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Roy Santos Alcantara

from Edmonds, WA
Age ~51
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Also known as:
Roy S Alcantara
Phone and address:
720 Hemlock St, Edmonds, WA 98020
Related to:
Ruth T Nguyen, 83Rex AlcantaraTimothy T Nguyen, 82Rolando R Alcantara, 77Kathleen T Nguyen, 51Rex S Alcantara, 58Rex S Alcantara, 44R Alcantara, 78Redencion S AlcantaraRita S Alcantara, 45Vanessa Alcantara
Connected to:
Abigail S Alcantara, 44Adelina M Alcantara, 79Adolfo G Alcantara, 63Alex Alcantar, 48Alexandra Alcantar, 32Amando S Alcantara, 75Andretti S Alcantara, 33Arjay Alcantara, 39Arnold Alcantara, 37Arthur D Alcantar, 46

Roy Alcantara Phones & Addresses

  • 720 Hemlock St, Edmonds, WA 98020
  • 10624 Rustic Rd, Seattle, WA 98178 (206) 772-6153
  • 10850 Lake Ridge Dr, Seattle, WA 98178 (206) 772-6153
  • Kirkland, WA
  • Spokane, WA
  • Port Tobacco, MD
  • Kiona, WA
  • 7327 126Th Ave NE, Kirkland, WA 98033

Work

Company: Boeing Dec 2014 Position: Avionics, technical integration lead engineer

Education

Degree: Bachelors, Bachelor of Science In Electrical Engineering School / High School: Gonzaga University Aug 1991 to Mar 1995

Skills

Avionics • Program Management • Flights • Project Management • Integration • Aerospace • Airlines • Management • Systems Engineering • Process Improvement • Business Analysis • Visio

Industries

Aviation & Aerospace

Resumes

Resumes

Roy Alcantara Photo 1

Avionics, Technical Integration Lead Engineer

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Location:
Seattle, WA
Industry:
Aviation & Aerospace
Work:
Boeing
Avionics, Technical Integration Lead Engineer
Boeing Jun 1996 - Oct 2013
Avionics, Flight Management System, Design Engineer
Education:
Gonzaga University Aug 1991 - Mar 1995
Bachelors, Bachelor of Science In Electrical Engineering
Skills:
Avionics
Program Management
Flights
Project Management
Integration
Aerospace
Airlines
Management
Systems Engineering
Process Improvement
Business Analysis
Visio

Publications

Us Patents

System And Method For Automatically Controlling Take-Off Thrust In An Aircraft

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US Patent:
8046120, Oct 25, 2011
Filed:
Oct 21, 2010
Appl. No.:
12/909360
Inventors:
Roy S. Alcantara - Seattle WA, US
Bradley J. Fischer - Sammamish WA, US
Raymond P. Craig - Federal Way WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06G 7/70
US Classification:
701 15, 701 16, 340959
Abstract:
A method for automatically selecting a take-off thrust setting for an engine of a jet powered mobile platform that has a flight management computer (FMC) that makes use of a configuration code. The configuration code is provided from a first set of information relating to operational parameters of the mobile platform. A database in communication with the FMC stores information pertaining to different locations from which a take-off operation can be performed. The FMC accesses the configuration code and the database to determine a take-off thrust setting to apply during the take-off operation at a specified one of the locations. The FMC also determines if an operator has overridden an automatic selection of the take-off thrust.

System And Method For Automatically Controlling Take-Off Thrust In An Aircraft

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US Patent:
20100030407, Feb 4, 2010
Filed:
May 2, 2007
Appl. No.:
11/743408
Inventors:
Roy S. Alcantara - Seattle WA, US
Bradley J. Fischer - Sammamish WA, US
Raymond P. Craig - Federal Way WA, US
International Classification:
G05D 1/00
G06F 19/00
US Classification:
701 15
Abstract:
A system and method for enabling a flight management computer (FMC) on a jet aircraft to automatically select the proper take-off thrust to use for a specific aircraft operating at a specific airport, and using a specific runway. A Model/Engine Database (MEDB) is created that assigns a specific aircraft configuration code to the aircraft, based on the model, engine and other factors specific to the aircraft. The aircraft configuration code is used by the FMC to query an Airport/Runway lookup table database that is loaded into the FMC. The Airport/Runway lookup table database provides a take-off thrust code indicating the take-off thrust to be used for the aircraft, based on the airport it is about to depart from, and the specific runway that it is assigned to use. The FMC uses the take-off thrust code to automatically select a specific take-off thrust to be used during the take-off phase of flight.

Flight Management System Having Customized Performance Database

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US Patent:
20190061971, Feb 28, 2019
Filed:
Aug 24, 2017
Appl. No.:
15/685147
Inventors:
- Chicago IL, US
Roy S. Alcantara - Seattle WA, US
Monica S. Alcabin - Seattle WA, US
Steven J. Moskalik - Seattle WA, US
Richard A. Herald - Lynnwood WA, US
Caroline Klein - Bothell WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64D 43/02
G07C 5/08
G08G 5/00
Abstract:
A flight management system which has access to customized information concerning the actual characteristics of a specific airplane or a specific fleet of airplanes of the same model when computing a predicted flight profile and associated trip prediction parameters. This up-to-date airplane-specific or fleet-specific information is digital data configured as a separately loadable database called a “customized performance database”. This customized performance database contains a smaller set of performance data—such as fuel flow correction, drag coefficient correction, and re-optimized speed/altitude tables—than is contained in the baseline performance database. The flight management system will continue to use a baseline performance database as a “limit” on the numbers computed using the customized performance database. The customized performance database can include tables or curves that are customizable by airlines.

Flight Management System Having Performance Table Datalink Capability

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US Patent:
20190035178, Jan 31, 2019
Filed:
Jul 27, 2017
Appl. No.:
15/662020
Inventors:
- Chicago IL, US
Roy S. Alcantara - Seattle WA, US
Steven J. Moskalik - Seattle WA, US
Monica S. Alcabin - Seattle WA, US
Caroline Klein - Bothell WA, US
Yian Guan - Edmonds WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G07C 5/08
G07C 5/00
Abstract:
A flight management system which is capable of monitoring changes in airplane characteristics. The flight management system is configured with a datalink management function that enables the uploading of updated performance table data from a ground station via a datalink. Upon receipt of updated aerodynamic and propulsion performance data via the datalink, the flight management system creates or updates a set of airplane performance tables or curves in a database which can be utilized to compute more accurate flight profile and trip prediction parameters, such as estimated time of arrival and predicted fuel consumption quantity.

Systems And Methods For Providing Airplane Performance Calculations

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US Patent:
20170197727, Jul 13, 2017
Filed:
Jan 13, 2016
Appl. No.:
14/995115
Inventors:
- Chicago IL, US
Roy S. Alcantara - Seattle WA, US
Christie M. Maldonado - Mukilteo WA, US
Steven J. Moskalik - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64D 45/00
B64D 37/00
Abstract:
A flight management system which is capable of monitoring changes in airplane characteristics such as fuel flow and drag. When a predetermined event is triggered, the flight management system (FMS) creates or updates a set of “dynamic” tables in a database which enable FMS performance algorithms to utilize the latest fuel flow and drag data.Using the updated aerodynamic and propulsion performance data in the dynamic tables, the flight management system is able to compute more accurate flight profile and trip prediction parameters such as estimated time of arrival and predicted fuel consumption quantity.
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Roy Santos Alcantara from Edmonds, WA, age ~51 Get Report