US3209692A - Explosion transfer device - Google Patents

Explosion transfer device Download PDF

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US3209692A
US3209692A US401416A US40141664A US3209692A US 3209692 A US3209692 A US 3209692A US 401416 A US401416 A US 401416A US 40141664 A US40141664 A US 40141664A US 3209692 A US3209692 A US 3209692A
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input
charge
output
recess
face
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US401416A
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Webb George
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Avco Corp
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Avco Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42DBLASTING
    • F42D1/00Blasting methods or apparatus, e.g. loading or tamping
    • F42D1/04Arrangements for ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42DBLASTING
    • F42D1/00Blasting methods or apparatus, e.g. loading or tamping
    • F42D1/04Arrangements for ignition
    • F42D1/043Connectors for detonating cords and ignition tubes, e.g. Nonel tubes

Definitions

  • the present invention relates to explosion transfer devices, and particularly to those of the type which remain sealed during and after transmittal of an explosion.
  • the present invention provides a reliable means for the propagation of a detonation wave across a physical barrier without rupture of the explosion chamber.
  • the invention is of utility in such applications as gas generators, rocket motors, and fuzing systems.
  • a primary object of the invention is to provide a safe and reliable means of explosion transfer which maintains the isolation of the original charge.
  • Another object of the invention is to provide means, of the character described, which is adapted to use in multiple explosive relay systems which involve parallel relays, series relays, or combinations thereof.
  • the input and output charges and the sealed barrier therebetween are shaped in such manner that the input charge, operating mechanically across a rigid seal, ignites the output charge, while the seal maintains its integrity and continues to function as a seal.
  • FIGS. 1 and 2 are axial sectional views of a preferred embodiment and an alternate embodiment, respectively, of explosion transfer device in accordance with the invention.
  • FIG. 1 there is shown a preferred form of explosion transfer device in accordance with the invention. It comprises a generally cylindrical metallic housing formed to provide a first, or input, fitting, and a second, or output, fitting.
  • the input fitting is interiorly threaded, as indicated at 11, and the output fitting is similarly threaded, as indicated at 12, the fittings being aligned and the metallic housing 10 being formed as to provide a central wall 13 between them.
  • the output face of wall 13 is formed to define a recess or concavity 14, which is in communication with the input face via a channel 15.
  • An explosive input charge 16 is disposed in this recess.
  • a seal between input and output charges is formed by a metallic barrier member 17, which is a disk-like seal provided with a hollow central protuberance projecting into the input charge 16 and the recess 14. Disposed within this protuberance is an output charge 18.
  • the input charge is detonated by a series arrangement of means comprising a first, or input, fuse 19 and an input relay 20, the latter being disposed adjacent port 15.
  • the FIG. 1 combination further comprises means detonated by the output charge, and this means comprises a second relay 21 and a second fuse 22, the relay 21 being disposed between the output charge 18 and fuse 22.
  • a first plug 23 is formed concentrically to carry the elements 19 and 20, and is threaded into threads 11.
  • a second plug 24 is formed concentrically to carry the elements 21 and 22, and it projects into the second fitting, being threaded onto the threads 12.
  • O-rings 25 and 26 are suitably positioned in frontal annular shoulders formed on the faces of the plugs 23 and 24, respectively, to gas-tightly seal the peripheries of the plugs.
  • the mild detonation fuse 19 initiates relay 20, so that the high explosive input charge 16 is detonated, slightly compressing the barrier 17.
  • the output charge 18, contained within the protuberance of the barrier member, is pinched under the increased pressure generated by the detonation of the input charge. Accordingly, the output charge is detonated.
  • Output charge 18 initiates relay 21, and mild detonation of fuse 22 continues propagation through the system. Gas generated forward of the output face is barred from rearward flow by barrier member 17, and O-ring 26 is located at a point where distortion of the barrier member is at a minimum.
