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...

Full description

Saved in:
Bibliographic Details
Main Authors WILLIAMS, JAMES A, OELKE, BRIAN S, DICKERSON, MATT R, JOHNSON, ROBERT, AMINZADEH, SHAHZAD
Format Patent
LanguageEnglish
French
German
Published 13.01.2016
Subjects
Online AccessGet full text

Cover

Loading…