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Matthew Lassen Phones & Addresses

  • Pensacola, FL
  • 84 Union St APT 205, Seattle, WA 98101
  • Everett, WA
  • Annapolis, MD
  • Chester, MD
  • Dearborn Hts, MI

Resumes

Resumes

Matthew Lassen Photo 1

Smartly School Of Business

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Location:
Seattle, WA
Industry:
Military
Work:
Booz Allen Hamilton
Staff Engineer

Us Navy May 2016 - Sep 2016
Special Projects Officer

Us Navy Aug 2013 - May 2016
Auxiliaries Division Officer

Aug 2013 - May 2016
Smartly School of Business
Education:
United States Naval Academy 2009 - 2013
Bachelors, Bachelor of Science, Computer Science
Naval Academy Preparatory School 2008 - 2009
Skills:
Web Development
Project Management
Programming
Managing Technical Personnel
Leadership
Management
Object Oriented Programming
Microsoft Office
Software Development
Linux
Relational Databases
Sql
Jquery
Blender
Cascading Style Sheets
Ajax
Information Technology
Networking
Xquery
Representational State Transfer
Soap
Visual Basic
Unity3D
Asp.net Mvc
Java Virtual Machine
Information Assurance
Databases
Network Security
Systems Engineering
Javascript
Languages:
English
Matthew Lassen Photo 2

Matthew Lassen

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Location:
Seattle, WA
Work:
Booz Allen Hamilton Nov 2016 - Jun 2019
Staff Engineer
Education:
Quantic School of Business and Technology
Master of Business Administration, Masters
Matthew Lassen Photo 3

Matthew Lassen

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Matthew Lassen Photo 4

Matthew Lassen

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Location:
United States
Matthew Lassen Photo 5

787 Flight Controls System Engineer At The Boeing Company

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Location:
Greater Seattle Area
Industry:
Aviation & Aerospace
Matthew Lassen Photo 6

Matthew Lassen

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Location:
United States

Publications

Us Patents

Wing Fold System With Latch Pins Through Multiple Mating Lugs

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US Patent:
20140061371, Mar 6, 2014
Filed:
Oct 9, 2013
Appl. No.:
14/049425
Inventors:
Jan A. Kordel - Redmond WA, US
Quentin Theodor Pietersen - Kirkland WA, US
Steven Paul Walker - Arlington WA, US
Kelly Thomas Jones - Snohomish WA, US
Matthew August Lassen - Seattle WA, US
Rickie Hansken - Tulalip WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/56
US Classification:
244 49
Abstract:
A wing fold system of a wing of an aircraft. The system may include a first lock of a latch to prevent movement of a latch pin of the latch to prevent movement of an unfixed portion of the wing with respect to a fixed portion of the wing, the first lock may include a first cam configured to prevent the second lock from transitioning to a second engaged position until the first lock may be in a first engaged position via contact with a second cam of the second lock. A second lock of the latch, the second lock may include the second cam configured to prevent the first lock from transitioning away from the first engaged position until the second lock transitions away from the second engaged position.

Hinged Raked Wing Tip

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US Patent:
20130099060, Apr 25, 2013
Filed:
Oct 30, 2012
Appl. No.:
13/664416
Inventors:
THE BOEING COMPANY - Chicago IL, US
Mark S. Good - Seattle WA, US
Jan A. Kordel - Redmond WA, US
Stephen J. Fox - Everett WA, US
Matthew A. Lassen - Seattle WA, US
Bruce Robert Fox - Everett WA, US
Steven Paul Walker - Arlington WA, US
Gregory M. Santini - Bothell WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64C 3/56
B64C 3/58
US Classification:
2441994
Abstract:
A wing assembly comprises a raked wing tip having an outboard portion hinged to one of a main wing having at least one moveable control surface and an inboard raked wing tip portion. The outboard portion of the raked wing tip does not carry any moveable flight control surfaces.

Backup System

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US Patent:
20180312240, Nov 1, 2018
Filed:
Jul 6, 2018
Appl. No.:
16/029327
Inventors:
- Chicago IL, US
Matthew August Lassen - Seattle WA, US
Michael E. Renzelmann - Woodinville WA, US
Mark J. Gardner - Snohomish WA, US
Mark William Lesyna - Everett WA, US
Brian Curtis Hill - Everett WA, US
Nicholas Seth Tyler - Everett WA, US
International Classification:
B64C 3/56
B64C 13/50
B64C 13/40
B64C 13/42
Abstract:
A system and method for a number of backup systems in an aircraft. The apparatus comprises a movement system; a latch system; a lock system; and at least one of a backup valve, a backup actuator, or a backup power source connected to at least one of the movement system, the latch system, or the lock system. The movement system has a first number of actuators and is connected to a hydraulic power source. The latch system has a second number of actuators and is connected to the hydraulic power source. The lock system has a third number of actuators and is connected to the hydraulic power source.

