Stephen A White

20020153129, Oct 24, 2002

Apr 25, 2000

09/557347

Stephen White - Whittier CA, US
Brian Naumann - Redwood City CA, US

F28D001/02

165/152000

A plate-fin heat exchanger includes a plurality of integral fin passages and a plurality of fins. Each fin is located between and bonded to outer surfaces of adjacent integral fin passages. Each integral fin passage has integrally formed plates and extended surfaces. The integral fin passages may be formed by extrusion.

58606254, Jan 19, 1999

Dec 30, 1996

8/827875

Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA

The Boeing Company - Seattle WA

B64C 1700
G05D 100

244195

An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

54528658, Sep 26, 1995

Jun 28, 1993

8/086447

Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA

The Boeing Company - Seattle WA

B64C 1316
G05D 100
G06G 770

244 75A

An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

58331735, Nov 10, 1998

Oct 8, 1996

8/731043

Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA

The Boeing Company - Seattle WA

B64C 1316
G05D 108

244 75A

An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

56671660, Sep 16, 1997

Feb 13, 1996

8/600779

Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA

The Boeing Company - Seattle WA

B64C 1300
B64C 1316

244 76C

An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

20220365665, Nov 17, 2022

May 14, 2021

17/321050

- Redmond WA, US
Rachel SIRKIN - Seattle WA, US
Aaron E. ERLANDSON - Kirkland WA, US
Yoon Jin LEE - Woodinville WA, US
Stephen WHITE - Grand Rapids MI, US
Erin GREENLY - Seattle WA, US
Evan W. LAVENDER - Redmond WA, US

Microsoft Technology Licensing, LLC - Redmond WA

G06F 3/0484
G06Q 10/10
G06F 3/0485

A computer-implemented method for implementing a map calendar graphical user interface (GUI) including content-variable view levels is described herein. The method includes executing a map calendar application to provide a map calendar GUI surfaced on a display. The map calendar GUI includes interactive visualizations of a map calendar that are organized into content-variable view levels that relate to specific units of time. The method also includes displaying, via the surfaced map calendar GUI, interactive visualizations of different content-variable view levels such that non-level-specific calendar content items are displayed with respect to all content-variable view levels that encompass the time fragments corresponding to the non-level-specific calendar content items, while level-specific calendar content items are only displayed with respect to one or more content-variable view levels to which the level-specific calendar content items have been specifically linked, as determined by one or more user inputs.

20220366376, Nov 17, 2022

May 14, 2021

17/320991

- Redmond WA, US
Rachel SIRKIN - Seattle WA, US
Aaron E. ERLANDSON - Kirkland WA, US
Stephen WHITE - Grand Rapids MI, US
Erin GREENLY - Seattle WA, US
Evan W. LAVENDER - Redmond WA, US
Yoon Jin LEE - Woodinville WA, US
Ilya GREYSUKH - Bellevue WA, US
Eugene AHN - Newcastle WA, US

Microsoft Technology Licensing, LLC - Redmond WA

G06Q 10/10
G06F 3/0481
G06F 3/0482
G06F 3/0485

A computer-implemented method for implementing a map calendar application and corresponding map calendar GUI that provide time mold functionality is described herein. The method includes executing the map calendar application to provide the map calendar GUI surfaced on a display. The map calendar GUI includes an interactive visualization of a map calendar, which includes a continuous, manipulable sequence of calendar content data corresponding to calendar content items that are organized based on units of time within a coordinate plane. The method also includes categorizing the calendar content items based on time categories corresponding to the calendar content items and identifying time patterns corresponding to the categorized calendar content items. The method further includes generating a time mold of the map calendar based on the identified time patterns and visually overlaying the time mold onto corresponding calendar content items within the interactive visualization.

20220239199, Jul 28, 2022

Jun 7, 2021

17/340982

- Charlotte NC, US
Robert A. Dietrich - Montebello CA, US
Evgeni Ganev - Torrance CA, US
Stephen L. White - Whittier CA, US

Honeywell International Inc. - Charlotte NC

H02K 9/22
H02K 5/20
H02K 11/33
H02K 21/14
B64D 27/24
B64D 35/02

In one embodiment, an advanced electric propulsion system comprises: a housing; an electric motor within the housing; a motor drive coupled to the motor; a thermal management system comprising: a manifold-mini-channel heat sink integrated into the housing, the manifold-mini-channel heat sink comprises: an inlet manifold having air inlets formed in front of the housing; a set of plurality of circumferentially grooved micro-channels formed in the housing and coupled to the air inlets and conductively thermally coupled to stator windings of the electric motor; an outlet manifold having an air outlets formed at a back of the housing and coupled to the set of plurality of circumferentially grooved micro-channels; wherein the electric motor comprises PEW stator windings that provide a low thermal resistance path from the stator of the electric motor to the housing; wherein the PEW stator windings comprise a high temperature tolerant thermally conductive electrical insulator.