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Manfred
Baumgartner Manfred, Berlin DE
| Patent application number | Description | Published |
|---|---|---|
| 20090185177 | Apparatus and method for the inspection of the surface of a component - An apparatus for inspection of a surface of a component includes a probing device ( | 07-23-2009 |
Kirchberger Manfred, Prambachkirchen AT
| Patent application number | Description | Published |
|---|---|---|
| 20090169907 | EXTRUSION COATED SUBSTRATE - Certain embodiments provide an article comprising a substrate, wherein the substrate is extrusion coated with a composition comprising a multi-branched polypropylene having a g′ of less than 1.00. In certain embodiments, the substrate is extrusion coated with a composition comprising a polypropylene material. Either the composition and/or the polypropylene material are represented by the equation: | 07-02-2009 |
Mark Manfred, Edina, MN US
| Patent application number | Description | Published |
|---|---|---|
| 20090216391 | INERTIAL SIGNALS FOR FLIGHT CONTROL BACKUP MODE - A flight control system is provided that includes a reference system and flight control actuators. The reference system includes one or more sets of gyroscopes and accelerometers. At least one set of the gyroscopes and accelerometers are configured to provide a first output of a first set inertial signals for normal mode flight control and second output of a second different set of inertial signals for backup mode flight control. The flight control actuators are configured to be controlled by one of the first set of inertial signals and the second set of inertial signals. | 08-27-2009 |
Mark T. Manfred, Edina, MN US
| Patent application number | Description | Published |
|---|---|---|
| 20100152929 | SYSTEMS AND METHODS OF REDUNDANCY FOR AIRCRAFT INERTIAL SIGNAL DATA - An aircraft inertial system comprises at least two inertial reference units (IRU) that provide a first set of inertial signal data for an aircraft and at least two attitude heading reference systems (AHRS) that provide a second set of the inertial signal data for the aircraft. At least one primary flight display receives the first and the second sets of the inertial signal data, and a standby flight display receives at least the second set of the inertial signal data from at least one of the AHRS. When a single fault condition occurs, the primary flight display continues to operate with fail-operational redundancy from at least three independent sources of the inertial signal data comprising one or more IRU and AHRS combinations. The standby flight display will operate using a different source of the inertial signal data than the source of the inertial signal data for the primary flight display. | 06-17-2010 |