Abstract: A process for preparing a bipolar transistor for very high frequencies is described, which is especially advantageous for the preparation of heterobipolar transistors and leads to components with low parasitic capacities and low base lead resistance. The process includes forming a structured first layer with collector zone and insulation areas surrounding the collector zone on a monocrystalline lead layer. A series of monocrystalline transistor layers are grown on the first layer over the collector zone by differential epitaxy and a series of polycrystalline layers is grown at the same time over the insulation areas. A series of polycrystalline layers is designed as a base lead.

Abstract: A process and apparatus for the selective catalyzed NO.sub.x reduction in oxygen-containing exhaust gases of internal-combustion engines. For improving the reduction of nitric oxides, hydrocarbons and air are supplied to the exhaust gas purifier and, for producing reactive short-chained unsaturated hydrocarbons, a defined quantity of fuel from the stored fuel intended for the fuel supply of the internal-combustion engine is catalytically cracked and is oxidized by the simultaneous supply of air. The resulting species are guided into the exhaust gas flow of the exhaust gases which are to be purified.

Abstract: A field-effect-controlled semiconductor device has a cathode, an anode, and a gate, and extends laterally on a first insulating layer covering a substrate. The device includes a main thyristor, a MOSFET switch and a diode which connects a highly doped region embedded in a first part of a second base region of the thyristor to the cathode of the device.

Abstract: The invention relates to a gasoline engine having a catalyst for reducing the emission pollutants, with an oxygen absorption device located in the exhaust line upstream of the catalyst. According to the invention, the gasoline engine is operated in a first operating range with a lean air/fuel ratio (.lambda.), and oxygen is removed from the exhaust by the absorption device. In a second operating range, the gasoline engine is operated at .lambda.=1, and the absorption device is bypassed or deactivated. In the case of a gasoline engine with a Denox catalyst the gasoline engine is operated constantly with a lean air/fuel ratio, with the active surface of the Denox catalyst being "depoisoned" temporarily by activating the oxygen absorption device.

Abstract: An intercept device for flying objects is formed of a lightweight, small-volume, packable structure made of a tear-resistant, pliable material, which can be stretched to a large, two-dimensional or three-dimensional expansion by means of a deployment device. To reduce the velocity of the intercepted flying objects, activatable, aerodynamic resistance bodies are incorporated into the structure. To end the intercept procedure, elements are integrated into the structure, which consist of material that can be destroyed from outside by means of high-energy beams and/or chemical reagents, or that destroys itself, or the structure as a whole consists of such material.

Abstract: A device with a pyrotechnic gas generator wherein gas pressurizes a hydraulic circuit via a cartridge-case base, a spring and a pressure piston. The pyrotechnic gas generator comprises a propellant charge, which is located in a combustion chamber and is ignited by an electronic igniting unit. The parts of the device are contained in a housing, which is exchangeably inserted into a wall surrounding the hydraulic circuit.

Abstract: The invention provides a catalyst, and a process for preparing the same, for the catalytic reduction of NO.sub.x and for the oxidation of hydrocarbons. The catalyst contains a copper oxide-zinc oxide-aluminum oxide spinel and a zeolitic support material.

Abstract: A semiconductor structure having one or a plurality of lateral, high-blocking semiconductor components in a semiconductor of a metalized substrate (2), a dielectric layer (3) contiguous to the substrate, a homogeneously doped drift zone (4) disposed above the dielectric layer, and having heavily-doped zones of the semiconductor components which are formed in or extend into the drift zone and are electrically contacted. At least the zones (5, 6) of the semiconductor components, which can have a high potential difference with respect to the substrate during operational functioning mode of the semiconductor components, extend up to the dielectric layer (3).

Abstract: A separation wall for dividing a cabin space inside a passenger aircraft is constructed of two wall elements rigidly connected to each other in an overlap area. The transition between the overlap area and a respective wall portion of the corresponding wall element is formed by an off-set (27B, 28B; 31B, 32B). The off-sets may slant in the same direction or in opposite directions. The wall elements have lateral edges facing either an aisle in the aircraft cabin or an aircraft body wall. For this purpose the respective lateral edge tapers or curves upwardly to accommodate the aisle or the curvature of the body wall. The overlap area provides an improved strength and wall extensions (28D or 31D) form a space (19) for storage of items or mounting of equipment.

Abstract: A process for stripping of used parts or reject parts, in particular of polycarbonate (PC) or of a polycarbonate blend, preferably with polybutylene terephthalate (PBT/PC), for the purpose of recycling the plastic. In this process the plastics parts are first mechanically comminuted to a pourable size and then are circulated together with anhydrous alkalified diethylene glycol or propylene glycol in a mass with mutual abrasion of the plastics chips at elevated temperatures of at least 50.degree. C., preferably from 80.degree. to 100.degree. C., until complete removal of the paint. Thereafter the stripped plastics chips are separated from the stripping agent, flushed and then dried. The quantity of glycol added corresponds to from 1 to 10% of the volume of the mass to be treated, so that the circulated parts are only wetted by the glycol, but with stripping agent being circulated continuously through the treatment space of the mass from a relatively large reservoir.

Abstract: An apparatus for locking an aircraft door provided in the outer wall of an aircraft includes at least one locking shaft pin that locks the aircraft door in a fixed, closed position relative to the outer wall of the aircraft when the locking shaft pin is positioned or rotated into a locking position. The locking shaft pin is connected to a mechanical linkage forming a positioning arrangement. The positioning arrangement is coupled to a control element, which essentially includes a membrane connected to a control rod. The membrane is arranged within a housing so as to form an interior air chamber on one side of the membrane and an exterior air chamber on the other side of the membrane. The air pressure of the cabin interior is applied to the interior air chamber through an interior air pressure port, and the exterior ambient air pressure is applied to the exterior air chamber through an exterior air pressure port.

