said ram and relatively adjacent thereto, said inner portion of said ram having a cylindrical recess formed therein relatively adjacent the extreme inner end of said ram, said inner portion of said ram also having a cylindrical port formed therethrough parallel to said recess and disposed more remote than said recess from said extreme inner end of said ram, the axes of said recess and port being perpendicular to said flat surface, a nipple element mounted radially on said valve body and having a blind inner end extending into said recess, said nipple element also having a passage therethrough adapted to conduct fluid in response to removal of said blind inner end, said blind inner end of said nipple being associated with the main body thereof by a frangible connecting portion, said valve body having a radial outlet passage disposed coaxially with said nipple, said passage through said nipple and said outlet passage having diameters corresponding to each other and to that of said port through said ram, and a squib mounted in said open end of said valve body and adapted to be ignited to effect explosive propulsion of said ram inwardly until said ram engages said positive stop means, said port being so related to said recess that said port will be disposed coaxially with said passage through said nipple and with said outlet passage when said ram is engaged with I, said positive stop means to thereby create a straightthrough flow passage through said port, said interior of said valve body being free of objects between said squib and said ram.
2. The invention as claimed in claim 1, in which sealing means are provided in the outer end portion of said ram between said squib and said tapered portion of said ram.
3. The invention as claimed in claim 1, in which the taper angles of said tapered portion of said ram and of said frustoconical wall of said valve body are small, and in which said ram is of unitary one-piece construction.
4. A normally-closed explosive-actuated valve, comprising an elongated hollow valve body having a closed end and an open end, the valve chamber defined by said body having a relatively small-diameter cylindrical wall adjacent said closed end and a relatively large-diameter cylindrical wall adjacent said open end, said cylindrical walls being coaxial, said large-diameter and small-diameter walls being axially spaced from each other and being connected by frustoconical wall, an elongated one-piece ram mounted axially of said valve body for longitudinal movement therein, positive stop means provided in said valve body to stop movement of said ram at a predetermined point relatively adjacent said closed end, said ram having a tapered portion corresponding generally to said frustoconical wall of ,said valve body and disposed to come into forceful engagement theerwith prior to engagement of said ram with said positive stop means, said ram also having an inner portion which is disposed radiallyinwardly of said small-diameter cylindrical wall when the'valve is in open condition, said inner portion of said ram being provided with a flat surface lying in a plane parallel to the axis of said ram and relatively adjacent thereto, said inner portion of said ram having a cylindrical recess formed therein relatively adjacent the extreme inner end of said ram, said inner portion of said ram also having a cylindrical port formed therethrough parallel to said recess and disposed more remote than said recess from said extreme inner end of said ram, the axes of said recess and port being perpendicular to said flat surface, a nipple element mounted radially on said valve body at said small-diameter cylindrical wall and having a blind inner end extending into said recess, said nipple element also having a passage therethrough adapted to conduct fluid in response to removal of said blind inner end, said blind inner end of said nipple being associated with the main body thereof by a frangible connecting portion, said nipple also having a shoulder adjacent said frangible connecting portion and adapted to be engaged by said flat ram surface to prevent rotation of said ram upon longitudinal shifting thereof, said valve body having a radial outlet passage disposed diametrically opposite said nipple coaxially thereof, said port in said ram being so related to said positive stop means that said port will be disposed coaxially with said passage through said nipple and with said outlet passage when said ram is engaged with said positive stop means to thereby create a straight-through flow passage through the valve, and a squib mounted in said open end of said valve body and adapted to be ignited to effect explosive propulsion of said ram inwardly until said ram engages said positive stop means, the valve chamber within said valve body being free of objects between said squib and said ram whereby the combustion gases generated upon ignition of said squib contact said ram.
5. The invention as claimed in claim 4, in which a sealing ring is mounted on the outer portion of said ram for sliding-sealing contact with said large-diameter cylindrical wall. in References Cited by the Examiner UNITED STATES PATENTS 2,365,364 12/44 Temple l3768 2,540,322 2/51 Christensen l3768 XR 2,937,654 5/60 Wilner l3768 2,997,051 8/61 Williams l3768 3,093,151 6/63 Merkowitz l3768 3,111,133 11/63 Fulton l3768 ISADOR WEIL, Primary Examiner.

