FLIGHT TEST HINGE ASSEMBLY
A system for calculating forces exerted into an aircraft component (12) may include a test hinge assembly (10) and a monitoring system (18). The test hinge assembly (10) may be a triangular shaped assembly, and may include at least one beam 22, 24, 28, at least one connecting joint 26, 34, 42 having...
Saved in:
Main Authors | , , , , |
---|---|
Format | Patent |
Language | English French German |
Published |
13.01.2016
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Be the first to leave a comment!