Schieferdecker
Adriaan Schieferdecker, Harrisburg, NC US
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20140358590 | TRACKING EROSION OF AGGREGATE LIMITS - Systems, methods and apparatuses for tracking erosion of insurance funds available in an aggregate environment are provided. In some examples, insurance policy information may be received and aggregated by coverage type into subject-oriented insurance segments. Within the subject-oriented insurance segments the various policies for that coverage type may be represented as policy segments. When a claim is made, the claim may be paid out of a policy segment that spans multiple coverage types and thus multiple subject-oriented insurance segments. The system may track these claims and reduce the amount of insurance available for each subject-oriented insurance segment associated with the policy segment from which the claim is being made. | 12-04-2014 |
Ina Schieferdecker, Zepernick DE
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20090319830 | System and Method for Automatically Testing a Model - A system for automatically testing a model of system under test includes (a) means for the automatic generation of a test harness; (b) means for automatic generation of test specifications based on the analysis of the results obtained from the simulation of the test harness; (c) means for the automatic generation of test data and test controls; (d) means for automatic evaluation of the test quality and the automatic generation of a verdict. A method for automatically testing a model system includes (a) detecting at least one feature of an input signal to the model system and (b) detecting at least one feature of an output signal of the model system, wherein the at least one feature of the input signal or the input signal is generated automatically depending on at least one feature of the at least one output signal. | 12-24-2009 |
Joerg Schieferdecker, Dresden DE
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20080216883 | Thermopile Infrared Sensor Array - A thermopile infrared sensor array, comprises a sensor chip with a number of thermopile sensor elements, made from a semiconductor substrate and corresponding electronic components. The sensor chip is mounted on a support circuit board and enclosed by a cap in which a lens is arranged. The aim is the production of a monolithic infrared sensor array with a high thermal resolution capacity with a small chip size and which may be economically produced. The aim is achieved by arranging a thin membrane made from non-conducting material on the semiconductor substrate of the sensor chip on which the thermopile sensor elements are located in an array. Under each thermopile sensor element, the back side of the membrane is uncovered in a honeycomb pattern by etching and the electronic components are arranged in the boundary region of the sensor chip. An individual pre-amplifier with a subsequent low-pass filter may be provided for each column and each row of sensor elements. | 09-11-2008 |
20110174978 | THERMOPILE INFRARED SENSOR BY MONOLITHIC SILICON MICROMACHINING - A thermal infrared sensor is provided in a housing with optics and a chip with thermoelements on a membrane. The membrane spans a frame-shaped support body that is a good heat conductor, and the support body has vertical or approximately vertical walls. The object is to provide a thermopile infrared sensor in monolithic silicon micromachining technology, wherein the infrared sensor has a high thermal resolution capacity with a small chip size, a high degree of filling and a high response rate. The thermopile sensor structure consists of a few long thermoelements per sensor cell. The thermoelements being arranged on connecting webs that connect together hot contacts on an absorber layer to cold contacts of the thermoelements. The membrane is suspended by one or more connecting webs and has, on both sides of the long thermoelements, narrow slits that separate the connecting webs from both the central region and also the support body. At least the central region is covered by the absorber layer. | 07-21-2011 |
Patrick Schieferdecker, Buehl DE
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20130179030 | METHOD FOR DETERMINING WEAR OF A FRICTION PLATE - Method for determining wear of a friction plate of an automatically actuated friction clutch, particularly in a motor vehicle driven by an internal combustion engine, wherein initially at a prescribed clutch slip and a prescribed clutch torque in an earlier friction lining test point an earlier clutch actuation travel is determined and stored, later again at the prescribed clutch slip and the prescribed clutch torque in a later friction lining test point a later clutch actuation travel is determined, thereafter the earlier clutch actuation travel and the later clutch actuation travel are compared to each other and a differential value is determined, and thereafter a friction lining wear is determined using the differential value, in order to reliably determine friction lining wear in a time interval and with only little effort, so that a depreciation of function due to a worn friction lining can be prevented in a timely manner. | 07-11-2013 |
Scott A. Schieferdecker, O'Fallon, MO US
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20090171490 | IDENTIFICATION OF ENGINEERING INTENT REQUIREMENTS IN AN ELECTRONIC ENVIRONMENT - Engineering requirements are defined in an electronic environment. In one embodiment, a method includes providing at least one of a set of master requirements and a set of version requirements to be applied to the electronic product definition, and referencing an electronic reference document from at least one of the set of master requirements and the set of version requirements, the electronic reference document including one or more particular engineering requirements to be applied to the electronic product definition. Alternately, a method includes defining a callout linked to the at least one of the set of master requirements and the set of version requirements, the callout being adapted to supersede a conflicting engineering requirement set forth in at least one of the set of master requirements and the set of version requirements. | 07-02-2009 |
20110172795 | CONSIDERATION OF MANUFACTURING CAPABILITY DURING AIRCRAFT DESIGN - A system comprises a configurator for providing a configuration definition that specifies existing engineering designs and manufacturing capability of aircraft structures that have already been designed and manufactured; and a processor for accessing the configuration definition from the configurator and filtering the configuration definition according to customer specifications for a new aircraft. The filtering selects existing designs and identifies existing manufacturing capability to fabricate structures for the new aircraft. | 07-14-2011 |