Abstract: Apparatus for trajectory control and/or position control of a missile (99), comprising a controllable gas generator (109, 200) with a fuel flow control valve (124, 213), an injector head (112, 202), a combustion chamber (111) and at least one outflow nozzle (103, 204) or at least one throttle.

Abstract: The invention relates to a device for burning off propellants or explosive substances, which has an activation temperature that lies below the spontaneous ignition temperature of the propellant or explosive substance. The device (1) comprises at least two substances (5, 6) reacting exothermically with one another, wherein at least one first substance (5) is present in a liquid aggregate state below the activation temperature of the device and is separated from at least one second substance (6) by at least one pressure-tight barrier (7).

Abstract: Missile having a jet engine (2) comprising at least one turbine (3) and at least one compressing means (4), wherein gas generated in at least one gas generator (7) of the missile (1) drives a turbine (3). The compressing means (4) and the turbine (3) are arranged opposite to the flight direction (6) adjacent to each other.

Abstract: A method for suppressing developing explosions, in particular in containers or rooms with explosive dusts or gases, having a gas generator whose pressure gas expels the extinguishing agent from its container as a unit after a maximum pressure is reached and then distributes it as a cloud of extinguishing dust to the side and forwards so as to fill the space.

Abstract: An extinguisher includes a compressed-gas generator for fighting fire and incipient explosions, and the extinguisher includes at least one rupture diaphragm having a rupture joint, in order to seal the extinguishing-agent vessel. In its center, the rupture diaphragm has a planar surface or a depression, which causes the rupture joint to simultaneously open at its entire circumference, in order for the extinguishing agent to escape in an axially symmetric manner.

Abstract: A fire extinguisher includes a compressed gas generator for fighting fires and nascent explosions, and has two bursting membranes with predetermined breaking points for closing the fire extinguishing material container. The predetermined breaking points of the bursting membranes are designed with differences in resistance in order to achieve a time delay between the breaking occurrences of the two predetermined breaking points. This time delay ensures a non-deformed and rotationally symmetrical expulsion of the fire extinguishing material.

Abstract: The invention concerns a tubular gas generator for the filling of an airbag in a retention system for occupants of motor vehicles, whereby two separate combustion chamber units have a common connector and each combustion chamber unit has an ignitor unit with respective filters.

Abstract: A gas generator (10) which generates propellant gas for inflating a gas bag in an air bag system comprises a housing (11) having a combustion chamber (21) which is formed by an upper part (12) of the housing and a lower part (13) of the housing in the interior of the housing (11), discharge openings (32) in the housing (11) for the exit of the propellant gas from the housing (11) into the gas bag, a filter device (30) upstream of the discharge openings (32) and an ignition device (23) for igniting a solid propellant (22) contained in the combustion chamber (21), the propellant gas escaping from the combustion chamber (21) being directed out of the housing (11) via flow chambers (29).

Abstract: A gas generator for passive restraint systems in motor vehicles. The generator includes a lower shell part having a cylindrical inner wall and a cylindrical outer wall coaxial with the cylindrical inner wall, the lower shell part further including first mechanical latch elements disposed on each of its inner wall and outer wall. An upper shell part of the gas generator has a cylindrical inner wall and a cylindrical outer wall coaxial with the cylindrical inner wall, the upper shell part further including second mechanical latch elements disposed on each of its inner wall and outer wall. The upper shell part is assembled with the lower shell part such that the first mechanical latch elements and the second mechanical latch elements are latched to one another.

Abstract: A method for non-invasively monitoring a pressure of a compressed gas inside a closed container includes: forming a magnetic circuit through a portion of the outside wall of the container; detecting magnetic flux amplitude changes in the magnetic circuit created by a transient stress in the outside wall of the container; producing data representing the magnetic flux amplitude changes; and monitoring pressure changes from a nominal pressure by evaluating the data representing the magnetic flux amplitude changes.

Abstract: Solid-propellant rocket engine with a combustion chamber, with a thrust nozzle, with one or more grains in the combustion chamber, at least one of which comprises two parts, namely, an inner burner part and an outer burner part, wherein the latter is connected to a support structure, has a cross section changing over its length, is accommodated in the hollow space of identical shape of the inner burner part, and is axially displaceable. A thermal barrier is arranged at the nozzle-side end of the two-part grain. The outer burner part is fitted gap-free into the inner burner part. The contour formed by the contact surfaces of the two grain parts encloses a cross section expanding from the front to the rear. The outer burner part can be moved from a front, inactive position, which is positive-locking with the inner burner part, into a rear, active position with a defined flow gap between the contact surfaces of the grains.

Abstract: Gas generators for passive restraint systems in motor vehicles, particularly for airbag systems or belt pre-tensioner systems, contain a gas generating compound which is ignited by an electrical ignition unit. The present ignition unit makes do with a small number of individual components and does not employ a plug. The connecting devices carrying the electrical ignition pulse are connected directly to the ignition charge without the intermediate circuitry of a plug, and the ignition carrier is formed as an enclosure for the connecting devices.