  • FIG. 2 there is illustrated an alternate embodiment of the invention having a cone-shaped protuberance on the barrier.
  • reference numerals identical with those of FIG. 1 are utilized to refer to identical elements, and reference numerals primed refer to similar elements.
  • the output charge is placed in a generally conically shaped projecting portion of the barrier 17'.
  • the angle is such that the charge 18' is placed in compression by detonation of the input charge 16, which is located in a complementary and generally conically shaped recess 14 in housing 10.
  • the inventive combination is in essence a form of relay, a form which is readily miniaturized and which readily lends itself to use in multiple sequence.
  • a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face; an input charge disposed in said recess; a metallic barrier member formed as a disk-like seal having a hollow walled protuberance projecting into said input charge and said recess; and an output charge within said protuberance.
  • An explosion transfer device which remains sealed during and after high energy transfer, comprising:
  • a generally cylindrical metallic housing formed to provide first and second aligned screw-threaded fittings having a central wall therebetween, said central Wall having input and output faces, the output face of said central wall being formed to define a recess which is in communication with the input face;
  • a metallic barrier member formed as a disk-like seal having a hollow central protuberance projecting into said input charge and said recess;
  • means for detonating said input charge comprising a first fuse and a first relay disposed between the input face and said fuse;
  • means detonated by said output charge comprising a second fuse and a second relay disposed between said output charge and said second fuse;
  • a first plug formed concentrically to carry said first fuse and relay and threaded into the first of said fittings
  • a second plug formed concentrically to carry said second fuse and relay and projecting into the second of said fittings to press said barrier member against said output face;
  • An explosion transfer device which remains sealed during and after high energy transfer, comprising:
  • a generally cylindrical metallic housing formed to provide first and second aligned fittings having a central wall therebetween, said central wall having input 1% and output faces, the output face of said central wall being formed to define a concavity which is in communication with the input face, said concavity and said housing having a common central longitudinal axis;
  • a single metallic barrier member formed as a disk-like seal having a hollow central continuous projection extending axially into said input charge and said concavity;
  • a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face, said recess and said divider having a common central longitudinal axis;
  • a single metallic barrier member formed as a disk-like seal having a hollow walled central continuous protuberance projecting axially into said input charge and said recess;
  • a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face, said recess and said divider having a common central longitudinal axis;
  • a single metallic barrier member formed as a seal having a hollow walled central continuous protuberance projecting axially into said input charge and said recess;
  • An explosion transfer device which remains sealed during and after high energy transfer, comprising:
  • a generally cylindrical metallic housing formed to provide first and second aligned fittings having a central wall therebetween, said central wall having input and output faces, the output face of said central wall being formed to define a recess which is in communication with the input face, said recess and said housing having a common central longitudinal axis;
  • a single metallic barrier member formed as a disk-like seal having a hollow central continuous protuberance projecting axially into said input charge and said recess;
  • means for detonating said input charge comprising a first fuse and a first relay disposed between the input face and said fuse;
  • said output charge being under initial pressure and responsive to pinching of said protuberance to be set off;
  • means detonated by said output charge comprising a second fuse and a second relay disposed between said output charge and said second fuse;
  • first plug means formed to carry said first fuse and relay and projecting into the first of said fittings; and a second plug means formed to carry said second fuse and relay and projecting into the second of said fittings to press said barrier member against said output face.

