US3119298A - Explosively separable fastener - Google Patents

Explosively separable fastener Download PDF

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Publication number
US3119298A
US3119298A US47415A US4741560A US3119298A US 3119298 A US3119298 A US 3119298A US 47415 A US47415 A US 47415A US 4741560 A US4741560 A US 4741560A US 3119298 A US3119298 A US 3119298A
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Prior art keywords
threaded
head
explosive
bore
squib
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Expired - Lifetime
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US47415A
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Clarence K Brown
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Hi Shear Corp
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Hi Shear Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/006Explosive bolts; Explosive actuators
    • 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
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B31/00Screwed connections specially modified in view of tensile load; Break-bolts
    • F16B31/005Breakbolts loosening due to the action of an explosive charge

Definitions

  • An object of this invention is to provide a fastener that will join structural members, primarily in shear applications, with the full shear strength for the size of the fastener and with the capability of withstanding the tensfle loads present in such a joint and the necessary installation torques; yet this fastener to be capable of being separated by a relatively small charge of solid propellant material which may be detonated from a remote point by an electrical signal.
  • a further object of this invention is to provide an explosive bolt which may be installed in an unarmed condition and which may be armed or disarmed for safety at any tirne.
  • a separable bolt is made in two primary sections, one having a threaded end and the other a head end.
  • the threaded end section has a re Jerusalem diameter which fits a longitudinal bore in the headed end.
  • a third member is employed to retain the reduced diameter of the threaded section of the bolt with in the headed section.
  • the longitudinal bore of the headed end is adapted at the head to receive a conventional explosive squib, the retaining member is of a size and form which will fail in shear upon detonation of the squib.
  • sealing means may be provided between the threaded section of the head section of the bolt to confine the explosive detonation of the squib and direct its full energy to separating the bolt.
  • FIG. 1 is a side elevation partially in cross-section of one embodiment of this invention shown assembled in structure with a squib and nut in place;
  • FIG. 2 is a cross-section of the device of FIG. 1 taken at line 22 of FIG. 1;
  • FIG. 3 is a cross-section taken at line 3-3 of FIG. 1;
  • FIG. 4 is a side elevation in cross-section of another embodiment of the invention.
  • FIG. 5 is a cross-section taken at line 5-5 of FIG. 4.
  • FIG. 1 there is shown a preferred embodiment of this invention.
  • the fastener is shown with two primary sections, 33 being a threaded member and a head member 16.
  • the threaded member 33 is cylindrical in shape with a thread 32,, a shank portion 31, and a reduced cylindrical diameter 30.
  • the head end 23 is of geometric shape to accept a Wrench and has a cylindrical shank portion 34.
  • the bore 26 is shown coaxially through head "tee Li member 16 and is of a size to receive a reduced shank diameter 30 of thread end 33 at the shank end of head member 16. At the head end 23 of head member 16 the bore 26 has a thread 17 to accept a standard squib 18.
  • Such a squib conventionally has an explosive chamber 24 and electrical leads l9 and 22 which may be attached to a source of D.C. current 2% and which squib will be detonated by closing a switch 21.
  • this fastener threaded end 33 is inserted into bore 26 of head member 1d and a transverse hole is drilled through both members to accept a shear pin 29.
  • the fastener in FIG. 1 is shown fastening two sheets of structure 14 and 15*, shown in phantom, held by nut 12, also shown in phantom.
  • the reduced diameter 3d of thread end 33 may have an undercut 27 of a size to receive an elastomeric O-ring sealing member 28.
  • This sealing member prevents leakage of gaseous products of the explosive charge contained in the squib upon detonation and concentrates the entire force of the explosion on surface 25 of thread end 33 to effect shear failure of pin 29, thus separating the fastener and the joint.
  • FIG. 4 there is shown another embodiment of th's invention.
  • Threaded end Si? is cylindrical in shape with a thread 49 at one end, a cylindrical shank S1 and a reduced cylindrical diameter 4/7 adjacent to shank 51.
  • the reduced diameter 47 term' mates in a tapered surface 4
  • Head member it has a smooth cylindrical shank 46 which is preferably the same diameter as the shank 51 of thread member 5t.
  • a longitudinal coaxial bore 42 extends through head member 4%, and at the end remote from the head, is enlarged to the same diameter as the reduced shank 4'7 of the threaded member 5d and terminates in a tapered face 641 to permit the reduced diameter 47 of threaded member 5% ⁇ to be completely inserted into the bore of member 46.