Abstract: A device for disconnecting the flow of current in the positive or impregnated battery cable of a motor vehicle has an electrically conductive plug-in connection that can be placed in the positive or impregnated battery cable in the form of a housing and a plug connector. The housing contains a gas generator of the kind used, for example, for belt tighteners. The gas generator is arranged in the housing in such a way that the propellant gas produced when the gas generator is ignited electrically separates the connector from the housing and this in turn interrupts the flow of current in the positive or impregnated battery cable. Consequently, a short circuit that might occur in the event of an accident and which could otherwise lead to damage of the cable tree and then set the vehicle on fire, is avoided in good time.

Abstract: Gas generator for a safety system for the protection of occupants of motor vehicles, with a tubular or cylindrical housing, wherein the gas-generating solid propellant is contained in a combustion chamber within which volume-equalizing structure is arranged, surrounding the propellant, both in the direction of flow--along the principal axis--and peripherally over the entire circumference.

Abstract: A hybrid gas generator for vehicle safety, systems, in particular airbag inflating and seat belt tensioning systems or pyrotechnical isolating switches for disconnecting the vehicle electrical system from the vehicle battery in the event of an impact accident, is described, whereby a moving piston is provided to destroy the bursting diaphragm which closes off the compressed gas container. This piston is moved towards the bursting diaphragm by igniting an ignition system whereby according to this invention the piston has a flange-shaped projection which is located against a shoulder on the internal surface of a sleeve facing the piston and is designed such that when the ignition system is ignited the flange-shaped projection shears off. Advantageously, the operating pressure in the combustion chamber of the hybrid gas generator according to this invention can thus be determined by the area of the shearing surface on the flange-shaped projection.

Abstract: A hybrid gas generator includes a pyrotechnic gas generator joined to a high-pressure vessel which is sealed with a sealing disk composed of a substance which chemically reacts with propellant gas produced in use so that the sealing disk is opened with an advantageously reduced acoustic pressure. The propellant gas is chemically reactive and is produced from a propellant composition which is present in a surplus amount and which is composed of a propellant which is oxidizable and at least one oxidant for oxidizing the propellant. The propellant gas attacks the sealing disk chemically and thermally, and continuously burns through it to release the gas from the high-pressure vessel into a mixing chamber in the pyrotechnic gas generator.

Abstract: Gas generator for an airbag that provides protection against side impact in a vehicle. The gas generator has a housing with a flange for attaching the gas generator to a part of the vehicle, in particular to the backrest of a vehicle seat, and for fixing the airbag. The gas generator also has a sealed fluid-tight propellant tank that acts as combustion chamber. The propellant tank is arranged concentrically in the housing such that an annular chamber is formed between the housing and the propellant tank to allow afterburning. The annular chamber can be connected on the one hand to the inside of the propellant tank through the passage that opens as a result of the burning process and on the other hand to the inside of the airbag through the outlet apertures provided in the housing wall, but otherwise it is sealed fluid-tight. The construction of the generator is therefore very simple and it is of very small size.

Abstract: A gas-generating mixture for an air bag, which has a rate of burnoff exceeding 40 mm/sec and good ignitability, but leads to a relatively low combustion temperature. The mixture is formed of an alkali or alkaline earth azide as the principal component, a metal oxide as the oxidizing agent and slag-forming agent, and 5 to 23 wt. % of an accelerator consisting of a metal nitrate and silicon dioxide, wherein the ratio of the metal nitrate to the silicon dioxide ranges from 4:1 to 1:4, and the silicon dioxide content is at least 4 wt. % of the mixture.

Abstract: Gas generator system of lightweight design, especially of an impact protection system for occupants of vehicles, containing a central area with an igniter for a combustion chamber enclosing the igniter for solid propellant, which combustion chamber in turn is enclosed by a filter chamber with discharge openings for inflating a downstream receiver, containing, in combination: a housing, consisting of an upper part and a lower part, which are screwed together, and which accommodate and hold between them the igniter, the propellant, and the filter, so that they are sealed tightly and in a pressure-proof manner from the outside, and that one of the two housing parts that can be connected to one another has an approximately mushroom-shaped cross section, as well as special filter designs and brackets for holding same during screwing together, and the selected ducting for the flow of the gas generated.

Abstract: The subject invention concerns a propellant mixture for producing propellant gas for passenger protection systems in motor vehicles, in particular airbag systems. According to this invention, this propellant mixture comprises fumaric acid, with a share of 20 to 45% by weight, as well as an inorganic oxidant with a share of 55 to 80% by weight. These revealed propellant components are non-toxic and characterized by a high thermal stability as well as low hygroscopicity. In addition, this propellant contains only minor traces of pollutant gases, with even combustion residues being non-toxic.