Aircraft quality characteristic simple measuring device and measuring method
A technology of quality characteristics and measuring devices, which is applied in the field of simple measurement devices for aircraft quality characteristics, can solve problems such as high cost, complicated measurement methods, and expensive measurement equipment, and achieve the effect of reliable methods and simple operations
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[0043] Example 1:
[0044] See figure 1 , A simple measurement device for aircraft quality characteristics, including a horizontal measurement platform 1 on which two support mechanisms are installed. The support mechanism includes a base and two hydraulic telescopic rods 2 vertically fixed on the base. The top of the hydraulic telescopic rod 2 is installed with a horizontal beam 3, the outer wall of the beam 3 is sleeved with a plurality of sleeves 4, the bottom of the outer wall of the sleeve 4 is fixed with a universal joint 5, and a hoisting rope is provided on the universal joint 5.
[0045] In this embodiment, the crossbeam 3 and the hydraulic telescopic rods 2 of the two supporting mechanisms form a gate-shaped structure. The bottom of the sleeve 4 on the outer wall of the crossbeam 3 is installed with a hoist rope through a universal joint 5 to hang the aircraft and extend it. The hydraulic telescopic rod 2 is hoisted with simple operation and low cost.
[0046] The sleeve ...
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[0074] Example 2
[0075] Such as Figure 5 with Image 6 , On the basis of Example 1, that is, the moment of inertia I of the aircraft measured when the two suspension ropes are parallel to the z-axis or the y-axis and are at the same distance from the z-axis or the y-axis z Or I y . However, this is often not possible in actual measurement. Sometimes it is difficult to find the position where the frame can be stuck to the front and rear fuselage at the same distance before and after the center of mass of the aircraft. It is necessary to make the position of the front and rear frames asymmetrical to the center of mass, so that the two The z-axis or y-axis represented by the center line of the sling is different from the zˊ-axis or yˊ-axis passing through the actual center of mass of the aircraft respectively by L z Or L y ; Or due to the difference between the actual center of mass of the aircraft and the theoretical center of mass during the deployment process, the z ˊ axis or y...
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