Multi-function pressure probe for aircraft

Measuring and testing – Navigation – Leeway incidence or side-slip

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

73189, G01C 2100

Patent

active

046728465

ABSTRACT:
Disclosed is an apparatus for measuring the aerodynamic parameters of an airflow around an aircraft. A streamlined body is rotatably mounted in the airflow such that it aligns itself freely with the flow. Total and static pressure pick-off apertures are provided in the body. The measurement of the true angle of incidence is obtained from two distinct measurements. A first measurement mechanically provides the orientation .alpha.m of the streamlined body relative to the aircraft and the other provides the aerodynamic pressure orientation .alpha.a of the same streamlined body relative to the airflow. The true angle of incidence .alpha. is then determined by summing .alpha.m and .alpha.a.

REFERENCES:
patent: 2662402 (1953-12-01), Ince, Jr. et al.
patent: 2936617 (1960-05-01), Beebe
patent: 3329016 (1967-07-01), Leavens et al.
patent: 3343412 (1967-09-01), Stout, Jr.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Multi-function pressure probe for aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Multi-function pressure probe for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Multi-function pressure probe for aircraft will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-676781

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.