Claims (1)

1. A NORMALLY-CLOSED EXPLOSIVE-ACTUATED VALVE, COMPRISING AN ELONGATED HOLLOW VALVE BODY HAVING A CLOSED END AND AN OPEN END, THE INTERIOR WALL OF SAID BODY BEING A RELATIVELY SMALL-DIAMETER CYLINFER ADJACENT SAID CLOSED END AND A RELATIVELY LARGE-DIAMETER CYLINDER ADJACENT SAID OPEN END, SAID LARGE-DIAMETER AND SMALL-DIAMETER CYLINDRICAL WALLS BEING AXIALLY SPACED FROM EACH OTHER AND BEING CONNECTED BY A FRUSTOCONICAL WALL, AN ELONGATED ONE-PIECE RAM MOUNTED AXIALLY OF SAID VALVE BODY FOR LONGITUDINAL MOVEMENT THEREIN, SAID RAM HAVING AN INNER PORTION WHICH IS DISPOSED RADIALLY-INWARDLY OF SAID SMALL-DIAMETER CYLINDRICAL WALL WHEN THE VALVE IS IN OPEN CONDITION, POSITIVE STOP MEANS PROVIDED IN SAID VALVE BODY TO STOP MOVEMENT OF SAID RAM AT A PREDETERMINED POINT RELATIVELY ADJACENT SAID CLOSED END, SAID RAM ALSO HAVING A TAPERED PORTION CORRESPONDING GENERALLY TO SAID FRUSTOCONICAL WALL OF SAID VALVE BODY AND DISPOSED TO COME INTO FORCEFUL ENGAGEMENT THEREWITH PRIOR TO ENGAGEMENT OF SAID RAM WITH SAID POSITIVE STOP MEANS, SAID INNER PORTION OF SAID RAM BEING PROVIDED EITH A FLAT SURFACE LYING IN A PLANE PARALLEL TO THE AXIS OF SAID RAM AND RELATIVELY ADJACENT THERETO, SAID INNER PORTION OF SAID RAM HAVING A CYLINDRICAL RECESS FORMED THEREIN RELATIVELY ADJACENT THE EXTREME INNER END OF SAID RAM, SAID INNER PORTION OF SAID RAM ALSO HAVING A CYLINDRICAL PORT FORMED THERETHROUGH PARALLEL TO SAID RECESS AND DISPOSED MORE REMOTE THAN SAID RECESS FROM SAID EXTREME INNER END OF SAID RAM, THE AXES OF SAID RECESS AND PORT BEING PERPENDICULAR TO SAID FLAT SURFACE, A NIPPLE ELEMENT MOUNTED RADIALLY ON SAID VALVE BODY AND HAVING A BLIND INNER END EXTENDING INTO SAID RECESS, SAID NIPPLE ELEMENT ALSO HAVING A PASSAGE THERETHROUGH ADAPTED TO CONDUCT FLUID IN RESPONSE TO REMOVAL OF SAID BLINF INNER END, SAID BLIND INNER END OF SAID NIPPLE BEING ASSOCIATED WITH THE MAIN BODY THEREOF BY A FRANGIBLE CONNECTING PORTION, SAID VALVE BODY HAVING A RADIAL OUTLET PASSAGE DISPOSED COAXIALLY WITH SAID NIPPLE SAID PASSAGE THROUGH SAID NIPPLE AND SAID OUTLET PASSAGE HAVING DIAMETERS CORRESPONDING TO EACH OTHER AND TO THAT SAID OPEN END OF SAID VALVE BODY AND ADAPTED TO BE IGNITED TO EFFECT EXPLOSIVE PROPULSION OF SAID RAM INWARDLY UNTIL OF SAID PORT THROUGH SAID RAM, AND A SQUIB MOUNTED IN SAID RAM ENGAGES SAID POSITIVE STOP MEANS, SAID PORT BEING SO RELATED TO SAID RECESS THAT SAID PORT WILL BE DISPOSED COAXIALLY WITH SAID PASSAGE THROUGH SAID NIPPLE AND WITH SAID OUTLET PASSAGE WHEN SAID RAM IS ENGAGED WITH SAID POSITIVE STOP MEANS TO THEREBY CREATE A STRAIGHTTHROUGH FLOW PASSAGE THROUGH SAID PORT, SAID INTERIOR OF SAID VALVE BODY BEING FREE OF OBJECTS BETWEEN SAID SQUIB AND SAID RAM.
US249953A 1963-01-07 1963-01-07 Normally-closed explosive-actuated valve Expired - Lifetime US3202162A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US249953A US3202162A (en) 1963-01-07 1963-01-07 Normally-closed explosive-actuated valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US249953A US3202162A (en) 1963-01-07 1963-01-07 Normally-closed explosive-actuated valve