  • a recess 38 which is of a shape and size to accept an elastomeric sealing member 39.
  • the bore reduces in size to produce a passage 52 which extends through the head of head member 49.
  • the bore d2 terminates in a threaded area 41 which is adapted to accept a conventional explosive squib.
  • Reraining member 37 is a split, resilient ring which engages groove as in threaded member 5% and groove 53 in head member 46* to retain both parts in assembly.
  • sealing ring 39 To assemble the device sealing ring 39 must first be inserted into recess 38. The retaining ring 37 must be compressed and inserted into groove 53. Groove 53 should be of sufficient depth to allow expansion of ring 37 as the tapered nose 44 of threaded member 5%) is pushed into bore 45 of head member it), thereby expanding retainer 3'7 until it snaps into groove 36 of the threaded member 5%.
  • a hole 56 may be drilled at the parting line 54 at the shank diameter of the two mating parts and transverse to the center line of the two parts and a pin 55 inserted to prevent relative rotation of threaded end 50 with head end it) during installation torquing of a nut.
  • a conventional squib 58, with electrical leads 59 and at is shown in place in the head end 48 of the stud. This squib may be removed at any time to disarm the stud without affecting the structural integrity of the stud or the structure that is assembled with the stud.
  • the fastener of FIG. 4 would be inserted into structure which comprises two or more sheets or members and installed with a conventional nut.
  • a conventional type of explosive squib 58 would be installed in the head end of the fastener with an explosive charge thereby contained within cavity 52.
  • External electrical leads 59 and 60 would connect to a source of power and upon completing, the circuit the explosive would detonate.
  • Confined in close quarters the resultant shock Wave would act upon surface 43 of threaded member '50 and react against the body of the squib to cause retaining member 37 to fail in shear, blowing both parts out of the struc ture longitudinally and thereby separating the structure.
  • the retaining member may be made of a strength that will require a very minimum of explosive to create a reliable separation.
  • a threaded stud assembly for explosive separation which comprises a first threaded member, said member having a threaded end, a smooth shank portion adjacent the threaded end, a reduced coaxial cylindrical section adjacent said smooth shank portion, said reduced cylindrical section terminating in a tapered face at the end opposite said threaded end, said tapered face truncated to form a fiat end to said first threaded member, an external annular groove in said reduced cylindrical section adjacent said tapered face; a second member, said second member having a head end, said head end of geometric shape adapted for wrenching, said second member having a.
  • said bore adapted at said head end of said second member to receive an explosive squib to form a closed chamber for maximum explosive effect in combination with said fiat end of said tapered face of said reduced cylindrical section and said coaxial bore of said second member; a retaining ring, said ring split at one side, said ring adapted to engage said external annular groove of said first threaded member and said internal annular groove of said second member to retain said members in assembly; key means between said first threaded member and said second member to prevent relative rotation; sealing means between said tapered face of said reduced cylindrical section of said first member and said tapered shoulder of said bore of said second member adapted to confine an explosive force Within said bore for maximum explosive effect.

Description

Jan. 28, 1964 c. K. BROWN EXPLOSIVELY SEPARABLE FASTENER Filed Aug. 4. 1960 INVEN TOR. CLARENCE K. BROWN BY wwm A GENT United States Patent antenna. EXPLQSHVELY SEPARABLE FASTENER Clarence K. Brown, Bellilower, Calif assignor to lili- Shear Corporation, Torrance, Calif., a corporation of California Filed Aug. 4, 19st Ser. No. 47,415 1 (Tlaim. (Cl. 85-1l) This invention relates to a fastener which may be explosively separated.
An object of this invention is to provide a fastener that will join structural members, primarily in shear applications, with the full shear strength for the size of the fastener and with the capability of withstanding the tensfle loads present in such a joint and the necessary installation torques; yet this fastener to be capable of being separated by a relatively small charge of solid propellant material which may be detonated from a remote point by an electrical signal.
A further object of this invention is to provide an explosive bolt which may be installed in an unarmed condition and which may be armed or disarmed for safety at any tirne.
Conventional explosive bolts have been made in the past but have always containedan explosive charge buried in a recess within the shank. The structure of the bolt had tobe weakened to provide :for fracture due to the explosive detonation; however, the bolt structure could not be weakened beyond a point Where the useful strength of the bolt would be excessively impaired so a relatively large explosive charge was required to separate the bolt. This excessive explosive energy could do damage to adjacent structures. Moreover, this type of bolt would have to be installed in an armed condition without the capability of being disarmed.
