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Brian K Naslund

from Minneapolis, MN
Age ~54
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Also known as:
Brian K Nashlund, Brian K Neslund, Brian K Nasland, Brian Anslund
Phone and address:
520 Ironton St NE, Minneapolis, MN 55432
(763) 443-5574
Related to:
Leland Royce Frazee, 62Rhonda Grant, 67Todd Olson, 54Janet Frazee, 70Ned Frazee, 31Richard L Johnson, 80
Connected to:
Bengt E Naslund, 77Charles D Naslund, 77Curtis L Naslund, 81Glen E Naslund, 111Jim Naslund, 66Katarina A Naslund, 35Lars E Naslund, 47Leona M Naslund, 95Philip Naslund, 35Therese M Nasman, 60

Brian Naslund Phones & Addresses

  • 520 Ironton St NE, Minneapolis, MN 55432 (763) 443-5574
  • 10392 Partridge St, Minneapolis, MN 55433 (763) 755-1484
  • Fridley, MN
  • Blaine, MN
  • 15310 Zirconium St NW, Anoka, MN 55303
  • Ramsey, MN
  • 520 Ironton St NE, Minneapolis, MN 55432

Work

Company: Collins aerospace Dec 2018 Position: Engineering site director

Education

Degree: Master of Business Administration, Masters School / High School: University of Minnesota - Carlson School of Management 2006 to 2008

Skills

Aerospace • Engineering Management • Engineering • Systems Engineering • Avionics • Aircraft • Root Cause Analysis • Cross Functional Team Leadership • Continuous Improvement • Lean Manufacturing • Design For Manufacturing • Earned Value Management • Program Management • Flight Test • Mechanical Engineering • Six Sigma

Languages

French • English

Industries

Aviation & Aerospace

Resumes

Resumes

Brian Naslund Photo 1

Engineering Site Director

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Location:
506 Del Rio Dr, Chanhassen, MN 55317
Industry:
Aviation & Aerospace
Work:
Collins Aerospace
Engineering Site Director
Utc Aerospace Systems Sep 2018 - Nov 2018
Engineering Site Director
Utc Aerospace Systems Feb 1, 2016 - Oct 2018
Program Chief - Smartprobe, Pressure, and Mems
Utc Aerospace Systems Sep 1, 2015 - Feb 1, 2016
Interim Coe Lead - Air Data Systems
Utc Aerospace Systems Aug 2012 - Feb 2016
Engineering Manager - Air Data Systems
Education:
University of Minnesota - Carlson School of Management 2006 - 2008
Master of Business Administration, Masters University of Minnesota 1998 - 2003
Bachelors, Bachelor of Science, Aerospace Engineering
Skills:
Aerospace
Engineering Management
Engineering
Systems Engineering
Avionics
Aircraft
Root Cause Analysis
Cross Functional Team Leadership
Continuous Improvement
Lean Manufacturing
Design For Manufacturing
Earned Value Management
Program Management
Flight Test
Mechanical Engineering
Six Sigma
Languages:
French
English

Publications

Us Patents

Method To Detect Angle Sensor Performance Degradation Through Dither Monitoring

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US Patent:
20110270576, Nov 3, 2011
Filed:
Apr 20, 2011
Appl. No.:
13/090950
Inventors:
Brian B. Naslund - Chanhassen MN, US
Jonathan R. Singleton - Burnsville MN, US
Robert A. Combs - Deephaven MN, US
Assignee:
Rosemount Aerospace Inc. - Burnsville MN
International Classification:
G06F 15/00
US Classification:
702183
Abstract:
A method for detecting angle sensor performance degradation in a flow angle measurement device in moving platform, such as aircraft and watercraft, as well as stationary platforms. Sensor dither in a flow angle measurement device is used to detect operational performance degradation of the sensor as a result of dynamic response changes caused by damaged or degraded mechanical components.

System For The Inspection Of Air Data Probes

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US Patent:
20210398263, Dec 23, 2021
Filed:
Jun 19, 2020
Appl. No.:
16/946412
Inventors:
- Burnsville MN, US
William Kunik - Lakeville MN, US
Brian Brent Naslund - Chanhassen MN, US
Rameshkumar Balasubramanian - Apple Valley MN, US
International Classification:
G06T 7/00
G01F 1/46
B64D 45/00
G06K 9/62
Abstract:
A method of inspecting an air data probe for damage or misalignment on a mounting surface includes retrieving reference data for the air data probe from a database, capturing images of the air data probe via a camera and generating dimensions from the captured images of the air data probe via a feature extractor. An alignment calculator analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify misalignment of the air data probe, and analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify damage of the air data probe. A maintenance recommendation for the air data probe is generated and outputted, based on the identified misalignment or damage of the air data probe.