Publications (1)

Publication Number Publication Date
US3202162A true US3202162A (en) 1965-08-24

Family

ID=22945712

Family Applications (1)

Application Number Title Priority Date Filing Date
US249953A Expired - Lifetime US3202162A (en) 1963-01-07 1963-01-07 Normally-closed explosive-actuated valve

Country Status (1)

Country Link
US (1) US3202162A (en)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3332432A (en) * 1966-01-14 1967-07-25 Pyronetics Inc Explosive-operated valve
US3416548A (en) * 1966-02-14 1968-12-17 Bendix Corp High pressure release valve
US3638669A (en) * 1970-05-22 1972-02-01 Us Navy Cantilevered breakaway fuel and oxidizer release
US3757810A (en) * 1972-01-11 1973-09-11 C B F System Inc Shear valve and frangible fitting
US3892253A (en) * 1973-07-20 1975-07-01 Cbf Systems Inc Shear valve with frangible fitting
US3985058A (en) * 1975-08-08 1976-10-12 The United States Of America As Represented By The Secretary Of The Army Self-sealing fluidic explosive initiator
US4003395A (en) * 1975-07-28 1977-01-18 Systron Donner Corporation Quick-opening valve operated by explosive charge
US4149555A (en) * 1977-08-22 1979-04-17 The United States Of America As Represented By The Secretary Of The Navy Gas-actuated valves
US4248257A (en) * 1979-03-26 1981-02-03 The United States Of America As Represented By The Secretary Of The Navy Flood valve
FR2467138A1 (en) * 1979-10-12 1981-04-17 Raytheon Co DEVICE FOR MAKING A BUOY FLOATABLE
US4619284A (en) * 1984-03-21 1986-10-28 Societe Nationale Industrielle Aerospatiale Pyrotechnic valve
EP0593867A1 (en) * 1992-10-17 1994-04-27 PAGG Produktions AG Giswil Quick-action stop valve
US20030168097A1 (en) * 2002-03-11 2003-09-11 Commissariat A I'energie Atomique Pyrotechnically actuated microvalve
US20060180201A1 (en) * 2001-01-16 2006-08-17 Evans Griffith S Piston-activated valve and methods and apparatus for restraining free play in a device
US20100314562A1 (en) * 2009-06-10 2010-12-16 Baker Hughes Incorporated Delay activated valve and method
US20110030941A1 (en) * 2009-08-07 2011-02-10 Autoliv Asp, Inc. Relief valve
RU2455547C1 (en) * 2010-12-15 2012-07-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Tapper valve
US20130167377A1 (en) * 2008-01-16 2013-07-04 United States Of America As Represented By The Administrator Of The National Aeronautics And Spac Systems, methods and apparatus of a nitinol valve
CN104912859A (en) * 2014-03-12 2015-09-16 空中客车Ds有限责任公司 Valve assembly, in particular for space travel drive systems, which is closed when not actuated
US10145482B2 (en) 2014-01-29 2018-12-04 Raytheon Company Frangible valve
RU2681558C1 (en) * 2018-03-12 2019-03-11 Акционерное общество "Конструкторское бюро химавтоматики" Pyro-valve
US10927962B1 (en) 2019-08-22 2021-02-23 William E. Hurst Pressure loss mitigation and durable valve
US11713816B1 (en) 2019-08-22 2023-08-01 Colt Irrigation, LLC Pressure loss mitigation and durable valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2365364A (en) * 1943-06-26 1944-12-19 Temple Velocity Equipment Inc Outlet valve
US2540322A (en) * 1947-08-22 1951-02-06 Drilling Equipment Mfg Co Device for testing blowout preventers and casing
US2937654A (en) * 1958-02-10 1960-05-24 Wilner L Bruce Tube shearing valve
US2997051A (en) * 1958-11-20 1961-08-22 Pneumo Dynamics Corp Explosive actuated valve
US3093151A (en) * 1958-09-12 1963-06-11 Gen Dynamics Corp Shear valve and frangible fitting
US3111133A (en) * 1959-08-11 1963-11-19 Hydro Space Technology Inc Explosive actuated normally closed valve