According to this invention a separable bolt is made in two primary sections, one having a threaded end and the other a head end. The threaded end section has a re duced diameter which fits a longitudinal bore in the headed end. A third member is employed to retain the reduced diameter of the threaded section of the bolt with in the headed section. The longitudinal bore of the headed end is adapted at the head to receive a conventional explosive squib, the retaining member is of a size and form which will fail in shear upon detonation of the squib.
According to a preferred but optional feature of the invention sealing means may be provided between the threaded section of the head section of the bolt to confine the explosive detonation of the squib and direct its full energy to separating the bolt.
The above and other features of this invention will be fully understood from the following detailed description and the accompanying drawings, of which:
FIG. 1 is a side elevation partially in cross-section of one embodiment of this invention shown assembled in structure with a squib and nut in place;
FIG. 2 is a cross-section of the device of FIG. 1 taken at line 22 of FIG. 1;
FIG. 3 is a cross-section taken at line 3-3 of FIG. 1;
FIG. 4 is a side elevation in cross-section of another embodiment of the invention;
FIG. 5 is a cross-section taken at line 5-5 of FIG. 4.
In FIG. 1 there is shown a preferred embodiment of this invention. The fastener is shown with two primary sections, 33 being a threaded member and a head member 16. The threaded member 33 is cylindrical in shape with a thread 32,, a shank portion 31, and a reduced cylindrical diameter 30. The head end 23 is of geometric shape to accept a Wrench and has a cylindrical shank portion 34. The bore 26 is shown coaxially through head "tee Li member 16 and is of a size to receive a reduced shank diameter 30 of thread end 33 at the shank end of head member 16. At the head end 23 of head member 16 the bore 26 has a thread 17 to accept a standard squib 18. Such a squib conventionally has an explosive chamber 24 and electrical leads l9 and 22 which may be attached to a source of D.C. current 2% and which squib will be detonated by closing a switch 21. In manufacturing this fastener threaded end 33 is inserted into bore 26 of head member 1d and a transverse hole is drilled through both members to accept a shear pin 29. The fastener in FIG. 1 is shown fastening two sheets of structure 14 and 15*, shown in phantom, held by nut 12, also shown in phantom.
As a preferred but optional feature the reduced diameter 3d of thread end 33 may have an undercut 27 of a size to receive an elastomeric O-ring sealing member 28. This sealing member prevents leakage of gaseous products of the explosive charge contained in the squib upon detonation and concentrates the entire force of the explosion on surface 25 of thread end 33 to effect shear failure of pin 29, thus separating the fastener and the joint.
in FIG. 4 there is shown another embodiment of th's invention. There are two primary members again, a threaded member 5t) and a head member 4b. Threaded end Si? is cylindrical in shape with a thread 49 at one end, a cylindrical shank S1 and a reduced cylindrical diameter 4/7 adjacent to shank 51. The reduced diameter 47 term'mates in a tapered surface 4 In the reduced diameter 47 there is an undercut of rectangular section 36. Head member it has a smooth cylindrical shank 46 which is preferably the same diameter as the shank 51 of thread member 5t. There is an enlarged head 48 of geometrical shape to accept a wrench. A longitudinal coaxial bore 42, extends through head member 4%, and at the end remote from the head, is enlarged to the same diameter as the reduced shank 4'7 of the threaded member 5d and terminates in a tapered face 641 to permit the reduced diameter 47 of threaded member 5%} to be completely inserted into the bore of member 46. In the tapered face 64- of this enlarged bore there is a recess 38 which is of a shape and size to accept an elastomeric sealing member 39. The bore reduces in size to produce a passage 52 which extends through the head of head member 49. The bore d2 terminates in a threaded area 41 which is adapted to accept a conventional explosive squib. Reraining member 37 is a split, resilient ring which engages groove as in threaded member 5% and groove 53 in head member 46* to retain both parts in assembly. To assemble the device sealing ring 39 must first be inserted into recess 38. The retaining ring 37 must be compressed and inserted into groove 53. Groove 53 should be of sufficient depth to allow expansion of ring 37 as the tapered nose 44 of threaded member 5%) is pushed into bore 45 of head member it), thereby expanding retainer 3'7 until it snaps into groove 36 of the threaded member 5%. After assembly of threaded end to head end 4d a hole 56 may be drilled at the parting line 54 at the shank diameter of the two mating parts and transverse to the center line of the two parts and a pin 55 inserted to prevent relative rotation of threaded end 50 with head end it) during installation torquing of a nut. A conventional squib 58, with electrical leads 59 and at is shown in place in the head end 48 of the stud. This squib may be removed at any time to disarm the stud without affecting the structural integrity of the stud or the structure that is assembled with the stud.
