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Dale T Ruebsamen

from Glendale, AZ
Age ~66
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Also known as:
Dale Thomas Ruebsamen, Julie A Ruebsamen, Julie Ann Ruebsamen, Haley Ruebsamen, Ruebsamen Haley
Related to:
John Thomas Newell, 76Haley N Ruebsamen, 33Derrick R Johnston, 54Amy C Ruebsamen, 37Derrick R Johnston, 42Richerd S Ruebsamen, 64Beverly J Newell, 69Holly L Ruebsamen, 40Beverly Newell, 57
Connected to:
Allyson M Ruebusch, 36Carl V Ruebush, 87Debbie A Ruebush, 95Julie R Ruebush, 51Kimberly A Rueby, 65John P Rueca, 53James C Rueck, 95Jean L Rueck, 86John G Rueck, 38Bruce G Ruecker, 72

Dale Ruebsamen Phones & Addresses

  • Glendale, AZ
  • Phoenix, AZ
  • Flagstaff, AZ
  • 4036 W La Junta Dr, Glendale, AZ 85310

Work

Company: Honeywell Jan 2012 Position: Manager project engineering

Education

Degree: Bachelor of Science In Mechanical Engineering, Bachelors School / High School: Northern Arizona University 1978 to 1981

Skills

Engineering Management • Aerospace • Systems Engineering • Six Sigma • Avionics • Earned Value Management • Do 178B • Engineering • Mechanical Engineering • Root Cause Analysis • Space Systems • Testing • Aerospace Engineering • Project Management • Manufacturing Engineering • Manufacturing • Program Management • Lean Manufacturing • Green Belt • Telelogic Doors • System Design • Continuous Improvement • Spacecraft • Satellite Systems Engineering • Flight Test • Value Stream Mapping • Aircraft • Simulations • Arinc 429 • Kaizen • Composites • Finite Element Analysis • Process Improvement • Requirements Management • Systems Design • Ms Project • Design For Manufacturing • Sensors • Fmea

Industries

Aviation & Aerospace

Resumes

Resumes

Dale Ruebsamen Photo 1

Lead System Engineer

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Location:
Phoenix, AZ
Industry:
Aviation & Aerospace
Work:
Honeywell
Manager Project Engineering
Honeywell Jan 1982 - Jan 2012
Principal Engineer
Honeywell Aerospace Jan 1982 - Jan 2012
Lead System Engineer
Education:
Northern Arizona University 1978 - 1981
Bachelor of Science In Mechanical Engineering, Bachelors
Skills:
Engineering Management
Aerospace
Systems Engineering
Six Sigma
Avionics
Earned Value Management
Do 178B
Engineering
Mechanical Engineering
Root Cause Analysis
Space Systems
Testing
Aerospace Engineering
Project Management
Manufacturing Engineering
Manufacturing
Program Management
Lean Manufacturing
Green Belt
Telelogic Doors
System Design
Continuous Improvement
Spacecraft
Satellite Systems Engineering
Flight Test
Value Stream Mapping
Aircraft
Simulations
Arinc 429
Kaizen
Composites
Finite Element Analysis
Process Improvement
Requirements Management
Systems Design
Ms Project
Design For Manufacturing
Sensors
Fmea

Publications

Us Patents

Hermetic Seal For Devices With Limited Rotation

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US Patent:
6796563, Sep 28, 2004
Filed:
Nov 22, 2002
Appl. No.:
10/302502
Inventors:
Dale T. Ruebsamen - Glendale AZ
Steve L. Hadden - Peoria AZ
Toren S. Davis - Peoria AZ
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16J 1552
US Classification:
277636, 277634, 277391, 403220
Abstract:
A hermetic seal ( ) for a limited rotation device ( ) includes a plurality of vertical convolutes ( ) bonded to a device housing ( ) at their respective first ends ( ). At their respective second ends ( ), plurality of the vertical convolutes ( ) are bonded to a plurality of horizontal convolutes ( ). The plurality of horizontal convolutes ( ) are bonded to a device shaft ( ) at an end opposite of the plurality of vertical convolutes ( ). The plurality of vertical convolutes ( ) stretch in order to provide limited rotation and the horizontal convolutes ( ) expand or contract to accommodate length changes of the plurality of vertical convolutes ( ). The hermetic seal ( ) permits limited rotation while defining a barrier ( ) and preventing viscous fluid leakage to an external environment.

Multifunction Vibration Isolation Strut

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US Patent:
6851529, Feb 8, 2005
Filed:
Apr 18, 2002
Appl. No.:
10/125876
Inventors:
Stephen R. Jones - Glendale AZ, US
James H. Boyd - Phoenix AZ, US
Dale T. Ruebsamen - Glendale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16F007/10
US Classification:
188378, 267136
Abstract:
An isolation strut and strut support system for supporting a load and capable of operating in a first mode and a second mode comprising an air suspension spring connected to a load bearing shaft; a hydraulic damping element having a first chamber and a second chamber separated by a piston connected to the load bearing shaft. A hydraulic line has a valve therein, one end of the hydraulic line connected to the first chamber and the other end of the hydraulic line connected to the second chamber. A vibration detector is coupled to the valve for actuating the valve upon the occurrence of vibration of an abnormal quality; whereby, in a first mode of operation the load is rigidly attached to the ground via a load path through the hydraulic damping element and in a second mode the load is isolated by the air suspension spring and damped by the hydraulic damping element.

