Murer
David Murer, Zurich CH
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20140264058 | Method for Obtaining Information Signatures from Nuclear Material or About the Presence, the Nature and/or the Shielding of a Nuclear Material and Measurement Setup for Performing Such Method - The invention relates to a method for obtaining information or signatures about the presence or the nature of a nuclear radiation source, especially in a homeland security application, said nuclear radiation source emitting in a time or angle correlated manner at least a first radiation and a second radiation. The method includes the steps of detecting said first radiation with at least one first radiation detector and detecting said second radiation with at least one second radiation detector. The detection of said second radiation is triggered by said detection of said first radiation in a manner that is adapted to the radiation's correlation structure, thereby increasing the signal-to-background ratio for the detection of said second radiation. | 09-18-2014 |
20140361186 | Method for Detecting and Identifying Nuclear Material in a Container and Radiation Monitoring Arrangement for Conducting the Method - The invention relates to an improved method for detecting and possibly identifying and/or characterizing nuclear and/or radiological material in a container, vehicle, or on a person, comprising the steps of: a. providing at least one detector, which is capable of detecting radiation events being interrelated to nuclear or radiological material; b. bringing the at least one detector in the vicinity of the container, vehicle or person to be monitored; c. detecting radiation events being interrelated to the container, vehicle or person to be monitored; d. assigning each detected radiation event an individual time stamp in order to generate a time pattern of the detected radiation events; and e. analyzing the time pattern with respect to time correlation structures in order to identify a presence and/or characteristics of the nuclear or radiological material. | 12-11-2014 |
Kenneth H. Murer, Chesterfield, MO US
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20130211306 | BUOYANCY-BASED CERVICAL TRACTION SYSTEM - A buoyancy-based cervical traction system has a floatation and a head rest supported by the flotation system. The head rest is adapted to support a person's head above the neck and apply traction to the neck when the person is in a body of liquid. The system has a position adjustment system adapted to allow selective adjustment of the position at which the person's head rest will be relative to an upper surface of the liquid when the person and the cervical traction system are in the liquid, the person's head is supported by the head rest, and the cervical traction system and person are floating in the liquid at equilibrium. | 08-15-2013 |
Kevin Murer, Basel CH
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20150096132 | Anthraquinone Azo Dyes - The present invention relates to azo dyes of the formula (1), wherein R | 04-09-2015 |
Peter Murer, Allschwil CH
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20080286693 | Sulfonate derivatives and the use thereof as latent acids - Chemically amplified photoresist compositions comprising, | 11-20-2008 |
20090042114 | Halogenated oxime derivatives and the use therof as latent acids - Compounds of the formula I or II | 02-12-2009 |
Peter Murer, Oberwill CH
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20090309068 | NOVEL ELECTROLUMINESCENT POLYMERS FOR ELECTRONIC APPLICATIONS - The present invention relates to novel polymers comprising a repeating unit(s) of the formula (I) wherein at least one of the substituents R | 12-17-2009 |
Peter Murer, Obervil DE
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20120168731 | PHENANTHROAZOLE COMPOUNDS AS HOLE TRANSPORTING MATERIALS FOR ELECTRO LUMINESCENT DEVICES - The present invention relates to electroluminescent devices, comprising a compound of the formula (I) as a component of the transporting/injecting and/or electron blocking layer. The compounds of formula (I) may function alone, or in combination with dopants to provide improved efficiency, driving voltage and/or lifetime of electroluminescent devices. | 07-05-2012 |
Sascha Murer, Steinhausen CH
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20100068429 | METHOD OF MANUFACTURING A REFERENCE ELECTRODE - A method of manufacturing a reference electrode which has a shaft into which a diaphragm body of a porous ceramic is incorporated is comprised of the following method steps: Impregnating the ceramic with a lyogel precursor prior to incorporating the ceramic body into the shaft, and subsequently transforming the lyogel precursor into a lyogel, from which the solvent is removed through a drying process. A reference electrode has a shaft that is filled with electrolyte, and a diaphragm body formed of a porous ceramic and containing a system of hollow spaces is incorporated into the wall of the shaft. The system of hollow spaces is filled at least partially with a material that is formed of a lyogel by drying and has at least one component that corresponds to the ceramic material. | 03-18-2010 |
Stefan Murer, Beckenried CH
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20100058582 | METHOD AND DEVICE FOR THE APPLICATION OF AN ELONGATED CONDUCTOR TO A SOLAR ELEMENT - A method and device for the application of an elongated electric conductor to a solar element wherein the required length of the elongated electric conductor is readied and the conductor is strained through application of a tensile stress. The conductor is then fastened to the solar element. Straining of the elongated electric conductor is monitored to prevent exceeding of a tensile limit. During fastening onto the solar element at least one press-on roller is employed. | 03-11-2010 |
Yann Murer, Saint-Jean FR
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20100071881 | COOLING SYSTEM FOR AIRCRAFT ELECTRIC OR ELECTRONIC DEVICES - A cooling system for cooling the electrical or electronic equipment on board an aircraft is equipped with a main closed circuit. A pump circulates a heat transfer medium through the main closed circuit. A main heat exchanger is thermally coupled with the heat transfer medium. A secondary heat exchanger allows direct thermal coupling of the heat transfer medium to air on the outside of the aircraft. A bypass valve located upstream from the secondary heat exchanger allows to block, at least partially, the circulation of the heat transfer medium towards the secondary heat exchanger. A bypass duct connects the bypass valve to a point on the main closed cooling circuit downstream from the secondary heat exchanger to bypass, at least partially, the heat transfer medium towards the main heat exchanger as a function of a setting of the bypass valve. | 03-25-2010 |
20100084118 | COOLING SYSTEM FOR AIRCRAFT ELECTRIC OR ELECTRONIC DEVICES - In a cooling system for the electrical or electronic equipment on board an aircraft, a heat transfer medium circulates through a main closed cooling circuit. A liquid coolant circulates through a secondary closed cooling circuit. A first heat exchanger makes it possible to transfer the heat from the heat transfer medium circulating through the main closed cooling circuit to the liquid coolant circulating through the secondary closed cooling circuit, by evaporation of the liquid coolant circulating through the secondary closed cooling circuit. A second heat exchanger makes possible the condensation of the liquid coolant circulating through the secondary closed cooling circuit. The second heat exchanger cools the liquid coolant by thermal coupling to the outside ambient air. | 04-08-2010 |
20110108662 | ATTACHMENT PYLON FOR AN AIRCRAFT TURBO-SHAFT ENGINE WITH CONCENTRIC HOT AIR CHANNELS - The invention relates to a pylon ( | 05-12-2011 |