In use the fastener of FIG. 4 would be inserted into structure which comprises two or more sheets or members and installed with a conventional nut. A conventional type of explosive squib 58 would be installed in the head end of the fastener with an explosive charge thereby contained within cavity 52. External electrical leads 59 and 60 would connect to a source of power and upon completing, the circuit the explosive would detonate. Confined in close quarters the resultant shock Wave would act upon surface 43 of threaded member '50 and react against the body of the squib to cause retaining member 37 to fail in shear, blowing both parts out of the struc ture longitudinally and thereby separating the structure. Due to this design, the retaining member may be made of a strength that will require a very minimum of explosive to create a reliable separation.
This invention is not to be limited by the embodiments shown in the drawings and described in the description, but only in accordance with the scope of the appended claim.
I claim:
A threaded stud assembly for explosive separation which comprises a first threaded member, said member having a threaded end, a smooth shank portion adjacent the threaded end, a reduced coaxial cylindrical section adjacent said smooth shank portion, said reduced cylindrical section terminating in a tapered face at the end opposite said threaded end, said tapered face truncated to form a fiat end to said first threaded member, an external annular groove in said reduced cylindrical section adjacent said tapered face; a second member, said second member having a head end, said head end of geometric shape adapted for wrenching, said second member having a. coaxial bore extending through said second member, said bore at the end opposite the head end adapted to accept said reduced cylindrical section of said first member in close engagement, said enlarged bore terminating in a tapered shoulder, said tapered shoulder adapted to fit closely with said tapered face of said reduced cylindrical section of said first member, an internal annular groove adjacent said tapered shoulder, said internal groove adapted to register with said. external groove of said first threaded member when said first and second members are assembled one to the other, said bore adapted at said head end of said second member to receive an explosive squib to form a closed chamber for maximum explosive effect in combination with said fiat end of said tapered face of said reduced cylindrical section and said coaxial bore of said second member; a retaining ring, said ring split at one side, said ring adapted to engage said external annular groove of said first threaded member and said internal annular groove of said second member to retain said members in assembly; key means between said first threaded member and said second member to prevent relative rotation; sealing means between said tapered face of said reduced cylindrical section of said first member and said tapered shoulder of said bore of said second member adapted to confine an explosive force Within said bore for maximum explosive effect.
References Cited in the file of this patent UNITED STATES PATENTS 1,390,645 Ritter Sept. 13, 1921 2,061,835 Haines Nov. 24, 1936 2,165,656 Ryan July 11, 1939 2,492,006 Raybould Dec. 20, 1949 2,577,009 Frantz Dec. 4, 1951 2,653,504 Smith Sept. 29, 1953 2,809,584 Smith Oct. 15, 1957 2,938,429 Jaglowski et a1. May 31, 1960 3,032,356 Botsford May 1, 1962
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Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3204515A (en) * 1962-05-17 1965-09-07 Space Ordnance Systems Explosively releasable nut assembly
US3254555A (en) * 1963-08-26 1966-06-07 Harvey Aluminum Inc Separation bolt
US3265408A (en) * 1961-11-06 1966-08-09 Hi Shear Corp Explosively separable coupling
US3331278A (en) * 1965-03-09 1967-07-18 Hi Shear Corp Separable fastener assembly
US3334924A (en) * 1963-07-09 1967-08-08 Fmc Corp Pipe hanging apparatus
