ASHOK VIJ
Pilots at Avenida De Kira, Tucson, AZ

2007012, May 31, 2007

Nov 29, 2005

11/288716

Ashok Vij - Tucson AZ, US

G08B 17/10

340632000

A sensing device for detecting the presence of carbon monoxide in a selected space of concern and communicating with a remote monitoring device is provided. The sensing device comprises (a) a detection device configured to sense the presence of carbon monoxide in the selected space of concern, (b) a monitoring device remote from the detection device, for communicating information to an operator, and (c) the detector in circuit communication with the monitoring device, to transmit information from the detection device to the monitoring device that is related to carbon monoxide in the selected space. According to one preferred embodiment, the sensing device is designed for an aircraft. The remote monitoring device is the multifunctional display of the aircraft cockpit. In addition, in a preferred embodiment, a reset/retest actuator is connected with the multifunctional display, and is in circuit communication with the detection device. The reset/retest actuator is selectively actuated from the multifunctional display to send a reset/retest signal to the detection device, to reset the detection device, and to initiate operation of the detection device to repeat its carbon monoxide detection process and provide a signal related to the level of carbon monoxide detected by the detection device. Moreover, in a preferred embodiment, a heating element is provided that is proximate to the carbon monoxide detection component. The heating element is selectively actuated to heat the air space about the carbon monoxide detection component. Also, an adjustment device associated with the output of the CO detection device, for adjusting the output of the detection device in response to a signal related to the air pressure in the selected space of concern. These features are particularly useful in a detection device for an aircraft, where ambient temperatures may drop to levels that can adversely affect the performance of the detection device, or where pressure changes in the aircraft may affect the sensitivity of the detection device.

8548547, Oct 1, 2013

Jun 29, 2010

12/803555

Ashok K. Vij - Tucson AZ, US

A61B 6/00

600323

An aircraft cockpit with health monitoring system and method enables an occupant (e. g. a pilot) and/or a ground station to monitor the physical condition of the occupant during a flight. A sensor such as a pulse oximetry sensor is in predetermined location to an occupant seat (e. g. an aircraft cockpit seat), within the field of reach of a person seated in the seat. The sensor is supported in the predetermined location in a stable manner that provides sufficient reaction to insertion of a finger to enable insertion of a finger in the sensor while the person is in a seated position, and the sensor is in communication with a control box that processes data from the sensor, and presents the data, e. g. at a the multi functional display in an aircraft cockpit. During a flight, a pilot seated in the aircraft cockpit seat will be prompted to insert a finger into the pulse oximetry sensor to produce output at the multi functional display.