Patents Assigned to Daimler
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Patent number: 5570755Abstract: A system for the control of couplings in the locking mechanisms or differentials of a drive train in an all-wheel-drive vehicle is disclosed. The drive train of a vehicle having at least two drive axles (4.times.4 vehicle) comprises, starting from the engine and transmission block 1, a power take-off with switchable coupling 2, a front axle differential with locking coupling 3, a rear axle differential with locking coupling 5, steering angle sensor 10, rotational speed sensors 11, status sensors 12 and actuators 13, 14, 15. The rotational speed sensors 11 are installed in proximity to the wheels 4, 6. To be able to automatically switch all the couplings in keeping with terrain conditions, a control system 18 having individual modules (21,24,25) for each coupling (2,3,5) is provided. The control modules (24,25) of the hierarchically lower couplings (3,5) also emit control signals for one or several hierarchically higher coupling(s) (2,5) before they actuate their own couplings (3,5).Type: GrantFiled: August 10, 1994Date of Patent: November 5, 1996Assignee: Steyr-Daimler-Puch AGInventors: Gerhard J. Fruhwirth, Johann Deinhofer, Franz Stelzeneder, Gunter Pichlbauer, Johann Hager, Johan P. Reif
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Patent number: 5567546Abstract: 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.Type: GrantFiled: June 9, 1995Date of Patent: October 22, 1996Assignee: Daimler-Benz AGInventors: Martha Maly-Schreiber, Josef Michel
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Patent number: 5566832Abstract: 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.Type: GrantFiled: August 7, 1995Date of Patent: October 22, 1996Assignee: Daimler-Benz AGInventors: Bjorn Stuckrad, Karsten Lohr
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Patent number: 5566655Abstract: 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.Type: GrantFiled: October 20, 1995Date of Patent: October 22, 1996Assignee: Daimler-Benz AGInventors: Werner Rumez, Siegfried Sumser
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Patent number: 5566910Abstract: 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.Type: GrantFiled: October 12, 1994Date of Patent: October 22, 1996Assignee: Daimler-Benz Aerospace Airbus GmbHInventors: Thomas Diekmann, Norbert Geyer, Wilhelm Martens
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Patent number: 5565052Abstract: 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.Type: GrantFiled: September 2, 1994Date of Patent: October 15, 1996Assignees: Industrieanlagen-Betriebsgesellschaft GmbH, Daimler-Benz Aerospace AGInventors: Ulrich Papenburg, Ernst Blenninger, Peter Goedtke, Michael Deyerler
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Patent number: 5564649Abstract: 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.Type: GrantFiled: April 5, 1995Date of Patent: October 15, 1996Assignee: Daimler-Benz Aerospace AGInventors: Wolfgang von Hoessle, Ernst-August Seiffarth
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Patent number: 5563374Abstract: 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.Type: GrantFiled: June 22, 1994Date of Patent: October 8, 1996Assignee: Daimler-Benz Aerospace Airbus GmbHInventor: Andreas Hubert
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Patent number: 5561238Abstract: A method detects and evaluates emissions from plants, in particular from incineration or industrial plants. The absolute quantities of the pollutants are determined at preset intervals and an average over a preset measuring interval is formed therefrom. When a preset limiting average is exceeded, a check is made to determine whether this excess is due to a functional fault of the plant. If so, the plant is switched over to emergency running. If there is no functional fault, the running of the plant is restricted until the average falls again below the limiting average. The pollutant quantities determined are stored and can be utilized for determining levies.Type: GrantFiled: June 10, 1994Date of Patent: October 1, 1996Assignee: Daimler-Benz AtkiengesellschaftInventors: Werner Rumez, Siegfried Sumser
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Patent number: 5556332Abstract: Service panels such as passenger service panels in an aircraft or other passenger conveyance are equipped with fresh air outlets. The air outlets are connected to an air supply duct in such a way that the service panels can be adjusted in their position lengthwise relative to the longitudinal aircraft cabin axis. This purpose is accomplished by making the tap connection between the service panel and a fresh air supply duct adjustable in the axial direction along the air duct while maintaining the proper seal between a tap member and the air duct. The seal is maintained by providing the duct with a slot covered by at least one sealing lip and by providing the tap member with a sealing guide slide that adjustably seals the tap member in the duct.Type: GrantFiled: January 24, 1994Date of Patent: September 17, 1996Assignee: Daimler-Benz Aerospace Airbus GmbHInventor: Markus Schumacher
