• Chinese Journal of Ship Research
  • Vol. 17, Issue 6, 70 (2022)
Qiongfang YANG1, Rui WU2, Minmin ZHENG2, Xuequan MA2..., Heng LIU2 and Yilin YANG2|Show fewer author(s)
Author Affiliations
  • 1College of Power Engineering, Naval University of Engineering, Wuhan 430033, China
  • 2Shanghai Ship and Shipping Research Institute Co., Ltd., Shanghai 200137, China
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    DOI: 10.19693/j.issn.1673-3185.02600 Cite this Article
    Qiongfang YANG, Rui WU, Minmin ZHENG, Xuequan MA, Heng LIU, Yilin YANG. New method for predicting full-scale power performance of pumpjet propulsion system based on statistical learning[J]. Chinese Journal of Ship Research, 2022, 17(6): 70 Copy Citation Text show less

    Abstract

    Objectives

    Aiming at the replacement of propellers behind surface ships with pumpjet propulsion systems, this paper introduces a novel method for predicting full-scale power performance based on statistical learning.

    Methods

    Pump performance maps originating from the neural network learning of existing pumpjet thrust coefficient maps and matched to a ship's drag line from model tests are used to determine the pumpjet's full-scale power performance behind a large surface ship. To validate its precision and availability, traditional complete model tests including the ship model drag test, pump model open water test and ship-pumpjet self-propulsion test are completed to determine the full-scale benchmark power performance under different ship speeds.

    Results

    The prediction errors of the pumpjet's rotation speed, thrust and power under different self-propulsion ship speeds from 18 knots to the design point of 30 knots are smaller than 5.4%, with no more than 2% from the design condition. As for the ship-propulsor interaction amplitude, the surface ship-pumpjet subsystem lies between ship-propeller interaction and ship-waterjet pump interaction with a thrust deduction coefficient approaching zero. From this point of view, the pumpjet propulsion system behind a surface ship can be recognized as a transitional stage from the propeller-shaft configuration to the waterjet propulsion system.

    Conclusions

    The method proposed herein can predict the full-scale power performance of a pumpjet propulsion system behind a ship while advancing pumpjet propulsion system design and applications for new large-scale surface warships.

    $ {T_{\text{p}}} = \frac{R}{{{k_{\text{p}}} \cdot (1 - t)}} = \frac{{{C_1} \cdot V_{\text{A}}^{\text{2}}}}{{{k_{\text{p}}} \cdot (1 - t) \cdot {{(1 - w)}^2}}} = {C_2} \cdot V_{\text{A}}^{\text{2}} $(1)

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    $ {K_{{T \text{,ship}}}} = \frac{{{C_2} \cdot V_{\text{A}}^{\text{2}}}}{{\rho n_{\text{p}}^{\text{2}}D_{\text{p}}^{\text{4}}}} = \frac{{{C_2}}}{{\rho D_{\text{p}}^{\text{2}}}} \cdot {J^2} = {C_3} \cdot {J^2} $(2)

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    $ J = \frac{{{V_{\text{A}}}}}{{{n_{\text{p}}}{D_{\text{p}}}}} \text{,} {K_{{T}}} = \frac{{{T_{\text{p}}}}}{{\rho n_{\text{p}}^{\text{2}}D_{\text{p}}^{\text{4}}}} \text{,} {K_{{Q}}} = \frac{{{Q_{\text{p}}}}}{{\rho n_{\text{p}}^{\text{2}}D_{\text{p}}^5}} \text{,} {\eta _0} = \frac{J}{{2{\text{π }}}} \cdot \frac{{{K_{{T}}}}}{{{K_{{Q}}}}} $(3)

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    $ {n_{\text{p}}} = \frac{{{V_{\text{A}}}}}{{J \cdot {D_{\text{p}}}}} = \frac{{(1 - w)}}{{J \cdot {D_{\text{p}}}}} \cdot {V_{\text{s}}} = {C_4} \cdot {V_{\text{s}}} $(4)

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    $ \varphi = \frac{Q}{{\varOmega {D^3}}} = \frac{{{V_{{\text{pump}}}}}}{{8nD}} = \frac{{{V_{{\text{in}}}}}}{{8nD \cdot IVR \cdot (1 - w)}} = \frac{J}{{8IVR \cdot (1 - w)}} $(5)

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    $ {n_{\text{ω }}} = \frac{{\varOmega \sqrt Q }}{{{{(gH)}^{3/4}}}} \text{,} {n_{{\text{ω s}}}} = \frac{{\varOmega \sqrt Q }}{{{{(gNPS{H_{\text{r}}})}^{3/4}}}} $(6)

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    $ {{\textit{z}}_{{\text{RTF}}}} = {\textit{z}_{{\text{TF}}}} \cdot \left(\frac{{{C_{{\text{fm}}}}}}{{{C_{{\text{fs}}}}}} - 1\right){\text{ = }}\frac{1}{2}\rho \cdot \Delta {C_{\text{f}}} \cdot V_{\text{m}}^{\text{2}} \cdot {S_{\text{m}}} \cdot \left(\frac{{{C_{{\text{fm}}}}}}{{{C_{{\text{fs}}}}}} - 1\right) $(7)

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    $ \alpha = \frac{P}{{{n^3}{D^5}}} \text{,} {K_{{T\text{J}}}} = \frac{T}{{{n^2}{D^4}}} \text{,} {J_{\text{J}}} = \frac{{{V_{\text{s}}}}}{{nD}} $(8)

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    $ {\tau _{\text{c}}} = \frac{{{T_{{\text{cav}}}}}}{{AV_{\text{s}}^{\text{2}}}} \text{,} \sigma = \frac{{{p_0} - {p_{\text{v}}}}}{{\rho V_{\text{s}}^{\text{2}}}} $(9)

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    Qiongfang YANG, Rui WU, Minmin ZHENG, Xuequan MA, Heng LIU, Yilin YANG. New method for predicting full-scale power performance of pumpjet propulsion system based on statistical learning[J]. Chinese Journal of Ship Research, 2022, 17(6): 70
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