Prognostic Monitoring Of Complementary Air Data System Sensors

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US Patent:
20200361627, Nov 19, 2020
Filed:
May 16, 2019
Appl. No.:
16/414539
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
John D. Winter - Apple Valley MN, US
Joel Boelke - Eden Prairie MN, US
International Classification:
B64D 45/00
G01P 13/02
G06N 3/02
G01L 13/00
G06F 17/14
Abstract:
A aircraft health management system for identifying an anomalous signal from one or more air data systems (ADS) includes one or more of a frequency processor, configured to provide a spectral signal that is representative of a frequency content of the first ADS signal, a noise processor, configured to provide a noise signal that is representative of a noise level of the first ADS signal, and a rate processor, configured to provide a rate signal that is representative of a rate of change of the first ADS signal. The aircraft health management system also includes a comparator configured to provide a differential signal between the first ADS signal and the second ADS signal, and a prognostic processor configured to determine if the ADS signal is anomalous by comparing values representative of a flight condition signal, the differential signal, and the spectral, noise, and/or rate signals.

Digital Air Data Systems And Methods

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US Patent:
20200309573, Oct 1, 2020
Filed:
Mar 25, 2019
Appl. No.:
16/363870
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
Benjamin John Langemo - Shakopee MN, US
Michael Robert Daup - Minneapolis MN, US
International Classification:
G01D 7/00
B64D 43/00
H04Q 9/00
Abstract:
An air data system with a digital interface includes least one air data component, a receiving system and at least one digital connection. The at least one digital connection is between the receiving system and the air data component. A method for transmitting data in an air data system with a digital interface includes measuring at least one air data parameter with at least one air data component. The method includes generating a digital signal representative of the at least one air data parameter with the at least one air data component, sending the digital signal to a receiving system, and processing the at least one air data parameter with the receiving system.

Image-Based Inspection For Physical Degradation Of An Air Data Probe

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US Patent:
20200211175, Jul 2, 2020
Filed:
Dec 27, 2018
Appl. No.:
16/233592
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
Scott J. Braun - Lakeville MN, US
International Classification:
G06T 7/00
G01N 17/00
G01N 21/88
G01B 11/16
G06T 7/13
G06T 7/70
H04N 5/262
H04N 5/232
Abstract:
Inspecting an air data probe for physical degradation includes generating a silhouette of the air data probe based on an identification of the air data probe to be inspected. The silhouette is simultaneously displayed with an image of the air data probe produced by a camera, and the displayed image of the air data probe is caused to conform to the silhouette on the display. An image of the air data probe is captured while the displayed image of the air data probe conforms to the silhouette on the display. The captured image is analyzed to identify physical degradation of the air data probe. A maintenance recommendation for the air data probe is generated based on the identified physical degradation.

Low Profile Air Data System Architecture

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US Patent:
20200018776, Jan 16, 2020
Filed:
Jul 13, 2018
Appl. No.:
16/034847
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
International Classification:
G01P 5/24
G01C 9/00
G01K 11/24
Abstract:
A system and method for an aircraft includes a low profile pneumatic sensing system and an acoustic sensing system. The low profile pneumatic sensing system includes a pneumatic sensor positioned to sense first sensed data of an airflow about an exterior of the aircraft and does not extend beyond a boundary layer of the aircraft. The first sensed data is used to determine first air data parameters. The acoustic sensing system is configured to emit acoustic signals about the exterior of the aircraft and sense the acoustic signals as second sensed data. The second sensed data is used to determine second air data parameters.

Architecture For Providing Enhanced Altitude Functionality To Aircraft Air Data System

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US Patent:
20190389594, Dec 26, 2019
Filed:
Jun 15, 2018
Appl. No.:
16/009911
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
Benjamin John Langemo - Shakopee MN, US
International Classification:
B64D 43/00
G01C 23/00
G01P 5/14
Abstract:
A system and method of augmenting an existing air data system includes a multi-function probe (MFP) having a portion extending into an oncoming airflow about an exterior of an aircraft. A plurality of pressure sensing ports in the portion includes at least first and second static pressure ports. A first electronics channel of the MFP includes pressure sensors communicating with the first and second static pressure ports and is configured to determine first and second altitude values based on sensed static pressures at the first and second static pressure ports, respectively, that are independent of the existing air data system.

Multi-Function Probe Air Data System Architecture Including Acoustic Sensors

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US Patent:
20190346278, Nov 14, 2019
Filed:
May 9, 2018
Appl. No.:
15/975355
Inventors:
- Burnsville MN, US
Brian Brent Naslund - Chanhassen MN, US
International Classification:
G01C 23/00
B64D 43/02
G01C 9/00
G01P 5/16
Abstract:
An air data system for an aircraft includes a multi-function probe (MFP) and an acoustic sensor system. The MFP is positioned to sense pressure of an airflow about an exterior of the aircraft. The pressure is used to generate first air data parameters for the aircraft. The acoustic sensor system is configured to emit acoustic signals about the exterior of the aircraft and sense the acoustic signals as sensed data, which is used to generate second air data parameters.
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Brian K Naslund from Minneapolis, MN, age ~54 Get Report