Rotary joint for a moving-vane multifunction pressure probe

Measuring and testing – Fluid flow direction – Relative to aircraft or watercraft

Reexamination Certificate

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C073S170010, C073S170050

Reexamination Certificate

active

07401507

ABSTRACT:
The present invention relates to pressure probes for measuring the aerodynamic flight parameters of an aircraft and more particularly those in which the orifices for measuring the static pressure and total pressure are located on a moving angle-of-attack or angle-of-sideslip measurement vane designed to be oriented in the direction of the wind. It consists of a pneumatic rotary joint employing flexible tubings rather than friction rotary joints between abutted parts of rigid tubings. Such a joint offers a much smaller resistance to the rotational movement of the moving vane, which consequently is oriented with greater accuracy in the direction of the wind.

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patent: 5866813 (1999-02-01), Nakaya et al.
patent: 6490510 (2002-12-01), Choisnet
patent: 6679112 (2004-01-01), Collot et al.
patent: 264 654 (1949-10-01), None
patent: 01/67115 (2001-09-01), None

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