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2365364A (en) * 1943-06-26 1944-12-19 Temple Velocity Equipment Inc Outlet valve
US2540322A (en) * 1947-08-22 1951-02-06 Drilling Equipment Mfg Co Device for testing blowout preventers and casing
US2937654A (en) * 1958-02-10 1960-05-24 Wilner L Bruce Tube shearing valve
US3093151A (en) * 1958-09-12 1963-06-11 Gen Dynamics Corp Shear valve and frangible fitting
US2997051A (en) * 1958-11-20 1961-08-22 Pneumo Dynamics Corp Explosive actuated valve
US3111133A (en) * 1959-08-11 1963-11-19 Hydro Space Technology Inc Explosive actuated normally closed valve

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3332432A (en) * 1966-01-14 1967-07-25 Pyronetics Inc Explosive-operated valve
US3416548A (en) * 1966-02-14 1968-12-17 Bendix Corp High pressure release valve
US3638669A (en) * 1970-05-22 1972-02-01 Us Navy Cantilevered breakaway fuel and oxidizer release
US3757810A (en) * 1972-01-11 1973-09-11 C B F System Inc Shear valve and frangible fitting
US3892253A (en) * 1973-07-20 1975-07-01 Cbf Systems Inc Shear valve with frangible fitting
US4003395A (en) * 1975-07-28 1977-01-18 Systron Donner Corporation Quick-opening valve operated by explosive charge
US3985058A (en) * 1975-08-08 1976-10-12 The United States Of America As Represented By The Secretary Of The Army Self-sealing fluidic explosive initiator
US4149555A (en) * 1977-08-22 1979-04-17 The United States Of America As Represented By The Secretary Of The Navy Gas-actuated valves
US4248257A (en) * 1979-03-26 1981-02-03 The United States Of America As Represented By The Secretary Of The Navy Flood valve
FR2467138A1 (en) * 1979-10-12 1981-04-17 Raytheon Co DEVICE FOR MAKING A BUOY FLOATABLE
US4619284A (en) * 1984-03-21 1986-10-28 Societe Nationale Industrielle Aerospatiale Pyrotechnic valve
EP0593867A1 (en) * 1992-10-17 1994-04-27 PAGG Produktions AG Giswil Quick-action stop valve
US20060180201A1 (en) * 2001-01-16 2006-08-17 Evans Griffith S Piston-activated valve and methods and apparatus for restraining free play in a device
US7096878B1 (en) 2002-03-11 2006-08-29 Commissariat A L'energie Atomique Pyrotechnically actuated microvalve
US20060185728A1 (en) * 2002-03-11 2006-08-24 Commissariat A L'energie Atomique Pyrotechnically actuated microvalve
US20030168097A1 (en) * 2002-03-11 2003-09-11 Commissariat A I'energie Atomique Pyrotechnically actuated microvalve
US7059339B2 (en) * 2002-03-11 2006-06-13 Commissariat A L'energie Atomique Pyrotechnically actuated microvalve
US20130167377A1 (en) * 2008-01-16 2013-07-04 United States Of America As Represented By The Administrator Of The National Aeronautics And Spac Systems, methods and apparatus of a nitinol valve
US8499779B2 (en) * 2008-01-16 2013-08-06 The United States Of America As Represented By The Administrator Of The National Aeronautics Space Administration Systems, methods and apparatus of a nitinol valve