Isolator Using Externally Pressurized Sealing Bellows

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US Patent:
7182188, Feb 27, 2007
Filed:
Feb 16, 2005
Appl. No.:
11/059054
Inventors:
Dale T. Ruebsamen - Glendale AZ, US
James H. Boyd - Phoenix AZ, US
Assignee:
Honeywell International, Inc. - Morristown NJ
International Classification:
F16F 9/04
F16F 9/08
US Classification:
188298, 1883225
Abstract:
Apparatus are provided for a damping system. The system includes a housing having an inner surface defining a passage therethrough, a first bellows disposed within the passage, the first bellows having an outer surface and spaced apart from the housing inner surface to define a first chamber having a volume, a second bellows disposed within the passage, the second bellows having an outer surface and spaced apart from the housing inner surface to define a second chamber having a volume, a restrictive flow passage in fluid communication with the first and second chambers, fluid disposed within the first chamber, the second chamber, and the restrictive flow passage, and a piston coupled to the second bellows and disposed at least partially within the restrictive flow passage, the piston configured to selectively receive a force to thereby move the piston through the housing passage.

Fluid Amplifiers And Vibration Damping And Isolation Systems

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US Patent:
7732988, Jun 8, 2010
Filed:
Sep 26, 2008
Appl. No.:
12/239166
Inventors:
James Boyd - Glendale AZ, US
Dale T. Ruebsamen - Glendale AZ, US
Brett M. McMickell - Scottsdale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
H01L 41/08
F16D 65/52
US Classification:
310328, 310311, 188298
Abstract:
Fluid amplifiers and vibration damping and isolation systems are provided. A fluid amplifier includes a housing assembly, a piezo-electric element, two amplification stages, and a rod. The piezo-electric element is disposed within the housing assembly and is capable of being energized to lengthen axially to provide an input stroke at an initial magnitude. The first amplification stage is disposed within the housing assembly adjacent to the piezo-electric element and is adapted to amplify the input stroke from the piezo-electric element to a first magnitude. The second amplification stage is disposed in series with the first amplification stage and is adapted to increase the input stroke from the first magnitude to a second magnitude that is greater than the first magnitude to yield an amplified input stroke. The rod extends through the second amplification stage and is coupled thereto to transmit the amplified input stroke having the second magnitude.

Vibration Isolators

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US Patent:
7967282, Jun 28, 2011
Filed:
Oct 23, 2008
Appl. No.:
12/256909
Inventors:
James R. Boyd - Glendale AZ, US
Dale Thomas Ruebsamen - Glendale AZ, US
Timothy Hindle - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16F 1/38
US Classification:
267293, 26714013, 267280
Abstract:
Vibration isolators are provided that include a shaft, a first bushing, a second bushing, a first outer annular member, a second outer annular member, a first elastomeric member, a second elastomeric member, and a shim. The first elastomeric member is adapted to provide a first stiffness for damping a first vibration, and the second elastomeric member is adapted to provide a second stiffness for damping a second vibration, the second stiffness being greater than the first stiffness.

Vibration Isolation Apparatus And Methods Of Manufacture

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US Patent:
8002094, Aug 23, 2011
Filed:
Jan 9, 2007
Appl. No.:
11/651163
Inventors:
Dale T. Ruebsamen - Glendale AZ, US
James H. Boyd - Phoenix AZ, US
Toren S. Davis - Peoria AZ, US
Joseph E. Vecera - Glendale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16F 7/10
US Classification:
188379, 188380
Abstract:
A vibration isolation apparatus is provided that includes a main spring and a tuned mass damper. The main spring has a first end and a second end, and is configured to resonate when vibrated within a predetermined frequency range with a first axial surge mode having a magnitude. The tuned mass damper is coupled to the main spring at a first axial position located substantially equidistantly between the main spring first end and the main spring second end and is configured to reduce the first axial surge mode magnitude at least 50% when the main spring is vibrated within the predetermined frequency range. Methods of manufacturing the vibration isolation apparatus are also provided.

Tuned Mass Dampers And Vibration Isolation Apparatus

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US Patent:
8261896, Sep 11, 2012
Filed:
Sep 18, 2008
Appl. No.:
12/233218
Inventors:
James H. Boyd - Glendale AZ, US
Dale T. Ruebsamen - Glendale AZ, US
Joseph E. Vecera - Glendale AZ, US
Toren S. Davis - Peoria AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16F 7/10
US Classification:
188379, 188378, 188380
Abstract:
A tuned mass damper is provided for use with a structure that vibrates at a first axial surge mode and a second axial surge mode, when exposed to a predetermined frequency range. The tuned mass damper includes a housing, an endcap, two masses, and two springs. The first and second masses are disposed in a housing cavity. The first tuned mass damper spring is disposed in the cavity coupling the first mass and the endcap. The second tuned mass damper spring is disposed in the cavity coupling the first and second masses. The tuned mass damper has first and second resonant frequencies in the predetermined frequency range to damp the first and second axial surge modes, respectively. The second mass resonates at an amplitude that is greater than an amplitude at which the first mass resonates, when the two masses are subjected to the second axial surge mode.

Two Stage Vibration Isolator

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US Patent:
8327985, Dec 11, 2012
Filed:
Jun 22, 2009
Appl. No.:
12/489128
Inventors:
James Boyd - Glendale AZ, US
Timothy Hindle - Peoria AZ, US
Dale Thomas Ruebsamen - Glendale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F16F 7/10
US Classification:
188379, 188298, 1883225, 188380, 248562
Abstract:
A vibration isolating system is disclosed. The vibration isolating system comprises a passive mechanical system comprising a damping assembly, a first resilient member coupled in series with the damping assembly, and a second resilient member coupled in parallel with the series combination of the damping assembly and the first resilient member. The vibration isolating system further comprises a support member coupled in series with the passive mechanical system, a viscoelastic mount coupled to the support member, and a motion limiter coupled to the support member such that the passive mechanical system transmits a force to the support member when the passive mechanical undergoes longitudinal displacement greater than a predetermined displacement.
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Dale T Ruebsamen from Glendale, AZ, age ~66 Get Report