Phillip W Gold DeceasedWest Sayville, NY

Phillip Gold Phones & Addresses

West Sayville, NY

Manorville, NY

Maine, NY

123 Hilary St, West Sayville, NY 11796

Mentions for Phillip W Gold

Career records & work history

Medicine Doctors

Phillip M. Gold

Specialties:
Pulmonary Disease, Sleep Medicine
Work:
Loma Linda Physicians Medical GroupLoma Linda University Faculty Physicians-Pulmonary & Sleep Medicine
11370 Anderson St STE 3300, Loma Linda, CA 92354
(909) 558-2896 (phone) (909) 558-2079 (fax)
Site
Education:
Medical School
University of California, Los Angeles David Geffen School of Medicine
Graduated: 1962
Procedures:
Pulmonary Function Tests, Vaccine Administration
Conditions:
Bronchial Asthma, Obstructive Sleep Apnea, Acute Bronchitis, Acute Sinusitis, Bacterial Pneumonia, Chronic Bronchitis, Gastroesophageal Reflux Disease (GERD), Hypertension (HTN), Hypothyroidism, Insomnia, Overweight and Obesity, Pneumonia, Pulmonary Embolism, Rheumatoid Arthritis, Sarcoidosis
Languages:
English, Spanish
Description:
Dr. Gold graduated from the University of California, Los Angeles David Geffen School of Medicine in 1962. He works in Loma Linda, CA and specializes in Pulmonary Disease and Sleep Medicine. Dr. Gold is affiliated with Loma Linda University Medical Center.

Phillip Gold resumes & CV records

Resumes

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Phillip Gold

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Phillip Gold

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Phillip Gold

Location:
United States
Phillip Gold Photo 26

Phillip Gold

Location:
United States
Phillip Gold Photo 27

Phillip Gold

Location:
United States

Publications & IP owners

Us Patents

Low Speed Model Following Velocity Command System For Rotary Wing Aircraft

US Patent:
5195700, Mar 23, 1993
Filed:
Aug 28, 1991
Appl. No.:
7/751437
Inventors:
Donald L. Fogler - Milford CT
James L. Richard - Stratford CT
Phillip J. Gold - Shelton CT
Steven L. Glusman - Springfield PA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B64C 1144
G05D 110
G05D 108
US Classification:
244 1721
Abstract:
A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).

High Speed Turn Coordination For Rotary Wing Aircraft

US Patent:
5238203, Aug 24, 1993
Filed:
Aug 28, 1991
Appl. No.:
7/751431
Inventors:
Joseph P. Skonieczny - Madison CT
Donald L. Fogler - Milford CT
Phillip J. Gold - Shelton CT
James F. Keller - Media PA
James B. Dryfoos - Wallingford PA
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
G06F 1550
US Classification:
244 1713
Abstract:
A helicopter flight control system (21) includes a model following control system architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate helicopter flight during a banked turn. The control system processes information from a variety of helicopter sensors (31) in order to provide the coordinating yaw command signal on an output line (72) to the tail rotor (20) of the helicopter.

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