System for measuring an airflow angle at the wingtip of an...

Measuring and testing – Fluid flow direction

Reexamination Certificate

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C073S170020, C073S17800T, C073S186000

Reexamination Certificate

active

07395705

ABSTRACT:
A vortex angle system includes one or more vortex angle sensors disposed on one or more wingtips of an aircraft. A summing circuit and computer compare signals from each sensor to provide a signal, which is indicative of the average vortex angle of the aircraft.

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patent: 4230290 (1980-10-01), Townsend et al.
patent: 4814764 (1989-03-01), Middleton
patent: 4908619 (1990-03-01), Bala et al.
patent: 4924401 (1990-05-01), Bice et al.
patent: 5060889 (1991-10-01), Nadkarni et al.
patent: 5590853 (1997-01-01), Greene
patent: 6531967 (2003-03-01), Djorup
patent: 2002/0171563 (2002-11-01), Djorup

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