Description

Oct. 5, 1965 G. WEBB EXPLOSION TRANSFER DEVICE Filed Oct. 5, 1964 INVENTOR.
GEORGE WEBB BY 44 flQ M ATTORNEYS.
United States Patent 3,209,692 EXPLOSION TRANSFER DEVICE George Webb, Richmond, Ind., assignor to Avco Corporation, Richmond, Ind, a corporation of Delaware Filed Oct. 5, 1964, Ser. No. 401,416 5 Claims. (Cl. 102--70) The present invention relates to explosion transfer devices, and particularly to those of the type which remain sealed during and after transmittal of an explosion. The present invention provides a reliable means for the propagation of a detonation wave across a physical barrier without rupture of the explosion chamber. The invention is of utility in such applications as gas generators, rocket motors, and fuzing systems.
A primary object of the invention is to provide a safe and reliable means of explosion transfer which maintains the isolation of the original charge.
Another object of the invention is to provide means, of the character described, which is adapted to use in multiple explosive relay systems which involve parallel relays, series relays, or combinations thereof.
In accordance with the invention, the input and output charges and the sealed barrier therebetween are shaped in such manner that the input charge, operating mechanically across a rigid seal, ignites the output charge, while the seal maintains its integrity and continues to function as a seal.
For a better understanding of the invention, together with other and further objects, advantages, and capabilities thereof, reference is made to the following description of the appended drawings, in which:
FIGS. 1 and 2 are axial sectional views of a preferred embodiment and an alternate embodiment, respectively, of explosion transfer device in accordance with the invention.
Referring now to FIG. 1, there is shown a preferred form of explosion transfer device in accordance with the invention. It comprises a generally cylindrical metallic housing formed to provide a first, or input, fitting, and a second, or output, fitting. The input fitting is interiorly threaded, as indicated at 11, and the output fitting is similarly threaded, as indicated at 12, the fittings being aligned and the metallic housing 10 being formed as to provide a central wall 13 between them. The output face of wall 13 is formed to define a recess or concavity 14, which is in communication with the input face via a channel 15. An explosive input charge 16 is disposed in this recess. A seal between input and output charges is formed by a metallic barrier member 17, which is a disk-like seal provided with a hollow central protuberance projecting into the input charge 16 and the recess 14. Disposed within this protuberance is an output charge 18. The input charge is detonated by a series arrangement of means comprising a first, or input, fuse 19 and an input relay 20, the latter being disposed adjacent port 15. The FIG. 1 combination further comprises means detonated by the output charge, and this means comprises a second relay 21 and a second fuse 22, the relay 21 being disposed between the output charge 18 and fuse 22.
A first plug 23 is formed concentrically to carry the elements 19 and 20, and is threaded into threads 11. A second plug 24 is formed concentrically to carry the elements 21 and 22, and it projects into the second fitting, being threaded onto the threads 12. O- rings 25 and 26 are suitably positioned in frontal annular shoulders formed on the faces of the plugs 23 and 24, respectively, to gas-tightly seal the peripheries of the plugs.
The mild detonation fuse 19 initiates relay 20, so that the high explosive input charge 16 is detonated, slightly compressing the barrier 17. The output charge 18, contained within the protuberance of the barrier member, is pinched under the increased pressure generated by the detonation of the input charge. Accordingly, the output charge is detonated. Output charge 18 initiates relay 21, and mild detonation of fuse 22 continues propagation through the system. Gas generated forward of the output face is barred from rearward flow by barrier member 17, and O-ring 26 is located at a point where distortion of the barrier member is at a minimum.
In FIG. 2 there is illustrated an alternate embodiment of the invention having a cone-shaped protuberance on the barrier. In FIG. 2 reference numerals identical with those of FIG. 1 are utilized to refer to identical elements, and reference numerals primed refer to similar elements.
In FIG. 2 the output charge is placed in a generally conically shaped projecting portion of the barrier 17'. The angle is such that the charge 18' is placed in compression by detonation of the input charge 16, which is located in a complementary and generally conically shaped recess 14 in housing 10.
The inventive combination is in essence a form of relay, a form which is readily miniaturized and which readily lends itself to use in multiple sequence.
It will be understood that, in accordance with the invention, there has been provided the combination of a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face; an input charge disposed in said recess; a metallic barrier member formed as a disk-like seal having a hollow walled protuberance projecting into said input charge and said recess; and an output charge within said protuberance.
