Timothy Dean Jackson

8135807, Mar 13, 2012

Sep 18, 2007

11/857155

Timothy Edward Jackson - Arlington WA, US

The Boeing Company - Chicago IL

G06F 15/16
G06F 15/177

709220, 709223, 709224

The present disclosure provides systems and methods for distributing data packets on an aircraft data network having a plurality of end systems. The systems and methods include retrieving a configuration module, retrieving a payload description module, selecting a network interface component, selecting a port rate for the network interface component, selecting a payload module, generating payload data, generating a data packet from the generated payload data, and transmitting the generated data packet to at least one of the plurality of end systems via the network interface component and the aircraft data network.

20120194666, Aug 2, 2012

Feb 2, 2011

13/019416

Timothy Edward Jackson - Mukilteo WA, US

THE BOEING COMPANY - Chicago IL

G06K 9/46
H04N 7/18
G09G 5/00

348123, 382195, 345641

A method and apparatus for testing a number of display devices. Images displayed on the number of display devices are received by a computer system for a platform during a performance of a number of tests at a number of test locations for the platform. A portion of the images from the images are identified as a number of images of interest using a policy.

20120260180, Oct 11, 2012

Apr 6, 2011

13/081102

Garry Gean Herzberg - Renton WA, US
Timothy Edward Jackson - Mukilteo WA, US
Tracy Andrew Smail - Seattle WA, US
Charles Daniel Cowles - Kent WA, US
Erin Elizabeth Warr - Kent WA, US
Allen R. Link - Snohomish WA, US
Mark D. McCleary - Bellevue WA, US

THE BOEING COMPANY - Chicago IL

G06F 15/16
G06F 3/00

715736

Status of complex system functions is diagnosed and reported by analyzing traffic on a data network of the complex system. The network traffic may be placed on the data network by systems that perform functions for the complex system. A user may make a view selection via a remote user interface. The view selection identifies rules for determining a status of a selected subset of the functions or a status of selected ones of the functions for a selected state of operation, such as during initial power-up. The status of the functions may be determined from the network traffic using the rules and presented to the user via the user interface. The user may interact with the presentation to make different view selections. Multiple different view selections made via multiple different user interfaces may be supported simultaneously.

20120266024, Oct 18, 2012

Apr 15, 2011

13/088143

Timothy Edward Jackson - Mukilteo WA, US

The Boeing Company - Chicago IL

G06F 11/00

714 35, 714E1102

A particular system includes a processor and a network interface configured to send and receive messages via a network using an asynchronous computer communication protocol. The system may include two or more buffers, such as an ingress buffer and an egress buffer. The system may include a memory accessible to the processor. The memory may include first node instructions that are executable by the processor to implement one or more functions of a first node. The memory may also include one or more script callbacks. The script callbacks may be executable by the processor to at least one of provide: the first content to a test script to be modified before the first content is provided to the first node instructions from the ingress buffer, and provide the second content to the test script to be modified before the outgoing message is provided to the egress buffer.

20130287995, Oct 31, 2013

Apr 25, 2012

13/455217

Lyle Ray Deobald - Shoreline WA, US
Kenneth L. Brook - Seattle WA, US
Timothy D. Jackson - Everett WA, US
Gregory B. Doty - Edmonds WA, US

B32B 7/04
B32B 7/00
B32B 38/04

428120, 156256, 156 91

The disclosure herein provides for disbond resistant stringer runouts. Various aspects may be used independently or in combination to mitigate disbonding associated with the stiffener runout under operational loads. Aspects include a stiffener runout having rounded base flange corners. A recessed notch may be incorporated within the base flange to provide a flange termination point that is forward of the web termination point, allowing the web to terminate prior to the base flange. The web may be trimmed from a full height to a reduced height at the web termination point. The base flange may be co-bonded to the underlying composite structure via a scarf joint. Perimeter clamp radius fillers may be used to concentrate a clamping force around the perimeter of the base flange.

20190389150, Dec 26, 2019

Jun 20, 2018

16/013548

- Chicago IL, US
Jeron D. Moore - Lynnwood WA, US
Gagandeep Saini - Snohomish WA, US
Luis A. Perla - Sammamish WA, US
Brice Aaron Johnson - Federal Way WA, US
Stewart James Ibbotson - Bothell WA, US
Timothy D. Jackson - Everett WA, US
Robert G. Meyer - Renton WA, US
Robert Graham Albers - Bellevue WA, US

B29C 70/38

A method and apparatus for forming a composite object. A first plurality of tows is laid up over a tool according to a first path. A second plurality of tows is laid up over the tool according to a second path. A first portion of the first plurality of tows runs non-parallel to a second portion of the second plurality of tows. First ends of the first portion of the first plurality of tows and second ends of the second portion of the second plurality of tows meet at a merge zone along the tool to form a ply of a composite laminate.

20190215072, Jul 11, 2019

Mar 16, 2019

16/355712

- Chicago IL, US
Eric Y. Chan - Mercer Island WA, US
Dennis G. Koshinz - Bellevue WA, US
Kim Quan Anh Nguyen - Seattle WA, US
Sean M. Ramey - Redmond WA, US
Timothy E. Jackson - Arlington WA, US

The Boeing Company - Chicago IL

H04B 10/278
H04B 10/27
G02B 6/28
H04B 10/272
H04B 10/66
H04B 10/50
G02B 6/42
H04L 12/40
G02B 6/30
G02B 6/44

A controller area network (CAN) comprising a plurality of CAN nodes that communicate via a CAN bus that comprises a fiber optical network. The fiber optical network uses a single fiber and a single wavelength for transmit and receive, and comprises a passive reflective optical star. The reflective optical star comprises an optical mixing rod having a mirror at one end. The other end of the reflective optical star is optically coupled to the transmitters and receivers of a plurality of optical-electrical media converters by way of respective high-isolation optical Y-couplers. Each CAN node produces electrical signals (in accordance with the CAN message-based protocol) which are converted into optical pulses that are broadcast to the fiber optical network. Those optical pulses are then reflected back to all CAN nodes by the reflective optical star.

20180302165, Oct 18, 2018

Apr 18, 2017

15/489810

- Chicago IL, US
Dennis G. Koshinz - Bellevue WA, US
Eric Y. Chan - Mercer Island WA, US
Kim Quan Anh Nguyen - Seattle WA, US
Sean M. Ramey - Redmond WA, US
Timothy E. Jackson - Arlington WA, US

The Boeing Company - Chicago IL

H04B 10/278
G02B 6/42
G02B 6/44
G02B 6/30
H04L 12/40
H04B 10/272
H04B 10/50
H04B 10/66

A controller area network (CAN) comprising a plurality of CAN nodes that communicate via a CAN bus that comprises a fiber optical network. The fiber optical network uses a single fiber and a single wavelength for transmit and receive, and comprises a passive reflective optical star. The reflective optical star comprises an optical mixing rod having a mirror at one end. The other end of the reflective optical star is optically coupled to the transmitters and receivers of a plurality of optical-electrical media converters by way of respective high-isolation optical Y-couplers. Each CAN node produces electrical signals (in accordance with the CAN message-based protocol) which are converted into optical pulses that are broadcast to the fiber optical network. Those optical pulses are then reflected back to all CAN nodes by the reflective optical star.