Helicopter blade dynamic balance experiment platform hinge moment parameter correction method

Helicopter blade dynamic balance experiment platform hinge moment parameter correction method

The invention belongs to the helicopter blade dynamic balance experiment platform measurement technology field and provides a helicopter blade dynamic balance experiment platform hinge moment parameter correction method. The method comprises the following steps of acquiring a moment difference value...

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Hauptverfasser: XIA XIAODONG, SHI YUE, XUE WEISONG, YANG SHITAO, ZHANG JUNMING, LI HUIBIN
Format: Patent
Sprache:eng
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MEASURING
MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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creator XIA XIAODONG
SHI YUE
XUE WEISONG
YANG SHITAO
ZHANG JUNMING
LI HUIBIN
description The invention belongs to the helicopter blade dynamic balance experiment platform measurement technology field and provides a helicopter blade dynamic balance experiment platform hinge moment parameter correction method. The method comprises the following steps of acquiring a moment difference value of a second propeller hub and a first propeller hub and a moment difference value of a third propeller hub and the first propeller hub; using (L-H) and (R-H) to replace a counterweight system of a helicopter blade dynamic balance rotor head to correct a hinge moment of batch production blades.
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subjects MEASURING
MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
title Helicopter blade dynamic balance experiment platform hinge moment parameter correction method
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