While there have been shown and described what are at present considered to be the preferred embodiments of the invention, it will be understood by those skilled in the art that various changes and modifications may be made therein without departing from the scope of the invention as defined by the appended claims.
1 claim: 1. An explosion transfer device which remains sealed during and after high energy transfer, comprising:
a generally cylindrical metallic housing formed to provide first and second aligned screw-threaded fittings having a central wall therebetween, said central Wall having input and output faces, the output face of said central wall being formed to define a recess which is in communication with the input face;
an input charge disposed in said recess;
a metallic barrier member formed as a disk-like seal having a hollow central protuberance projecting into said input charge and said recess;
an output charge within said protuberance;
means for detonating said input charge, comprising a first fuse and a first relay disposed between the input face and said fuse;
means detonated by said output charge, comprising a second fuse and a second relay disposed between said output charge and said second fuse;
a first plug formed concentrically to carry said first fuse and relay and threaded into the first of said fittings;
a second plug formed concentrically to carry said second fuse and relay and projecting into the second of said fittings to press said barrier member against said output face;
and O-ring means for gas-tightly sealing the peripheries of said plugs.
2. An explosion transfer device which remains sealed during and after high energy transfer, comprising:
a generally cylindrical metallic housing formed to provide first and second aligned fittings having a central wall therebetween, said central wall having input 1% and output faces, the output face of said central wall being formed to define a concavity which is in communication with the input face, said concavity and said housing having a common central longitudinal axis;
an input charge disposed in said concavity;
a single metallic barrier member formed as a disk-like seal having a hollow central continuous projection extending axially into said input charge and said concavity;
an output charge within said projection;
means for detonating said input charge;
means detonated by said output charge;
a first plug formed to carry said detonating means and secured into the first of said fittings;
and a second plug formed to carry said detonated means and secured into the second of said fittings to press said barrier member against said output face.
3. In an explosion transfer device which remains sealed during and after high energy transfer, the combination of:
a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face, said recess and said divider having a common central longitudinal axis;
an input charge disposed in said recess;
a single metallic barrier member formed as a disk-like seal having a hollow walled central continuous protuberance projecting axially into said input charge and said recess;
and an output charge within said protuberance.
4. In an explosion transfer device which remains sealed during and after high energy transfer, the combination of:
a divider having input and output faces, the output face being formed to define a recess which is in communication with the input face, said recess and said divider having a common central longitudinal axis;
an input charge disposed in said recess;
a single metallic barrier member formed as a seal having a hollow walled central continuous protuberance projecting axially into said input charge and said recess;
an output charge within said protuberance;
means for detonating said input charge;
and means detonated by said output charge.
5. An explosion transfer device which remains sealed during and after high energy transfer, comprising:
a generally cylindrical metallic housing formed to provide first and second aligned fittings having a central wall therebetween, said central wall having input and output faces, the output face of said central wall being formed to define a recess which is in communication with the input face, said recess and said housing having a common central longitudinal axis;
an input charge disposed in said recess;
a single metallic barrier member formed as a disk-like seal having a hollow central continuous protuberance projecting axially into said input charge and said recess;
an output charge within said protuberance;
means for detonating said input charge, comprising a first fuse and a first relay disposed between the input face and said fuse;
said output charge being under initial pressure and responsive to pinching of said protuberance to be set off;
means detonated by said output charge, comprising a second fuse and a second relay disposed between said output charge and said second fuse;
a first plug means formed to carry said first fuse and relay and projecting into the first of said fittings; and a second plug means formed to carry said second fuse and relay and projecting into the second of said fittings to press said barrier member against said output face.
References Cited by the Examiner UNITED STATES PATENTS 2,601,245 6/52 Bowersett 1027O 2,707,438 5/55 Mann et a1 l0227 2,736,263 2/56 Lewis et a1. l0227 SAMUEL FEINBERG, Primary Examiner.
BENJAMIN A. BORCHELT, Examiner.

