A system for calculating forces exerted into an aircraft component includes a test hinge assembly and a monitoring system. In at least one embodiment, the test hinge assembly is a triangular shaped assembly, and includes at least one beam, at least one connecting joint having a channel configured to receive and retain a fastening member, and at least one strain gage secured to an outer surface of the beam(s). The strain gage(s) is configured to detect one or more strains exerted into the beam(s). The monitoring system is in communication with the strain gage(s). The monitoring system is configured to calculate forces exerted into the fastening member(s) by analyzing the strain(s) exerted into the beam(s).
Flight test hinge assembly configured for calculating exerted forces through strain analysis
17.10.2017
Patent
Elektronische Ressource
Englisch
IPC: | G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE / B64C AEROPLANES , Flugzeuge / 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 |
Dynamic Forces Exerted by Oscillating Cables
AIAA | 1974
|ASSEMBLY CONFIGURED TO OPERATE AS A HINGE AND DOOR BRAKE
Europäisches Patentamt | 2024
|Lateral Forces Exerted by Locomotives on Curved Track
Engineering Index Backfile | 1950
ASSEMBLY CONFIGURED TO OPERATE AS A HINGE AND DOOR CHECK FOR MOTOR VEHICLE
Europäisches Patentamt | 2024
|