US20100314562A1 (en) * 2009-06-10 2010-12-16 Baker Hughes Incorporated Delay activated valve and method
US8397741B2 (en) * 2009-06-10 2013-03-19 Baker Hughes Incorporated Delay activated valve and method
US20110030941A1 (en) * 2009-08-07 2011-02-10 Autoliv Asp, Inc. Relief valve
US8671967B2 (en) * 2009-08-07 2014-03-18 Autoliv Asp, Inc. Relief valve
RU2455547C1 (en) * 2010-12-15 2012-07-10 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Tapper valve
US10145482B2 (en) 2014-01-29 2018-12-04 Raytheon Company Frangible valve
CN104912859A (en) * 2014-03-12 2015-09-16 空中客车Ds有限责任公司 Valve assembly, in particular for space travel drive systems, which is closed when not actuated
US9746092B2 (en) * 2014-03-12 2017-08-29 Airbus Ds Gmbh Valve assembly, in particular for space travel drive systems, which is closed when not actuated
CN104912859B (en) * 2014-03-12 2018-11-23 空中客车Ds有限责任公司 It is used for the valve module of aerospace drive system closed when not manipulating in particular
US20150260300A1 (en) * 2014-03-12 2015-09-17 Airbus Ds Gmbh Valve Assembly, In Particular for Space Travel Drive Systems, Which is Closed When Not Actuated
RU2681558C1 (en) * 2018-03-12 2019-03-11 Акционерное общество "Конструкторское бюро химавтоматики" Pyro-valve
US10927962B1 (en) 2019-08-22 2021-02-23 William E. Hurst Pressure loss mitigation and durable valve
US11313476B1 (en) 2019-08-22 2022-04-26 Colt Irrigation, LLC Pressure loss mitigation and durable valve
US11713816B1 (en) 2019-08-22 2023-08-01 Colt Irrigation, LLC Pressure loss mitigation and durable valve
US12013047B1 (en) 2019-08-22 2024-06-18 Colt Irrigation, LLC Pressure loss mitigation and durable valve

Similar Documents

Publication Publication Date Title
US3202162A (en) Normally-closed explosive-actuated valve
US3844585A (en) Pipe coupling
US4724857A (en) Pressure relief valve
US3375026A (en) Tube coupling
US4872471A (en) Separable and breakaway valve interconnecting a fluid line
CA2233184A1 (en) Dual valve fitting for enabling quick measurement of pressure
US3260272A (en) Normally-closed explosive-actuated valve
US5110160A (en) High pressure port fitting system
US3027903A (en) Explosively actuated valves
KR100990296B1 (en) Straight thread adjustable port end
US3494370A (en) Explosive valve
US3474809A (en) Normally-closed explosive-operated valve
US3332432A (en) Explosive-operated valve
US2732169A (en) matteo
US2679411A (en) High-pressure tubing coupling
US3972343A (en) Shuttle valve
US2322658A (en) Valve
US2845282A (en) Pipe connector having adjustable elbow
US3180664A (en) Ball pipe joint with composite ball member
RU2142085C1 (en) Pyrovalve
US3548861A (en) Line tapping service valve
US3473543A (en) Chip-free explosively actuated valve
US1136606A (en) Safety-valve.
US3601362A (en) Stop for valve shank
JPS5930956B2 (en) Valves with breakable closures