Optics: measuring and testing – Material strain analysis – With polarized light
Patent
1986-05-15
1987-08-25
Willis, Davis L.
Optics: measuring and testing
Material strain analysis
With polarized light
250225, 250231SE, 356364, G01B 1116
Patent
active
046889345
ABSTRACT:
A system for measuring aeroelastic deformation of an aircraft wing in flight or in a wind tunnel utilizing light from a linearly polarized light source (101). The light is transmitted through modulating elements (104, 105) to provide a carrier beam, and a small portion of the beam is reflected through a linear polarizer (107) into a photo-detector (108) for utilization as a reference electrical signal (208). The remainder of the beam is reflected back from a retro-reflector target (700) located on the wing into another photo-detector (114) to provide the target electrical signal (209). The two amplified electrical signals are compared in a phase detector (FIG. 3) for providing an angle measurement output signal E.sub.0.
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Donahue B. A.
Gardner Conrad O.
Koren Matthew W.
The Boeing Company
Willis Davis L.
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