MARIO RUIZ
Pilots at Luz De Lumbre Ave, El Paso, TX
License number
Texas A4874829
Issued Date
Nov 2013
Expiration Date
Nov 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
7382 Luz De Lumbre Ave, El Paso, TX 79912
Organization information
See more information about MARIO RUIZ at bizstanding.comMARIO RUIZ
5837 Burning Tree Dr, El Paso, TX 79912
Industry:
Interior Designers
Phone:
(915) 585-0239 (Phone)
Professional information
Mario Ruiz
Work:
OLIVE GARDEN
SERVER IMPACT/MODEL, ABERCROMBIE & FITCH - El Paso, TX
Sales Associate HOLLISTER CO - El Paso, TX
Sales Associate
SERVER IMPACT/MODEL, ABERCROMBIE & FITCH - El Paso, TX
Sales Associate HOLLISTER CO - El Paso, TX
Sales Associate
Education:
El Paso Community College - El Paso, TX
Associate of Science in Biological Sciences
Associate of Science in Biological Sciences
Method And Apparatus For Automatically Controlling Aircraft Flight Control Trim Systems
US Patent:
2011013, Jun 9, 2011
Filed:
Dec 3, 2010
Appl. No.:
12/959418
Inventors:
Michael Louis Everett - El Paso TX, US
Louis Jackson Everett - El Paso TX, US
Mario Ruiz - El Paso TX, US
Louis Jackson Everett - El Paso TX, US
Mario Ruiz - El Paso TX, US
International Classification:
G05D 1/00
US Classification:
701 3
Abstract:
An automatic trim system and method is disclosed for automatically trimming a flight control surface of an aircraft. A force sensor measures a force applied by a pilot to a flight control system actuator. The length of time that the force is applied by the pilot is then timed by a tinier. A trim system to reduce the applied force is included on the flight control surfaces. A processor determines if trim is required if a predetermined amount of time is exceeded based on the force sensor measurement. The processor can set the trim system to the trim required therein. An airspeed sensor is used to verify that the aircraft has sufficient speed for flight. A force sensor can be utilized to measure the input force being applied by the pilot. If a pilot input force is applied to the controls and the aircraft is in a steady state, a timer can be activated. If the force sensor continues to sense a force after the tinier times for a predetermined time, the trim can he adjusted in the appropriate direction until the force sensor measures no significant pilot input force.
Light Aircraft Stabilization System
US Patent:
2010010, Apr 29, 2010
Filed:
Oct 21, 2009
Appl. No.:
12/603321
Inventors:
Michael L. Everett - El Paso TX, US
Louis J. Everett - El Paso TX, US
Mario Ruiz - El Paso TX, US
Louis J. Everett - El Paso TX, US
Mario Ruiz - El Paso TX, US
International Classification:
B64C 13/16, G05D 1/00
US Classification:
244175
Abstract:
Control systems, controllers, systems, and methods of stabilizing a light aircraft during flight and/or ground maneuvers, such as by detecting and/or correcting undesired yaw characteristic, such as, for example, yaw angle, yaw rate, and/or yaw fluctuations.