Aircraft pitot and static pressure sensing device and aircraft h

Details Aircraft pitot and static pressure sensing device and aircraft h Aircraft pitot and static pressure sensing device and aircraft h

1997-10-01

2000-03-21

Patel, Harshad

Measuring and testing

Volume or rate of flow

Using differential pressure

7386168, 73182, G01F 146, G01C 2100

Patent

active

06038932&

ABSTRACT:
An aircraft pitot and static pressure sensing device and an aircraft having the sensing device, more particularly a fighter aircraft, include a plurality of pressure sensors disposed in a radome of the aircraft. In addition, a plurality of air intake ports is provided in the radome. The air intake ports are connected through connecting passages to the pressure sensors.

REFERENCES:
patent: 3079758 (1963-03-01), Vogel et al.
patent: 3262316 (1966-07-01), Hansen et al.
patent: 3318146 (1967-05-01), De Leo et al.
patent: 3428270 (1969-02-01), Knight et al.
patent: 4378696 (1983-04-01), DeLeo et al.
patent: 5025661 (1991-06-01), McCormack
patent: 5099686 (1992-03-01), Kohler
patent: 5438880 (1995-08-01), Washburn
International Patent Application WO 89/02061 (Hagen et al.), dated Mar. 9, 1989.

Affiliated with

Also associated with

Rating

Aircraft pitot and static pressure sensing device and aircraft h does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft pitot and static pressure sensing device and aircraft h, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft pitot and static pressure sensing device and aircraft h will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-721600