An aircraft static test adapter assembly comprising a static test head for performing testing at an aircraft static port on an aircraft body. The static test head is biased, and optionally supported by a biasing member extending in use from the static test head to the ground. A biasing mechanism provides a biasing force to the biasing member which is transferred by the biasing member to the static test head such that it is held in place. Abstract not intended to be limiting.
Aircraft static test for pitot static system
2019-11-12
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes |
Springer Verlag | 2018
|Commercial Transport Aircraft Pitot-Static System Installation & Calibration
British Library Conference Proceedings | 2018
|MAINTENANCE OF PITOT-STATIC SYSTEMS OF TRANSPORT AIRCRAFT
SAE Technical Papers | 1996