Abstract: In a method for the ejection and distribution of submunition bodies to be ejected from a submunition carrier for combatting targets in a line, such as vehicle columns, the submunition carrier (3) comprises vertical ejecting tubes (3a) for the submunition bodies, which vertical ejecting tubes (3a) are directed downward as well as upward. Submunition bodies (7) which are connected with a wind sock for stabilization are ejected downward. The submunition bodies (9) which are to be ejected in an upward direction are connected with a parachute which is provided with at least one eccentric slot.

Abstract: Fastening of a thermal protection structure on the airframe of a craft such as a spaceplane, rocket, missile, re-entry capsule, or any hypersonic airplane wherein the thermal protection structure consists of a plurality of highly heat-resistant, mechanically stable panels, which may be provided with an additional gap seal if desired, with a plurality of fastening points per panel, which are arranged at spaced locations from one another and establish a positive-locking connection between the insulation structure and the airframe. The fastening has a first fastening point, which does not permit any movement, or it does permit an at least limited rotary movement of the panel around an axis extending at right angles to the airframe surface; a second fastening point, which permits a limited, linear displacement of the panel in parallel to the airframe surface; and at least one additional fastening point, which permits a limited displacement of the panel in all directions.

Abstract: An ion conductor for electrochemical cells, comprising an alkali metal salt or a mixture of alkali metal salts, and mixed therewith on oligomer and/or polymer (hereinafter referred to simply as "polymers"), having at least one phosphazene base unit. The polymers are chemically stable with respect to the constituents of the ion conductor, and have an inorganic atom or an inorganic compound positioned at the phosphorous atom of at least one phosphazene base unit thereof. To form the ion conductor the alkali metal salts are heated to the melting temperature and the alkali metal salts, preferably fused to a low viscosity state, are admixed with the polymers which are dissolved in the alkali metal salt melt.

Abstract: A wing gap closure flap is positioned in an aircraft wing so that a gap between the wing structure and the leading edge of a landing flap can be closed during normal cruising positions of the landing flap and opened when the landing flap is in a starting position or in a landing position. The gap is formed on the underside of the aircraft wing and the gap closure flap is operated by a positioning shaft which itself is driven through a drive lever linkage by the drive shaft for the landing flap. The wing gap closure flap is connected through a lever mechanism to the positioning shaft which is preferably divided into shaft sections where a plurality of wing gap closure flaps are used. Each shaft section is driven by the landing flap drive shaft. A defined motion of the wing gap closure flap or flaps is achieved in that the positioning of the wing gap closure flaps is synchronized in a limited angular range with the positioning of the landing flap by the cooperation of the respective drive mechanisms.

Abstract: In a method and system for controlling the flow of fluid through the intake duct of an internal combustion engine of which the exhaust gas is measured and its composition compared with values desired for minimum fuel consumption and minimum emission values and the flow of additional fluid supplied to the intake duct is controlled depending on a characteristic diagram, the mass flow and flow profiles are varied depending on the characteristic diagram by controlled injection of the additional flow into the intake duct and by controlled removal of gas from the intake duct.

Abstract: A method for separating plastic particles by types from a particle mixture of plastics of different types by flotation. The plastic particles are initially processed by a type-dependent change in their wetting behavior in such a manner that the various types can be floated individually out of the particle mixture. This surface treatment of the plastic particles takes place prior to flotation and outside of the flotation device in a physically dry manner by plasma processing of the particle mixture followed by storage for a predetermined time period. Storage results in a material-specific classification wetting behavior.

Abstract: In order to produce lightweight mirror structures or other reflecting components, preformed silicon elements of sufficient wall thickness are applied to a CFC or CMC substrate structure with the dimensions of the component to be produced, at a temperature in the range 1300.degree. C. and 1600.degree. C. either in vacuum or in a protective atmosphere. In this way a mirror structure or reflector is formed directly. It is possible to work at temperatures in the range of 300.degree. C. to 600.degree. C. when the silicon is applied in the form of a preform such as a wafer, which is joined to the substrate by way of a zone of a melt eutectic incorporating a nonferrous metal, which is preferably gold. The surfaces are subsequently coated.

Abstract: The invention provides an apparatus for the remote control of missiles or torpedoes launched from a launching container, by means of a cable of which a portion is wound onto a supply reel connected with the launching and of which the other portion is wound onto a supply reel in the missile or the torpedo. The supply reel in the launching container is arranged on the forward end of the container, and the supply reel in the missile or torpedo is arranged on the rearward end of the missile or torpedo. The cable section between the two supply reels, before the launching of the missile or torpedo, is fastened along the major portion of its length on the interior wall of the launching container, by means of a gluing arrangement which consists of a material whose combustion temperature is at least by 800.degree. C. lower than the melting temperature of the optical waveguide, or by means of a flexible clamping arrangement whose holding force can be adjusted.

Abstract: A flexible pipe coupling is constructed for flexibly interconnecting pipe sections especially in a vacuum toilet system on board an aircraft. For this purpose each coupling member of a pair forming the coupling has a bushing for connection to a pipe end by a hose clamp, a flange integrally connected to the bushing, and a support ring for backing the respective flange but permitting the flange to retain a certain flexibility. Each support ring has a conical circumferential rim. The coupling also includes a clamp member encircling with radially inwardly facing conical surfaces the radially outwardly facing conical rim of both support rings to clamp the coupling members together. The clamp member has a threaded or snap device for applying the clamping force.