Optical fiber arrangement and bridge-forming method for helicopter rotor composite load test
A helicopter rotor and composite load technology, applied in the direction of aircraft component testing, etc., can solve problems such as life limitation, and achieve the effects of small size, good economic benefits and long life.
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[0027] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention.
[0028] In the blade load detection process, the load monitoring requirements for the specific section of the blade are generally put forward for the airfoil shape and mass distribution of the helicopter blade, including the strain loads in the upward swing and shimmy directions of the blade. Determine the load monitoring surface and monitoring content of the rotor system, and put forward specific scope and requirements for the position and arrangement of the measuring optical fiber.
[0029] For above-mentioned requirements, the present invention provides a kind of helicopter rotor composite load test optical fiber arrangement and bridge assembly method, and it comprises:
[0030] 1) Fi...
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