Career records & work history
Lawyers & Attorneys
Victor Riley - Lawyer
ISLN:
1000522418
Admitted:
2001
Victor W Riley, 83Blaine, WA
Victor Riley Phones & Addresses
Blaine, WA
2507 Wetmore Ave, Everett, WA 98201 425-3390992
Snohomish, WA
Work
Position:
Construction and Extraction Occupations
Education
Degree:
Graduate or professional degree
Mentions for Victor W Riley
Victor Riley resumes & CV records
Resumes
Victor Riley
Work:
Helping Hands of No
Retired
Retired
Victor Riley
Victor Riley
Victor Riley
Victor Riley
Publications & IP owners
Us Patents
Integrated Approach Navigation System, Method, And Computer Program Product
US Patent:
8027756, Sep 27, 2011
Filed:
Dec 7, 2006
Appl. No.:
11/608064
Inventors:
Robert B. Davis - Mill Creek WA, US
Daniel J. Boorman - Woodinville WA, US
L. Kirk Gagnon - Bothell WA, US
William L. Goodman - Coupeville WA, US
Alan R. Jacobsen - Renton WA, US
William A. Miller - Arlington WA, US
James E. Mitchell - Renton WA, US
Victor A. Riley - Point Roberts WA, US
William F. Royce - Kirkland WA, US
William D. Tafs - Issaquah WA, US
Daniel J. Boorman - Woodinville WA, US
L. Kirk Gagnon - Bothell WA, US
William L. Goodman - Coupeville WA, US
Alan R. Jacobsen - Renton WA, US
William A. Miller - Arlington WA, US
James E. Mitchell - Renton WA, US
Victor A. Riley - Point Roberts WA, US
William F. Royce - Kirkland WA, US
William D. Tafs - Issaquah WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G05D 1/06
US Classification:
701 8, 701 3, 701 5, 701 9, 701 14, 701 16, 701200, 701205
Abstract:
Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.
Integrated Approach Navigation System, Method, And Computer Program Product
US Patent:
8423207, Apr 16, 2013
Filed:
Aug 26, 2011
Appl. No.:
13/218978
Inventors:
Robert B. Davis - Mill Creek WA, US
Daniel J. Boorman - Woodinvill WA, US
L. Kirk Gagnon - Bothell WA, US
William L. Goodman - Coupeville WA, US
Alan R. Jacobsen - Renton WA, US
William A. Miller - Arlington WA, US
James E. Mitchell - Renton WA, US
Victor A. Riley - Point Roberts WA, US
William F. Royce - Kirkland WA, US
William D. Tafs - Issaquah WA, US
Daniel J. Boorman - Woodinvill WA, US
L. Kirk Gagnon - Bothell WA, US
William L. Goodman - Coupeville WA, US
Alan R. Jacobsen - Renton WA, US
William A. Miller - Arlington WA, US
James E. Mitchell - Renton WA, US
Victor A. Riley - Point Roberts WA, US
William F. Royce - Kirkland WA, US
William D. Tafs - Issaquah WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G05D 1/00
G05D 1/06
G05D 3/00
G06F 17/00
G05D 1/06
G05D 3/00
G06F 17/00
US Classification:
701 8, 701 3, 701 5, 701 9, 701 14, 701 16, 701400, 701466
Abstract:
Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.
Aircraft Dispatch Information
US Patent:
2010029, Nov 18, 2010
Filed:
May 15, 2009
Appl. No.:
12/466570
Inventors:
Victor Andrew Riley - Point Roberts WA, US
Robert G. Borst - Renton WA, US
Armando Gonzalez - Issaquah WA, US
David Scott Kinney - Everett WA, US
Robert G. Borst - Renton WA, US
Armando Gonzalez - Issaquah WA, US
David Scott Kinney - Everett WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 17/00
US Classification:
701 3
Abstract:
Systems and methods to manage aircraft dispatch information are provided. A particular method includes receiving fault information at a dispatch information computing system. The fault information is associated with an aircraft. The method also includes accessing operational restriction information associated with the aircraft based on the fault information. The method further includes automatically determining a set of bottom line operational limitations of the aircraft based on the fault information and the operational restriction information. The method also includes generating customized checklists for the various users of the information. The method also includes sending output data from the dispatch information computing system to an output device. The output data identifies the set of bottom line operational limitations of the aircraft and tasks to be completed by the various users.
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