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Patent number: 5557520Abstract: A method for determining variables characterizing vehicle handling is provided, in particular the attitude angle. Signals of measured variables are fed to a computing device. At least the attitude angle is determined in the computing device using equations of motion and using a two-track model of the vehicle.Type: GrantFiled: July 29, 1994Date of Patent: September 17, 1996Assignee: Daimler-Benz AGInventors: Avshalom Suissa, Zoltan Zomotor, Friedrich Boettiger
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Patent number: 5549981Abstract: The invention relates to an electrochemical storage device having a plurality of serially connected individual cells, each of the individual cells having two spatially separated electrodes, between which an electrolyte and an intermediate part ensuring the spacing of the electrodes is arranged. In the interior of the storage device, each individual cell has a protective element which is formed from a solid material having a nonlinear current/voltage characteristic curve, and which makes electrical contact with the positive and the negative electrode within the individual cell and provides a voltage-dependent electrical connection between said electrodes. The electrical resistance of the protective element above a critical voltage is smaller, and below the critical voltage larger, than the resistance present between the electrodes at the respective voltages without the protective element.Type: GrantFiled: March 20, 1995Date of Patent: August 27, 1996Assignee: Daimler-Benz AGInventors: Martha Maly-Schreiber, Robert A. Huggins
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Patent number: 5548962Abstract: A refueling process for cryogenic liquids, in which the cryogenic liquid in question is transferred from a storage tank into a receiving tank via a detachable line connection. Before or during the refueling process, the cryogenic liquid is cooled in the storage tank to a temperature that is below the lowest operating temperature intended in the tank and above the freezing point of the liquid. The cryogenic liquid is transferred into the tank through a filter with a fineness of 5 to 40 .mu.m, and its temperature is increased during the transfer to a value that at least approximately corresponds to the intended operating temperature in the receiving tank.Type: GrantFiled: March 1, 1995Date of Patent: August 27, 1996Assignees: Daimler-Benz Aerospace AG, Tupolev AGInventors: Peter Luger, Franz Grafwalliner, Helmuth Peller, Martin Muller, Valentin V. Malyshev, Viacheslav P. Logviniouk, Vladmimir S. Ozeretskovsky, Alexander S. Shengardt
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Patent number: 5549187Abstract: A free-wheeling coupling sensitive to the direction of rotation for a motor vehicle comprises a first ring which constitutes a driving element in a towing mode of the motor vehicle, a second ring which constitutes a driven element in the towing mode, clamping elements which act between the first and second rings to transfer torque in both directions of torque flow, a cage in which the clamping elements are disposed, a fixed friction ring, and a friction element actively connecting the cage to the fixed friction ring. The friction element comprises a plurality of friction segments disposed between the cage and the fixed friction ring, the friction segments being slaved to rotate in the circumferential direction with the cage and being lifted away from the fixed friction ring by centrifugal force when they are caused to rotate at a rotational speed which is greater than a predetermined rotational speed.Type: GrantFiled: August 9, 1994Date of Patent: August 27, 1996Assignee: Steyr-Daimler-Puch AGInventor: Hansjorg Kofler
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Patent number: 5548536Abstract: The invention relates to a method for determining quantities which characterize driving behavior. Signals indicative of steering angle, longitudinal speed of the vehicle, and two transverse accelerations located one behind the other in the longitudinal direction of the vehicle, are fed to a computing device. The measured quantities are used to derive further quantities in the computing device using vehicle-specific quantities and a vehicle model. Furthermore, at least one of the further quantities is the sideslip angle or the yaw-angle velocity which are determined and output by the computing device.Type: GrantFiled: October 17, 1994Date of Patent: August 20, 1996Assignee: Daimler-Benz AgInventor: Dieter Ammon