Claims (1)

  1. 3. IN AN EXPLOSION TRANSFER DEVICE WHIC REMAINS SEALED DURING AND AFTER HIGH ENERGY TRANSFER, THE COMBINATION OF: A DIVIDER HAVING INPUT AND OUTPUT FACES, THE OUTPUT FACE BEING FORMED TO DEFINE A RECESS WHICH IS IN COMMUNICATION WITH THE INPUT FACE, SAID RECESS AND SAID DIVIDER HAVING A COMMON CENTRAL LONGITUDINAL AXIS; AN INPUT CHARGE DISPOSED IN SAID RECESS; A SINGLE METALLIC BARRIER MEMBER FORMED AS A DISK-LIKE SEAL HAVING A HOLLOW WALLED CENTRAL CONTINUOUS PROTUBERANCE PROJECTING AXIALLY INTO SAID INPUT CHARGE AND SAID RECESS; AND AN OUTPUT CHARGE WITHIN SAID PROTUBERANCE.
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Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3351011A (en) * 1966-09-07 1967-11-07 Louis J Montesi Detonator
US3352236A (en) * 1966-03-28 1967-11-14 George W Baker Explosive energy transfer means
US3460477A (en) * 1967-12-26 1969-08-12 Explosive Tech One-way detonation transfer device and assembly
US3678853A (en) * 1970-06-12 1972-07-25 Us Navy Quick disconnect explosive connector assembly
US3688702A (en) * 1969-08-12 1972-09-05 Dynamit Nobel Ag Detonator device for explosive charge exhibiting detonating effect capable of bridging gap between spaced charges
US3789764A (en) * 1973-02-20 1974-02-05 Us Navy Explosive lead plug
US3893395A (en) * 1965-07-26 1975-07-08 Us Navy End coupler for heat resistant mild detonating fuse
US3982488A (en) * 1975-02-19 1976-09-28 The United States Of America As Represented By The Secretary Of The Army Flueric through bulkhead rocket motor ignitor
US4033267A (en) * 1976-10-01 1977-07-05 The United States Of America As Represented By The Secretary Of The Navy Flueric cartridge initiator
US4272102A (en) * 1978-08-07 1981-06-09 Explosive Technology, Inc. Coupling device for ignitive reactions
US4301707A (en) * 1979-10-29 1981-11-24 Mcdonnell Douglas Corporation Embedded explosive severance of non-metallic materials
US4592281A (en) * 1982-07-29 1986-06-03 Special Devices, Inc. Arming and firing device
US4608926A (en) * 1984-09-13 1986-09-02 Thiokol Corporation Swivel type through bulkhead initiator
US4653400A (en) * 1985-07-03 1987-03-31 The United States Of America As Represented By The Secretary Of The Army Two component thru-bulkhead initiator
US4850438A (en) * 1984-04-27 1989-07-25 Halliburton Company Modular perforating gun
US4920883A (en) * 1989-01-27 1990-05-01 Halliburton Logging Services, Inc. Detonation transfer methods and apparatus
US4938141A (en) * 1989-06-19 1990-07-03 Honeywell Inc. Shock initiator device for initiating a percussion primer
US5036588A (en) * 1989-10-02 1991-08-06 The United States Of America As Represented By The Secretary Of The Navy Nonvolatile, fast response wire cutter
US6662883B2 (en) 2001-09-07 2003-12-16 Lri Oil Tools Inc. Charge tube assembly for a perforating gun
US7987787B1 (en) * 2007-03-07 2011-08-02 Ensign-Bickford Aerospace & Defense Company Electronic ignition safety device configured to reject signals below a predetermined ‘all-fire voltage’
US8622149B2 (en) 2010-07-06 2014-01-07 Schlumberger Technology Corporation Ballistic transfer delay device
US20150144399A1 (en) * 2012-04-24 2015-05-28 Fike Corporation Energy transfer device
US10844696B2 (en) 2018-07-17 2020-11-24 DynaEnergetics Europe GmbH Positioning device for shaped charges in a perforating gun module
US11021923B2 (en) 2018-04-27 2021-06-01 DynaEnergetics Europe GmbH Detonation activated wireline release tool
US11480038B2 (en) 2019-12-17 2022-10-25 DynaEnergetics Europe GmbH Modular perforating gun system
US11753889B1 (en) 2022-07-13 2023-09-12 DynaEnergetics Europe GmbH Gas driven wireline release tool
US11808093B2 (en) 2018-07-17 2023-11-07 DynaEnergetics Europe GmbH Oriented perforating system
USD1010758S1 (en) 2019-02-11 2024-01-09 DynaEnergetics Europe GmbH Gun body
USD1019709S1 (en) 2019-02-11 2024-03-26 DynaEnergetics Europe GmbH Charge holder
US11946728B2 (en) 2019-12-10 2024-04-02 DynaEnergetics Europe GmbH Initiator head with circuit board

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Publication number Priority date Publication date Assignee Title
US2601245A (en) * 1948-01-30 1952-06-24 Charles F Bowersett Underwater signaling device
US2707438A (en) * 1954-05-26 1955-05-03 Canadian Ind 1954 Ltd Short interval delay blasting device
US2736263A (en) * 1956-02-28 Blasting explosive device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736263A (en) * 1956-02-28 Blasting explosive device
US2601245A (en) * 1948-01-30 1952-06-24 Charles F Bowersett Underwater signaling device
US2707438A (en) * 1954-05-26 1955-05-03 Canadian Ind 1954 Ltd Short interval delay blasting device

