A method can include forming a mixture of an explosive and a thermally conductive material; disposing at least a portion of the mixture in a chamber of a capsule; and at least partially sealing the chamber.

A method can include forming a mixture of an explosive and a thermally conductive material; disposing at least a portion of the mixture in a chamber of a capsule; and at least partially sealing the chamber.

An igniter assembly including, an igniter, a metal collar arranged around the igniter, and a resin joining portion, the collar including, a joining surface portion having an annular surface covered with the resin joining portion, a first joining groove opened in the annular surface and including a first inner circumferential edge that has a first corner portion formed on the entire circumference of the first inner circumferential edge, and a second joining groove opened in an inner wall surface of the first joining groove and including a second inner circumferential edge that has a second corner portion formed on the entire circumference of the second inner circumferential edge, and the joined state being established when the resin joining portion enters the first joining groove and the second joining groove in a state in which the resin joining portion presses the first corner portion and the second corner portion.

A capacitive discharge unit for a fireset for initiating a fuzing event to detonate an explosive material. The capacitive discharge unit includes a capacitor for storing a voltage, and a silicon carbide thyristor for switching from a high to a low impedance state in response to a triggering pulse, which results in electrical current flowing from the capacitor to the fuzing load. The fireset may further include a controller for providing the triggering pulse to the silicon carbide thyristor. The capacitor stores between 500 V and 1200 V, and the silicon carbide thyristor has a rise time of between 78 ns and 141 ns. The capacitive discharge unit may further include a silicon carbide diode, in the form of a reverse current blocking diode or a Schottkey diode, functioning as a shunt to prevent a reverse current from passing through the switching silicon carbide thyristor.

A capacitive discharge unit for a fireset for initiating a fuzing event to detonate an explosive material. The capacitive discharge unit includes a capacitor for storing a voltage, and a silicon carbide thyristor for switching from a high to a low impedance state in response to a triggering pulse, which results in electrical current flowing from the capacitor to the fuzing load. The fireset may further include a controller for providing the triggering pulse to the silicon carbide thyristor. The capacitor stores between 500 V and 1200 V, and the silicon carbide thyristor has a rise time of between 78 ns and 141 ns. The capacitive discharge unit may further include a silicon carbide diode, in the form of a reverse current blocking diode or a Schottkey diode, functioning as a shunt to prevent a reverse current from passing through the switching silicon carbide thyristor.

The present development includes a non-explosive, programmable electronic initiation system, whose objective is to initiate rock blasting in a controlled and safe manner. Its application is mainly in the area of Mining and Civil Works. This system solves a sensitive issue in the industry, such as the non-activation of the devices at the time of blasting (shots left behind) and reduces the risks of operation in the fragmentation work, providing continuity to field work. The above is based on the fact that this system allows precise operation times for vibration control, through previously defined delays, immediately identifying non-operational initiators due to line or connection failures; since there are no explosive components, they can be programmed remotely if so required by the user; finally, each initiator is programmed to be unique and unrepeatable.

A tubing conveying perforating system with a firing head is provided, and a method for using the same is provided. The firing head includes a firing pin and a percussion initiator. The firing pin is configured to degrade over a predetermined period of time from an initial state to a degraded state, and in the degraded state the firing head is inoperable.

A tubing conveying perforating system with a firing head is provided, and a method for using the same is provided. The firing head includes a firing pin and a percussion initiator. The firing pin is configured to degrade over a predetermined period of time from an initial state to a degraded state, and in the degraded state the firing head is inoperable.

A detonation system for a perforating gun assembly. The detonation system includes a tandem sub having a first end and a second opposing end. Each of the first and second ends is connected to a respective perforating gun. The tandem sub has an inner bore, and a switch housing residing within the inner bore. The tandem sub also has an addressable switch residing within the switch housing with the switch being configured to receive instruction signals from a surface by means of an electric line. The addressable switch is in communication with a signal transmission pin and a detonator pin. The detonator pin sends a detonation signal from the addressable switch to a detonator in an adjacent perforating gun. The wiring connections for the pins may be pre-assembled before the perforating guns are delivered to the field. The detonation system utilizes a carrier end plate, wherein the end plate and pins seal off the tandem sub from wellbore fluids and debris following detonation of explosive charges in an associated perforating gun.

A selectable force gas generator (SFGG) includes support material of honeycomb structure and a gas collection chamber contained in a housing. Gas-generating propellant cells are partially embedded in the support material. Each of the gas-generating propellant cells includes a steel jacket having a convex portion exposed to the gas collection chamber. The steel jacket has an orifice through the convex portion. Each propellant cell includes a propellant packet contained in the jacket. Each propellant cell includes a fire wire electrically connectable to an electrically-fired initiator and electrically connected to the propellant packet. The fire wire transmits a firing signal that causes the propellant packet to produce gas. A cap is positioned between the propellant packet and the jacket. The cap has a tip that blocks the orifice of the jacket and the thickness of the jacket is sufficient to prevent sympathetic detonation of the propellant packet.