US3362290A (en) * 1965-04-13 1968-01-09 Mc Donnell Douglas Corp Non-contaminating thrusting separation system
US3505925A (en) * 1967-10-16 1970-04-14 Mc Donnell Douglas Corp Structure release system
US3599528A (en) * 1969-08-21 1971-08-17 Allied Chem Pressure relief bolt
US3640174A (en) * 1971-01-13 1972-02-08 Us Air Force Pyromechanical release device
US3675533A (en) * 1968-04-22 1972-07-11 Heinz Gawlick Fastening means severable by ignition of an explosive charge
US3741583A (en) * 1970-06-25 1973-06-26 Nissan Motor Motor vehicle safety device
US3791300A (en) * 1971-09-04 1974-02-12 Rheinmetall Gmbh Flare shell
DE2317930A1 (en) * 1972-06-26 1974-02-21 France Etat METHOD AND DEVICE FOR SEPARATING A MECHANICAL PART BY USING THE ENERGY OF AN EXPLOSIVE
US3944023A (en) * 1975-03-07 1976-03-16 The B. F. Goodrich Company Releasable restraint in an inflatable emergency evacuation slide
US3981467A (en) * 1975-10-17 1976-09-21 The United States Of America As Represented By The Secretary Of The Air Force Launch lock device
US4446932A (en) * 1981-04-24 1984-05-08 Petro-Drive, Inc. Hydrostatic shear pin
US4511296A (en) * 1983-03-16 1985-04-16 Invocas, Inc. Anchor bolt with mechanical keys deployed by internal pressurization
US4671715A (en) * 1986-04-03 1987-06-09 Hi-Shear Corporation Lesser shock separation fastener
US4754706A (en) * 1983-06-27 1988-07-05 Etienne Lacroix Tous Artifices Munition scattering projectile
US4836081A (en) * 1988-02-11 1989-06-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Toggle release
US4864910A (en) * 1989-02-23 1989-09-12 United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Double swivel toggle release
US4867357A (en) * 1987-12-21 1989-09-19 General Dynamics Corp., Pomona Division Jettisonable protective cover device
US4986708A (en) * 1989-06-12 1991-01-22 The United States Of America As Represneted By The Secretary Of The Navy Self-sealing separation fastener for small confines
US5361676A (en) * 1993-07-19 1994-11-08 Gibbs Jerry L Explosively-separable fastener with umbilical cord cutter
US5807589A (en) * 1996-12-02 1998-09-15 Diversified Machining, Inc. Rotational molding machine
US6464442B1 (en) * 1996-05-31 2002-10-15 O.I.A., Llc Safety release fasteners
US20040255811A1 (en) * 2003-01-29 2004-12-23 Uwe Brede Pyromechanical separating element
US7114427B1 (en) * 2005-10-19 2006-10-03 Special Devices, Inc. Quick-loosening mechanical linking device
US20110017315A1 (en) * 2001-01-05 2011-01-27 Bs&B Safety Systems, Inc. Pressure relief device assemblies
US20110204177A1 (en) * 2010-02-25 2011-08-25 Pacific Scientific Energetic Materials Company Projectile diverter release and method of diverting a projectile
US11852181B1 (en) * 2021-08-30 2023-12-26 United States Of America, As Represented By The Secretary Of The Navy Separation bolt by eutectic decohesion

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1390645A (en) * 1920-03-26 1921-09-13 George B Bassett Water-meter
US2061835A (en) * 1932-11-12 1936-11-24 Technicraft Engineering Corp Ammunition
US2165656A (en) * 1938-09-15 1939-07-11 Michael H Ryan Connector
US2492006A (en) * 1945-05-17 1949-12-20 Weatherhead Co Pressure cylinder
US2577009A (en) * 1946-11-12 1951-12-04 Virgil L Frantz Sander nozzle assembly
US2653504A (en) * 1950-03-20 1953-09-29 Thomas C Smith Explosively severable bolt
US2809584A (en) * 1953-04-01 1957-10-15 Smith Bernard Connector ring for two stage rockets
US2938429A (en) * 1957-05-23 1960-05-31 Jr Joseph J Jaglowski Explosive release actuator
US3032356A (en) * 1960-01-26 1962-05-01 Neilan B Botsford Explosive means to separate casing members

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1390645A (en) * 1920-03-26 1921-09-13 George B Bassett Water-meter
US2061835A (en) * 1932-11-12 1936-11-24 Technicraft Engineering Corp Ammunition
US2165656A (en) * 1938-09-15 1939-07-11 Michael H Ryan Connector
US2492006A (en) * 1945-05-17 1949-12-20 Weatherhead Co Pressure cylinder
US2577009A (en) * 1946-11-12 1951-12-04 Virgil L Frantz Sander nozzle assembly
