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Louis BaileySeattle, WA

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Louis Bailey Photo 49

Systems Engineer

Location:
Seattle, WA
Industry:
Airlines/Aviation
Work:
The Boeing Co
Systems Engineer
Education:
Embry - Riddle Aeronautical University 1992 - 1996
Skills:
Flight Management Systems, Flight Optimization, Flight Efficiency, Mobile Application Development, Weather Applications, Aircraft Performance, Avionics Integration, United States Army Airborne Graduate, United States Army Air Assault Graduate, Head Up Displays, Flight Planning
Languages:
German
English
Louis Bailey Photo 50

Customer Care Team Lead

Location:
Seattle, WA
Industry:
Environmental Services
Work:
1World Llc Jan 2015 - Mar 2018
Marketing Coordinator 1World Llc Feb 2002 - Jan 2015
Customer Service Representative Prolitec Inc. Feb 2002 - Jan 2015
Customer Care Team Lead
Education:
Seattle Central College 2003 - 2005
Skills:
E Commerce, Microsoft Office, Leadership, Research, Sales, Social Media, E Commerce Optimization
Louis Bailey Photo 51

Louis Bailey

Skills:
English
Louis Bailey Photo 52

Louis Bailey

Louis Bailey Photo 53

Louis Bailey

Location:
United States

Publications & IP owners

Us Patents

Dynamic Weather Selection

US Patent:
8165790, Apr 24, 2012
Filed:
Aug 26, 2009
Appl. No.:
12/547821
Inventors:
Louis J. Bailey - Kent WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G05D 1/00
G01S 13/95
US Classification:
701120, 340901, 701 10, 701 14
Abstract:
The different advantageous embodiments provide a system comprising a weather band selection process and a processor unit. The processor unit is configured to run the weather band selection process. The weather band selection process identifies a flight trajectory associated with an aircraft, identifies weather information for the flight trajectory, and identifies a weather band selection for the aircraft using the flight trajectory, aircraft information and the weather information.

Four-Dimensional Weather Predictor Based On Aircraft Trajectory

US Patent:
8332084, Dec 11, 2012
Filed:
Jun 23, 2009
Appl. No.:
12/490290
Inventors:
Louis J. Bailey - Kent WA, US
Gregory T. Saccone - Kirkland WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G05D 3/00
G06F 7/00
G06F 17/00
G01C 23/00
US Classification:
701 10, 701 3, 701 4, 701 14, 701415
Abstract:
A method of determining environmental data along a trajectory of an aircraft may assist in the evaluation of flight conditions along the trajectory. Environmental data may be at least one of collected, derived, and fused from a plurality of weather sources using at least one processor. The environmental data may be filtered, extrapolated, and fused, using the at least one processor, within at least one selected volume of airspace over a trajectory of the aircraft based on selected weather-applicability time intervals, and on at least one of user-selected parameters and weighted environmental data criteria. The trajectory may comprise at least one of a planned trajectory, a current trajectory, and an intent trajectory of the aircraft. An effect of the filtered, extrapolated, and fused environmental data on the trajectory may be determined using the at least one processor.

Dynamic Environmental Information Transmission

US Patent:
8416099, Apr 9, 2013
Filed:
Aug 26, 2009
Appl. No.:
12/547809
Inventors:
Louis J. Bailey - Kent WA, US
Ryan D. Hale - Kent WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G08G 1/00
US Classification:
340901, 340506, 340517, 340521, 34053922, 340 31, 340949, 340968, 701 14, 702 3
Abstract:
The different advantageous embodiments provide a system comprising a dynamic transmission process and a processor unit. The processor unit is configured to run the dynamic transmission process. The dynamic transmission process is configured to receive environmental information. The dynamic transmission process determines whether to send the environmental information to a subscriber.

Determining Current Meteorological Conditions Specific To An Aircraft

US Patent:
8437893, May 7, 2013
Filed:
Mar 5, 2008
Appl. No.:
12/042904
Inventors:
Robert W. Mead - Covington WA, US
Louis J. Bailey - Kent WA, US
Paul D. Hansen - Kent WA, US
Ferdinando Dijkstra - Amstelveen, NL
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 7/70
US Classification:
701 14, 701 3, 701408
Abstract:
A method of providing meteorological data for aeronautical use. The method includes collecting data from a plurality of data sources, processing the data to determine current meteorological conditions of a current location of an aircraft in an airspace, and providing the current meteorological conditions to the aircraft and other users as appropriate, such as airline operations centers, air navigation service providers, and national weather service providers. Based on current aircraft behavior data and guidance systems design, beneficial wind and meteorological data can be established for a given flight and its cleared route and descent path.