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Patent number: 5547054Abstract: A free-wheeling coupling sensitive to the direction of rotation for a motor vehicle comprises a first ring which constitutes a driven element in a towing mode of the vehicle, a second ring which constitutes a driven element in the towing mode, clamping elements (e.g., rollers) which act between the first and second rings to transfer torque between them in both directions of torque flow, a cage in which the clamping elements are disposed, and a friction element acting between the cage and the second ring. The free-wheeling coupling further comprises a fixed switching ring, a cam rotatably mounted on the cage or the first ring, the cam including a control lever, and a spring which urges the control lever into engagement with the fixed switching ring until there is sufficient centrifugal force to lift the control lever out of engagement with the fixed switching ring.Type: GrantFiled: September 9, 1994Date of Patent: August 20, 1996Assignee: Steyr-Daimler-Puch AGInventor: Franz Gratzer
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Patent number: 5547526Abstract: A pressed explosive charge with high performance capacity and low sensitivity is formed of a pressable granular product. The pressable granular product has a high explosive content, preferably above 94% by weight and even more preferably above 96% by weight. The binder is a gel-like silicon rubber.Type: GrantFiled: April 21, 1994Date of Patent: August 20, 1996Assignee: Daimler-Benz Aerospace AGInventors: Paul Wanninger, Richard Wild, Ernst Kleinschmidt, Helmut Spath
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Patent number: 5547776Abstract: A fuel cell assembly within an electrochemical fuel cell stack has a cooling jacket disposed adjacent the cathode layer. The cooling layer comprises a coolant stream inlet, a coolant stream outlet, and at least one channel for directing a coolant stream from the coolant stream inlet to the coolant stream outlet. The coolant stream channels extend such that the coolest region of the cooling layer substantially coincides with the region of the adjacent cathode layer having the highest concentration of oxygen (and also the lowest water content), and the warmest region of the cooling layer substantially coincides with the region of the adjacent cathode layer having the lowest concentration of oxygen (and also the highest water content).Type: GrantFiled: June 24, 1994Date of Patent: August 20, 1996Assignees: Ballard Power Systems Inc., Daimler-Benz AGInventors: Nicholas J. Fletcher, Clarence Y. Chow, Eric G. Pow, Boguslav M. Wozniczka, Henry H. Voss, Gerald Hornburg
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Patent number: 5544589Abstract: An axially extending fragmentation warhead having a plurality of separate axially extending deformation charges in its radially outer surface. The deformation charges are located in a damping layer enclosing a fragmentation layer covering a cylindrical jacket enclosing a main explosive charge. The deformation charges facing a target can be individually ignited to inwardly deform the cylindrical jacket and the fragmentation layer prior to igniting the main explosive charge for selectively directing the fragmentation layer at the target. The deformation charges can be ignited individually or in selected groups to increase the effectiveness of the fragments directed at the target.Type: GrantFiled: December 2, 1992Date of Patent: August 13, 1996Assignee: Daimler-Benz Aerospace AGInventor: Manfred Held
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Patent number: 5538208Abstract: A single or twin spacer mounting permits the rapid and efficient installation of elongated elements for example in an aircraft. Such elements include, for example, electrical cable bundles, pipes, hoses, cables and the like, whereby these elongated elements must be maintained at a precise spacing from one another and/or from a support. Additionally, the elongated elements may need to be arranged at an angle relative to each other. For this purpose, substantially identical interlocking spacer mounting members are used. Each spacer mounting member has a saddle to which the elongated element is secured, for example, by a cable binder or hose clamp. The saddle is connected to an interlocking section that either includes a female plug-in socket or a male plug. In another embodiment interlocking pins with locking heads are used to hold two identical spacer mounting members to each other.Type: GrantFiled: February 24, 1994Date of Patent: July 23, 1996Assignee: Daimler-Benz Aerospace Airbus GmbHInventors: Rolf Cordes, Hermann Hinrichs, Werner Piede, Guy Rossini