US2653504A (en) * 1950-03-20 1953-09-29 Thomas C Smith Explosively severable bolt
US2809584A (en) * 1953-04-01 1957-10-15 Smith Bernard Connector ring for two stage rockets
US2938429A (en) * 1957-05-23 1960-05-31 Jr Joseph J Jaglowski Explosive release actuator
US3032356A (en) * 1960-01-26 1962-05-01 Neilan B Botsford Explosive means to separate casing members

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265408A (en) * 1961-11-06 1966-08-09 Hi Shear Corp Explosively separable coupling
US3204515A (en) * 1962-05-17 1965-09-07 Space Ordnance Systems Explosively releasable nut assembly
US3334924A (en) * 1963-07-09 1967-08-08 Fmc Corp Pipe hanging apparatus
US3254555A (en) * 1963-08-26 1966-06-07 Harvey Aluminum Inc Separation bolt
US3331278A (en) * 1965-03-09 1967-07-18 Hi Shear Corp Separable fastener assembly
US3362290A (en) * 1965-04-13 1968-01-09 Mc Donnell Douglas Corp Non-contaminating thrusting separation system
US3505925A (en) * 1967-10-16 1970-04-14 Mc Donnell Douglas Corp Structure release system
US3675533A (en) * 1968-04-22 1972-07-11 Heinz Gawlick Fastening means severable by ignition of an explosive charge
US3599528A (en) * 1969-08-21 1971-08-17 Allied Chem Pressure relief bolt
US3741583A (en) * 1970-06-25 1973-06-26 Nissan Motor Motor vehicle safety device
US3640174A (en) * 1971-01-13 1972-02-08 Us Air Force Pyromechanical release device
US3791300A (en) * 1971-09-04 1974-02-12 Rheinmetall Gmbh Flare shell
DE2317930A1 (en) * 1972-06-26 1974-02-21 France Etat METHOD AND DEVICE FOR SEPARATING A MECHANICAL PART BY USING THE ENERGY OF AN EXPLOSIVE
US3944023A (en) * 1975-03-07 1976-03-16 The B. F. Goodrich Company Releasable restraint in an inflatable emergency evacuation slide
US3981467A (en) * 1975-10-17 1976-09-21 The United States Of America As Represented By The Secretary Of The Air Force Launch lock device
US4446932A (en) * 1981-04-24 1984-05-08 Petro-Drive, Inc. Hydrostatic shear pin
US4511296A (en) * 1983-03-16 1985-04-16 Invocas, Inc. Anchor bolt with mechanical keys deployed by internal pressurization
US4754706A (en) * 1983-06-27 1988-07-05 Etienne Lacroix Tous Artifices Munition scattering projectile
US4671715A (en) * 1986-04-03 1987-06-09 Hi-Shear Corporation Lesser shock separation fastener
US4867357A (en) * 1987-12-21 1989-09-19 General Dynamics Corp., Pomona Division Jettisonable protective cover device
US4836081A (en) * 1988-02-11 1989-06-06 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Toggle release
US4864910A (en) * 1989-02-23 1989-09-12 United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Double swivel toggle release
US4986708A (en) * 1989-06-12 1991-01-22 The United States Of America As Represneted By The Secretary Of The Navy Self-sealing separation fastener for small confines
US5361676A (en) * 1993-07-19 1994-11-08 Gibbs Jerry L Explosively-separable fastener with umbilical cord cutter
US6464442B1 (en) * 1996-05-31 2002-10-15 O.I.A., Llc Safety release fasteners
US6101699A (en) * 1996-12-02 2000-08-15 Defatte; Robert G. Method of repairing bolts with replaceable threads
US5807589A (en) * 1996-12-02 1998-09-15 Diversified Machining, Inc. Rotational molding machine
US20110017315A1 (en) * 2001-01-05 2011-01-27 Bs&B Safety Systems, Inc. Pressure relief device assemblies
US8517041B2 (en) * 2001-01-05 2013-08-27 Bs&B Safety Systems, Inc. Pressure relief device assemblies
US20040255811A1 (en) * 2003-01-29 2004-12-23 Uwe Brede Pyromechanical separating element
US7188558B2 (en) * 2003-01-29 2007-03-13 Delphi Technologies, Inc Pyromechanical separating element
US7114427B1 (en) * 2005-10-19 2006-10-03 Special Devices, Inc. Quick-loosening mechanical linking device
US20110204177A1 (en) * 2010-02-25 2011-08-25 Pacific Scientific Energetic Materials Company Projectile diverter release and method of diverting a projectile
US11852181B1 (en) * 2021-08-30 2023-12-26 United States Of America, As Represented By The Secretary Of The Navy Separation bolt by eutectic decohesion

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