JEFFREY R. WHITE, MD
Marriage and Family Therapists at Lidgerwood St, Spokane, WA

7772953, Aug 10, 2010

Dec 16, 2008

12/336457

Jian Huang - Everett WA, US
Jeffrey J. White - Shoreline WA, US

The Boeing Company - Chicago IL

H01F 30/12, H02M 7/06

336 5, 336 12, 363 5

Various embodiments of multi-phase transformers are disclosed. Exemplary transformer includes primary windings, secondary windings and third windings. Primary windings, secondary windings and third windings may include sub windings coupled to form functions. Primary windings are coupled at ends to form a delta configurations. Secondary windings are coupled to primary windings. Third windings are coupled to primary windings and secondary windings. Secondary windings and the third windings are magnetically coupled to primary windings. The outputs at second ends of third windings are greater than the outputs at the second ends of secondary windings. In some embodiments, the outputs at adjacent second ends of the third windings are substantially equal. In some embodiments, the phase angle difference of outputs at adjacent second ends of third windings are substantially equal. In some embodiments, the phase angle difference of outputs at adjacent second ends of secondary windings are substantial equal.

2013014, Jun 13, 2013

Dec 9, 2011

13/315555

Eugene V. Solodovnik - Lake Stevens WA, US
Jeffrey J. White - Shoreline WA, US

THE BOEING COMPANY - Chicago IL

H02H 3/00, B60L 1/00, H02P 3/02

318454, 361 18, 307 91

An apparatus and method for protecting a power system comprising a generator providing power to an alternating current bus, a power converter for converting alternating current power on the alternating current bus to direct current power on a direct current bus, and a direct current load powered by the direct current power on the direct current bus. An undesired condition is identified at the input to the power converter from the alternating current bus. The undesired condition is caused by at least one of the power converter, the direct current bus, or the load. The power converter is disconnected from the alternating current bus in response to identifying the undesired condition for at least a time delay. The time delay is selected such that the power converter is disconnected from the alternating current bus before the alternating current bus is disconnected from the generator due to the undesired condition.

8432059, Apr 30, 2013

Feb 13, 2012

13/371859

Benjamin D. Waite - Seattle WA, US
Jeffrey J. White - Shoreline WA, US
Warren A. Atkey - Bothell WA, US

The Boeing Company - Chicago IL

G05B 15/00

307 91, 700291, 700295

In one embodiment, a method is used to provide dynamic electrical power management which may minimize the potential for overload conditions and may ensure that system performance limits are maintained. The method may dynamically limit the primary load system power draw in response to the net power draw of all other electrical power users on the aircraft which may ensure that the total power levels remain below critical limits. The method may also provide predictive controls to handle rapid load transients. Additionally, if vital functions are not being met, the method may shed other selected aircraft electrical loads which may ensure that adequate power is provided to the primary load system.

8237308, Aug 7, 2012

Dec 12, 2007

11/954480

Warren A. Atkey - Bothell WA, US
Benjamin D. Waite - Seattle WA, US
Jeffrey J. White - Shoreline WA, US

The Boeing Company - Chicago IL

H02J 3/14

307 31, 700295

In one embodiment, a method is used to provide dynamic electrical power management which may minimize the potential for overload conditions and may ensure that system performance limits are maintained. The method may dynamically limit the primary load system power draw in response to the net power draw of all other electrical power users on the aircraft which may ensure that the total power levels remain below critical limits. The method may also provide predictive controls to handle rapid load transients. Additionally, if vital functions are not being met, the method may shed other selected aircraft electrical loads which may ensure that adequate power is provided to the primary load system.

2014002, Jan 23, 2014

Sep 23, 2013

14/033722

Jeffrey J. White - Shoreline WA, US

The Boeing Company - Chicago IL

H01F 27/34

336 73

According to an embodiment, a transformer is provided that includes a first conductive coil wound about a first coil axis and a second conductive coil wound about a second coil axis. The second conductive coil is disposed proximate to the first conductive coil and the second coil axis is substantially parallel to the first coil axis. A closed-loop conductive winding is disposed proximate to the first conductive coil and the second conductive coil. The closed-loop conductive winding is wound about a loop axis at least one time where the loop axis is substantially parallel to the first coil axis and the second coil axis.

2013009, Apr 11, 2013

Apr 9, 2012

13/442298

Timothy T. Gray - Seattle WA, US
Jeffrey A. White - Seattle WA, US
Aaron Michael Donsbach - Seattle WA, US
Mark R. Privett - Seattle WA, US

Amazon Technologies, Inc. - Reno NV

G06F 3/033, G06F 3/048

715810

A device can display content on a page associated with a dimension. A user can adjust an orientation of the device to adjust a displayed orientation of the page, enabling pages for additional dimensions to be displayed. A user can select one of these dimensions, and adjust an orientation of the device to enable the user to access content for the selected dimension. The change in orientation can be a tilt or flick of the device in a first direction to select a dimension, and then a user could tilt or flick the device in another direction to view pages, sub-dimensions, or other groupings of content among that dimension. Such an approach can enable a user to quickly locate content corresponding to a sub-dimension without having to scroll down a long page of content or otherwise manually navigate to specific content.

7513119, Apr 7, 2009

Feb 3, 2005

11/051272

Edward Zielinski - Seattle WA, US
Alan T. Bernier - Seattle WA, US
Kent W. Knechtel - Seattle WA, US
Thomas A. Campbell - Seattle WA, US
Jeffrey J. White - Seattle WA, US
Mark D. Ralston - Seattle WA, US

The Boeing Company - Chicago IL

F02C 7/22, B63H 11/00

60778, 60204

Methods and systems for starting aircraft turbofan engines are disclosed. A system in accordance with one embodiment includes an electrically-powered starter motor coupled to a turbofan engine to provide power to the turbofan engine during an engine start procedure. The system can further include an on-board, deployable, ram air driven turbine coupled to an electrical generator, which is in turn coupled to the starter motor to provide electrical power to the starter motor. In other embodiments, the ram air driven turbine can be replaced with a fuel cell or a battery. In still further embodiments, a single controller can control operation of both the engine starter and other motors of the aircraft.

8155876, Apr 10, 2012

Sep 7, 2006

11/518379

Jeffrey J. White - Shoreline WA, US
David K. Toy - Marysville WA, US
J. Everett Groat - Snohomish WA, US

The Boeing Company - Chicago IL

B64C 13/38

701300, 318432

Systems and methods for controlling aircraft electrical power are disclosed. A system in accordance with one embodiment includes an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to vary an output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes, with individual controller modes corresponding to an operation mode of the aircraft and a non-zero output level of the electric motor. In further embodiments, motor controllers can be substituted for each other, e. g. , in the event one motor controller becomes unoperational.