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893395A (en) * 1965-07-26 1975-07-08 Us Navy End coupler for heat resistant mild detonating fuse
US3352236A (en) * 1966-03-28 1967-11-14 George W Baker Explosive energy transfer means
US3351011A (en) * 1966-09-07 1967-11-07 Louis J Montesi Detonator
US3460477A (en) * 1967-12-26 1969-08-12 Explosive Tech One-way detonation transfer device and assembly
US3688702A (en) * 1969-08-12 1972-09-05 Dynamit Nobel Ag Detonator device for explosive charge exhibiting detonating effect capable of bridging gap between spaced charges
US3678853A (en) * 1970-06-12 1972-07-25 Us Navy Quick disconnect explosive connector assembly
US3789764A (en) * 1973-02-20 1974-02-05 Us Navy Explosive lead plug
US3982488A (en) * 1975-02-19 1976-09-28 The United States Of America As Represented By The Secretary Of The Army Flueric through bulkhead rocket motor ignitor
US4033267A (en) * 1976-10-01 1977-07-05 The United States Of America As Represented By The Secretary Of The Navy Flueric cartridge initiator
US4272102A (en) * 1978-08-07 1981-06-09 Explosive Technology, Inc. Coupling device for ignitive reactions
US4301707A (en) * 1979-10-29 1981-11-24 Mcdonnell Douglas Corporation Embedded explosive severance of non-metallic materials
US4592281A (en) * 1982-07-29 1986-06-03 Special Devices, Inc. Arming and firing device
US4850438A (en) * 1984-04-27 1989-07-25 Halliburton Company Modular perforating gun
US4608926A (en) * 1984-09-13 1986-09-02 Thiokol Corporation Swivel type through bulkhead initiator
US4653400A (en) * 1985-07-03 1987-03-31 The United States Of America As Represented By The Secretary Of The Army Two component thru-bulkhead initiator
US4920883A (en) * 1989-01-27 1990-05-01 Halliburton Logging Services, Inc. Detonation transfer methods and apparatus
US4938141A (en) * 1989-06-19 1990-07-03 Honeywell Inc. Shock initiator device for initiating a percussion primer
US5036588A (en) * 1989-10-02 1991-08-06 The United States Of America As Represented By The Secretary Of The Navy Nonvolatile, fast response wire cutter
US6662883B2 (en) 2001-09-07 2003-12-16 Lri Oil Tools Inc. Charge tube assembly for a perforating gun
US7987787B1 (en) * 2007-03-07 2011-08-02 Ensign-Bickford Aerospace & Defense Company Electronic ignition safety device configured to reject signals below a predetermined ‘all-fire voltage’
US8622149B2 (en) 2010-07-06 2014-01-07 Schlumberger Technology Corporation Ballistic transfer delay device
US20150144399A1 (en) * 2012-04-24 2015-05-28 Fike Corporation Energy transfer device
US9476686B2 (en) * 2012-04-24 2016-10-25 Fike Corporation Device for transferring energy output from one pyrotechnic device to another
US9963398B2 (en) 2012-04-24 2018-05-08 Fike Corporation Energy transfer device
US11021923B2 (en) 2018-04-27 2021-06-01 DynaEnergetics Europe GmbH Detonation activated wireline release tool
US11634956B2 (en) 2018-04-27 2023-04-25 DynaEnergetics Europe GmbH Detonation activated wireline release tool
US11339632B2 (en) 2018-07-17 2022-05-24 DynaEnergetics Europe GmbH Unibody gun housing, tool string incorporating same, and method of assembly
US10920543B2 (en) 2018-07-17 2021-02-16 DynaEnergetics Europe GmbH Single charge perforating gun
US11525344B2 (en) 2018-07-17 2022-12-13 DynaEnergetics Europe GmbH Perforating gun module with monolithic shaped charge positioning device
US10844696B2 (en) 2018-07-17 2020-11-24 DynaEnergetics Europe GmbH Positioning device for shaped charges in a perforating gun module
US11773698B2 (en) 2018-07-17 2023-10-03 DynaEnergetics Europe GmbH Shaped charge holder and perforating gun
US11808093B2 (en) 2018-07-17 2023-11-07 DynaEnergetics Europe GmbH Oriented perforating system
USD1010758S1 (en) 2019-02-11 2024-01-09 DynaEnergetics Europe GmbH Gun body
USD1019709S1 (en) 2019-02-11 2024-03-26 DynaEnergetics Europe GmbH Charge holder
US11946728B2 (en) 2019-12-10 2024-04-02 DynaEnergetics Europe GmbH Initiator head with circuit board
US11480038B2 (en) 2019-12-17 2022-10-25 DynaEnergetics Europe GmbH Modular perforating gun system
US11753889B1 (en) 2022-07-13 2023-09-12 DynaEnergetics Europe GmbH Gas driven wireline release tool

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