Systems For Latching And Locking A Folding Wing

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US Patent:
20170152017, Jun 1, 2017
Filed:
Feb 9, 2017
Appl. No.:
15/428304
Inventors:
- Chicago IL, US
Matthew A. Lassen - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/56
Abstract:
A folding wing comprises a fixed section, a folding section, and a latch system for latching the folding section to the fixed section. The latch system includes a plurality of latch pins, and a corresponding plurality of non-backdriveable mechanical actuators for extending the latch pins to engage the folding section.

Wing Fold System Rotating Latch

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US Patent:
20170066521, Mar 9, 2017
Filed:
Sep 14, 2016
Appl. No.:
15/265258
Inventors:
- Chicago IL, US
Jan A. Kordel - Redmond WA, US
Keith Townsend - Everett WA, US
Matthew August Lassen - Seattle WA, US
Mark John Gardner - Snohomish WA, US
Mark Steven Good - Seattle WA, US
International Classification:
B64C 3/56
Abstract:
An apparatus and method of a wing fold system may include a latch assembly rotating an unfixed portion of a wing, with respect to a fixed portion of the wing, between a flight position of the wing and a folded position of the wing. A first portion of the wing may hold a rotating portion of the latch assembly. A second portion of the wing may hold a secured portion of the latch assembly. The rotating portion of the latch assembly may rotate between an open position and a closed position. A slot in the rotating portion may receive the secured portion of the latch assembly. A securing portion of the rotating portion may secure a secured portion of the latch assembly. The latch assembly may prevent rotation of the second portion when the wing may be in the flight position.

Wingtip Control System

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US Patent:
20160280392, Sep 29, 2016
Filed:
Mar 25, 2016
Appl. No.:
15/080586
Inventors:
- Chicago IL, US
Joshua Jay Baer - Shoreline WA, US
Joseph Adam Sikora - Seattle WA, US
Matthew August Lassen - Seattle WA, US
Michael Edwin Foster - Bellingham WA, US
Timothy P. Gallagher - Granite Falls WA, US
International Classification:
B64D 45/00
B64C 9/00
B64C 13/04
B64C 23/06
B64C 3/38
Abstract:
A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.

Backup System

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US Patent:
20160251073, Sep 1, 2016
Filed:
Nov 7, 2014
Appl. No.:
14/535864
Inventors:
- Chicago IL, US
Matthew August Lassen - Seattle WA, US
Michael E. Renzelmann - Woodinville WA, US
Mark J. Gardner - Snohomish WA, US
Mark William Lesyna - Everett WA, US
Brian Curtis Hill - Everett WA, US
Nicholas Seth Tyler - Everett WA, US
International Classification:
B64C 3/56
B64C 13/50
B64C 13/42
Abstract:
A system and method for a number of backup systems in an aircraft. The apparatus comprises a movement system; a latch system; a lock system; and at least one of a backup valve, a backup actuator, or a backup power source connected to at least one of the movement system, the latch system, or the lock system. The movement system has a first number of actuators and is connected to a hydraulic power source. The latch system has a second number of actuators and is connected to the hydraulic power source. The lock system has a third number of actuators and is connected to the hydraulic power source.

Wing Fold System Rotating Latch

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US Patent:
20150298793, Oct 22, 2015
Filed:
Aug 14, 2013
Appl. No.:
13/966754
Inventors:
- Chicago IL, US
Jan A. Kordel - Redmond WA, US
Keith Townsend - Everett WA, US
Matthew August Lassen - Seattle WA, US
Mark John Gardner - Snohomish WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 3/56
Abstract:
An apparatus and method of a wing fold system may include a latch assembly rotating an unfixed portion of a wing, with respect to a fixed portion of the wing, between a flight position of the wing and a folded position of the wing. A first portion of the wing may hold a rotating portion of the latch assembly. A second portion of the wing may hold a secured portion of the latch assembly. The rotating portion of the latch assembly may rotate between an open position and a closed position. A slot in the rotating portion may receive the secured portion of the latch assembly. A securing portion of the rotating portion may secure a secured portion of the latch assembly. The latch assembly may prevent rotation of the second portion when the wing may be in the flight position.
Matthew J Lassen from Pensacola, FL, age ~34 Get Report