Static balancing method of whole propeller combination of adjustable pitch propellers
A technology of static balance and controllable pitch propellers, which is applied in the field of static balance of controllable pitch propellers and marine adjustable pitch propellers. It can solve the problems of narrow application range and difficult operation, and achieve convenient operation , Improve production efficiency, save judgment time
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[0028] Example 1:
[0029] In the following, a five-blade propeller is taken as an example to further illustrate a method of static balance of the entire propeller combination of a controllable pitch propeller.
[0030] The weight of the entire propeller of the propeller: 12635kg, propeller diameter: 4.1m, speed: 208r / min, manufacturing accuracy: IS0484, class I, the unbalanced moment Mp of the entire propeller is 7301.1kgmm
[0031] First, the unbalance value M1 of the hub assembly 1 is 1825.3kgmm measured according to the above method.
[0032] Then measure the unbalance value M2 of the blade group, the steps are as follows:
[0033] The static balance test data of each blade is as follows:
[0034] Numbering
[0035] See image 3 , P is the weight of each blade, Y is the distance from the center of gravity of the blade to the centerline d of the controllable pitch propeller, and Z is the distance from the center of gravity of the blade to the centerline c of the blade. For the fiv...
Example Embodiment
[0082] Example 2:
[0083] In the following, a four-blade propeller is taken as an example to further illustrate a method of static balance of the entire propeller combination of a controllable pitch propeller.
[0084] The weight of the entire propeller of the four-blade propeller: 11530kg, propeller diameter: 4.2m, speed: 179.3r / min, manufacturing accuracy: IS0484, class I. The unbalanced moment Mp of the whole propeller: 8966.3kgmm.
[0085] First, the unbalance value M1 of the hub assembly 1 is 2241.6kgmm measured according to the above method.
[0086] Then measure the unbalance value M2 of the blade group, the steps are as follows:
[0087] The static balance test data of each blade is as follows:
[0088] Numbering
[0089] See image 3 , P is the weight of each blade, Y is the distance from the center of gravity of the blade to the centerline d of the propeller, and Z is the distance from the center of gravity of the blade to the centerline c of the blade. For a four-blade p...
Example Embodiment
[0115] Example 3:
[0116] In the following, a three-blade propeller is taken as an example to further illustrate a method of static balance of the entire propeller combination of a controllable pitch propeller.
[0117] The weight of the entire propeller of the three-blade propeller: 9630kg, propeller diameter: 4.1m, speed: 208r / min, manufacturing accuracy: IS0484, class I, and the unbalanced moment Mp of the entire propeller: 5564.7kgmm.
[0118] First, the unbalance value M1 of the hub assembly 1 is 1391.2kgmm measured according to the above method.
[0119] Then measure the unbalance value M2 of the blade group, the steps are as follows:
[0120] The static balance test data of each blade is as follows:
[0121] Numbering
[0122] See image 3 , P is the weight of each blade, Y is the distance from the center of gravity of the blade to the centerline d of the controllable pitch propeller, and Z is the distance from the center of gravity of the blade to the centerline c of the blad...
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