System And Method For Real-Time Aircraft Efficiency Analysis And Compilation

US Patent:
8509968, Aug 13, 2013
Filed:
Mar 20, 2012
Appl. No.:
13/424661
Inventors:
Gregory T. Saccone - Kirkland WA, US
Ryan D. Hale - Kent WA, US
Nicholas P. G. Impert - Bellevue WA, US
Louis J. Bailey - Covington WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 17/00
US Classification:
701 3, 701 296, 701 314, 701116, 701117, 701120, 701301, 701500, 244 121, 244 124, 244 1711, 244 1723, 244 39, 340945, 702138, 702144, 60230, 60477, 342 36, 416 96 R
Abstract:
Systems and methods for real-time efficiency and aircraft performance monitoring and delta efficiency calculations between various user- or system-selected phases of flight by determining an efficiency messaging index that gets translated into a messaging profile. That messaging profile is then used to obtain necessary flight and other information from multiple sources. The efficiency calculations and deltas can be used to determine real-time or post-processed benefits, which can then be used to optimize flight(s). Additionally, data is post-processed, which allows the calculation, storage and subsequent usage of efficiency coefficients to enhance the accuracy of the efficiency calculations. There are a number of ways to implement the architecture and order of processing.

Systems And Methods For Amalgamating Flight Information

US Patent:
8630790, Jan 14, 2014
Filed:
Oct 3, 2011
Appl. No.:
13/251406
Inventors:
Louis J. Bailey - Covington WA, US
Ryan D. Hale - Kent WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 19/00
US Classification:
701120, 340951
Abstract:
Systems and methods for receiving flight messages relating to a particular flight from multiple sources and processing information in those flight messages to create a single representation of an updated current and intended trajectory of such flight. Preferably, the system comprises one or more processors for performing the following operations: determining which flight message is the most recent; determining which flight messages are relevant; authenticating and processing proposed updates; and merging information contained in the flight messages to create a single representation of one or both of current or intended flight information.

Dynamic Adaptation Of Trigger Thresholds To Manage When Data Messages Are Transmitted

US Patent:
8639401, Jan 28, 2014
Filed:
Sep 20, 2011
Appl. No.:
13/237358
Inventors:
Louis J. Bailey - Covington WA, US
Ryan D. Hale - Kent WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 19/00
G08G 5/00
US Classification:
701 14, 701 2, 701 3
Abstract:
Systems and methods for remotely setting a value for a trigger threshold variable used by a processor unit onboard an aircraft to determine if and when a data message should be transmitted from the aircraft. The method comprises the following steps performed by a computer: (a) obtaining data representing a flight plan or flight trajectory of the aircraft and flight information; (b) obtaining data representing business considerations; (c) computing a value of the trigger threshold variable as a function of at least the flight plan or flight trajectory data and the business considerations data; and (d) constructing a trigger threshold data message containing the computed value of the trigger threshold variable.

Air Traffic Control Delay Factor

US Patent:
2009015, Jun 18, 2009
Filed:
Dec 12, 2007
Appl. No.:
11/954553
Inventors:
Louis J. Bailey - Kent WA, US
Marissa K. Singleton - Bellevue WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G08G 5/00
G05D 1/00
US Classification:
701121, 701122
Abstract:
A time factor corresponding to an airspace delay or acceleration is communicated to an aircraft. A flight management computer or other computational device of the aircraft calculates a proposed change in trajectory in order to accommodate the time factor in an optimum or nearly optimum manner. One or more proposed changes in trajectory are subject to review by the pilot or other flight personnel. An operator-selected change in trajectory is then implemented in order to accommodate a new arrival time of the aircraft at its destination or a positional point.

Possible Relatives

Davida Bailey  Davis M Bailey  Dean B Bailey  Deana R Bailey  Deangelo M Bailey  Daisy K Bailey  Debbie W Bailey  Louis E Johnson  Louis E White  Louis N Jones 

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