DR. JOHN W. HO, MD
Radiology in Seattle, WA

License number
Washington MD00042236
Category
Radiology
Type
Vascular & Interventional Radiology
Address
Address 2
500 S Swedish Providence Medical Ctr, Seattle, WA 98124
728 134Th St SW SUITE 120, Everett, WA 98204
Phone
(206) 320-3700
(425) 297-6200
(425) 297-6250 (Fax)

Organization information

See more information about JOHN W. HO at bizstanding.com

Seattle Children's Hospital - John W Ho MD

4800 Sand Pt Way NE #5G-1, Seattle, WA 98105

Categories:
Radiology Physicians & Surgeons
Phone:
(206) 987-2000 (Phone)


John W Ho MD

4800 Sand Pt Way NE, Seattle, WA 98105

Industry:
Nonclassifiable Establishments

Professional information

John Ho Photo 1

Business Development Manager At Emagin Corporation

Position:
Business Development Manager at eMagin Corporation
Location:
Greater Seattle Area
Industry:
Computer Software
Work:
eMagin Corporation since Apr 2011 - Business Development Manager Microsoft Oct 2006 - Nov 2009 - Partner Marketing and Business Development Manager Amtren Corporation 2005 - 2006 - VP Marketing and Sales HP 1993 - 2005 - Business Development Manager
Education:
California State University-Long Beach 1986 - 1988
MS, Electrical Engineering
University of California, Santa Barbara
BS, Physics
Interests:
Avid fan of, and coach of, girls fastpitch softball. Helped coached the Woodinville Reign '97 team to a fourth place finish at Triple Crown World Series. Also involved with the Acers Fastpitch Organization. Daughter will soon be on her way to China, helping to represent Washington State, playing softball and spreading good will. Same daughter who has just committed to Ashford University for fastpitch softball!


John W Ho Photo 2

Dr. John W Ho, Everett WA - MD (Doctor of Medicine)

Specialties:
Diagnostic Radiology
Address:
1100 Pacific Ave, Everett 98201
(425) 339-2433 (Phone)
728 134Th St SW, Everett 98204
(425) 297-6200 (Phone)
Certifications:
Diagnostic Radiology, 2001
Awards:
Healthgrades Honor Roll
Languages:
English, Cantonese, Mandarin
Hospitals:
1100 Pacific Ave, Everett 98201
728 134Th St SW, Everett 98204
Providence Regional Medical Center Everett
1321 Colby Ave, Everett 98201
Swedish Medical Center/Cherry Hill
500 17Th Ave, Seattle 98122
Swedish Medical Center/First Hill
747 Broadway, Seattle 98122
Education:
Medical School
University Of Connecticut School Of Medicine
Graduated: 1995
Beth Israel Med Center
University Of Washington


John Ho Photo 3

Business Analyst At Boeing Commercial Airplanes

Position:
Channel Analyst Level 2 at T-Mobile
Location:
Greater Seattle Area
Industry:
Aviation & Aerospace
Work:
T-Mobile - Bellevue, WA since Jun 2011 - Channel Analyst Level 2 Boeing - Tukwila, WA Jun 2008 - Jun 2011 - Staff Analyst
Education:
University of Washington 2000 - 2006
Bachelors, Neurobiology


John W Ho Photo 4

John W Ho, Seattle WA

Specialties:
Radiologist
Address:
500 17Th Ave, Seattle, WA 98122
728 134Th St Sw, Everett, WA 98204
Education:
University of Connecticut, School of Medicine - Doctor of Medicine
Board certifications:
American Board of Radiology Certification in Diagnostic Radiology (Radiology)


John Ho Photo 5

Wing-Body Load Alleviation For Aircraft

US Patent:
8024079, Sep 20, 2011
Filed:
May 20, 2008
Appl. No.:
12/123942
Inventors:
Kioumars Najmabadi - Clyde Hill WA, US
William F. Shivitz - Renton WA, US
Edward Ernest Coleman - Forest Park WA, US
John Koon-hung Ho - Shoreline WA, US
Richard D. Johnson - Edmonds WA, US
William F. Carver - Shoreline WA, US
David W. Grubb - Monroe WA, US
Robert James McIntosh - Bothell WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G01C 23/00, G06F 17/10, B64C 3/58
US Classification:
701 3, 701124, 244 49, 244213
Abstract:
A computer implemented method, apparatus, and computer usable program product for symmetric and anti-symmetric control of aircraft flight control surfaces to reduce wing-body loads. Commands are sent to symmetrically deploy outboard control surfaces to shift wing air-loads inboard based on airplane state and speed brake deployment. Surface rate retraction on a wing with peak loads is limited to reduce maximum loads due to wheel checkback accompanied by utilization of opposite wing control surfaces to retain roll characteristics. Airloads are shifted inboard on a swept wing to move the center of pressure forward, thereby reducing the tail load required to perform a positive gravity maneuver. In a negative gravity maneuver, speed brakes are retracted, thereby reducing the positive tail load and reducing the aft body design loads. High gain feedback commands are filtered from wing structural modes above one hertz by a set of linear and non-linear filters.


John Ho Photo 6

Aircraft Multi-Axis Modal Suppression System

US Patent:
7191985, Mar 20, 2007
Filed:
Jul 12, 2005
Appl. No.:
11/180309
Inventors:
Kioumars Najmabadi - Bellevue WA, US
Chuong B. Tran - Mukilteo WA, US
John Koon-Hung Ho - Shoreline WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 13/16
US Classification:
244195, 244177, 244 751
Abstract:
Vibrations due to excitation of the natural modes of an aircraft's body are suppressed by an active multi-axis modal suppression system. Dedicated sensors are positioned in the aircraft at optimal locations for sensing modal induced vibrations. The sensor produced signals are processed through control logic which, in response thereto, and in response to aircraft inertial, velocity and altitude related signals produces output control signals. The control signals effect control surface deployment creating forces to suppress the natural mode induced vibrations on multiple geometric axis's. More particularly, a symmetric and anti-symmetric control surface deployments are used on one or more geometric axis'to damp lateral, longitudinal, vertical and most importantly torsional vibrational modes.


John Ho Photo 7

Aircraft Multi-Axis Modal Suppression System

US Patent:
6915989, Jul 12, 2005
Filed:
May 1, 2002
Appl. No.:
10/136907
Inventors:
Kioumars Najmabadi - Bellevue WA, US
Chuong B. Tran - Mukilteo WA, US
John Koon-Hung Ho - Shoreline WA, US
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C013/16
US Classification:
244195, 244177, 244 75 R
Abstract:
Vibrations due to excitation of the natural modes of an aircraft's body are suppressed by an active multi-axis modal suppression system. Dedicated sensors are positioned in the aircraft at optimal locations for sensing modal induced vibrations. The sensor produced signals are processed through control logic which, in response thereto, and in response to aircraft inertial, velocity and altitude related signals produces output control signals. The control signals effect control surface deployment creating forces to suppress the natural mode induced vibrations on multiple geometric axis's. More particularly, symmetric and anti-symmetric control surface deployments are used on one or more geometric axis's to damp lateral, longitudinal, vertical and most importantly torsional vibrational modes.