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プロペラへの気泡流入状況観察結果ならびに考察

ドキュメント内 九州大学学術情報リポジトリ (ページ 163-170)

Fig.B.8: Pattern of bubbly flow on ship bottom

Fig.B.9: Bubbly flow into propeller

表目次

1.1 List of ships installed with air lubrication system. . . 10

3.1 Condition of air blowing test in the cavitation tunnel. . . 27

3.2 List of baffle plate. . . 32

4.1 Principal particulars of ship. . . 56

4.2 Energy saving effect. . . 76

4.3 energy saving effect (F.O. consumption). . . 78

5.1 Positions of shear force sensors and void fraction sensors on 15 m long model. 84 5.2 Positions of shear forces sensors and void fraction sensors on round model. . . 85

5.3 15 m long model test conditions. . . 87

5.4 Round model test conditions. . . 87

6.1 Principal particulars of “Ferry NAMINOUE”. . . 99

6.2 Voyage schedule from Kagoshima to Okinawa. . . 106

6.3 Approximation coefficient of fuel oil consumption (F OC =aVp0+b). . . 112

7.1 Air lubrication system design conditions and blower speciffications. . . 116

7.2 Air lubrication system components. . . 120

A.1 Princupal particulars of tested propeller . . . 139

B.1 Experimental conditions of visualization of bubbly flow . . . 149

図目次

1.1 Relationship between EEDI reduction rate and regulation value to be attained

by ships [1]. . . 2

1.2 Bubble Injection Device (SEIUN MARU [9]). . . 6

1.3 Effect of mean bubble diameter on frictional resistance reduction [43]. . . 7

1.4 Comparison of bubble diameter and frictional resistance reduction effect [54]. 8 1.5 Comparison of frictional resistance reduction effect by Madavan et al. [26] and Kawakita et al. [42]. . . 8

1.6 ACS Demonstrator the first vessel with Air Cavity System [65]. . . 10

1.7 Large scale protptype model of the Stena Airmax [66]. . . 11

2.1 Schematic diagram of full scale ship power estimation with bubble flow drag reduction system [75]. . . 17

2.2 Definition of area covered with air bublles. . . 18

2.3 Approximation curve of skin friction coefficient [68]. . . 19

2.4 Example of energy consumption reductuin effect estimation worksheet. . . 21

3.1 Dimension of air hole. . . 26

3.2 Model of air blowing hole. . . 26

3.3 Arrangement of cavitation tunnel. . . 27

3.4 Photograph of air blowing situation. . . 29

3.5 Air blowing and diffusing situation. . . 30

3.6 Outline drawing of chamber model. . . 31

3.7 Inside of the chamber model. . . 32

3.8 Test Model of Baffle plates. . . 33

3.9 Test Model of perforated panel. . . 34

3.10 Test Model of cup. . . 34

3.11 Number of holes and Measurement position of hole. . . 35

3.12 Result of air blow test of chamber. . . 36

3.13 Sellected baffle pltaes from experiment result. . . 37

3.14 Mock-up of air chamber and recess. . . 37

3.15 Photograph of the experiment. . . 38

3.16 Air blow for mock-up model(heel angle is 0 deg). . . 38

3.17 Air blow for mock-up model(heel angle is 3 deg). . . 39

3.18 Flow diagram. . . 40

3.19 Comparison of flow rate distribution. . . 41

3.20 Analytical result of flow rate distribution (All valves are fully opened). . . 42

3.21 Analytical result of flow rate distribution (Flow rate is equally distributed under minimum valve pressure loss). . . 43

3.22 Analytical result of flow rate distribution (Heel angle is 3degrees (port side down)). . . 44

3.23 Analytical result of flow rate distribution (Valve opening is adjusted as the distribution of flow rate becomes even). . . 44

3.24 Analytical result of flow rate distribution (All valve openings are 60 deg). . . . 45

3.25 Analytical result of flow rate distribution (Valve opening are linearly varied from starboard to port). . . 46

3.26 Comparison of valve opening and flow rate (Without Heeling). . . 48

3.27 Comparison of valve opening and power of blower. . . 48

3.28 Comparison of valve opening and flow quantity (Heel angle is 1.8 degrees to-ward starboard). . . 49

3.29 Air blow of full-scale ship. . . 50

3.30 Relation between pressure loss and vale opening angle. . . 51

3.31 Analytical and measured result of flow rate distribution. . . 52

4.1 Modular carrier ship YAMATAI . . . 54

4.2 Image figure of Air Lubrication Method. . . 55

4.3 Towed vehicle for ship bottom observation. . . 57

4.4 Observation method by towed vehicle. . . 58

4.5 Observation point by towed vehicle. . . 58

4.6 Propeller observation cameras. . . 59

4.7 Shear stress sensor. . . 60

4.8 Sensor arrengement on ship bottom. . . 60

4.9 Sensor position of propeller pressure fluctuation measurements. . . 61

4.10 Sensor position of hull vibration measurements. . . 62

4.11 Air blow for full-scale ship. . . 63

4.12 Experimental result of air blow. . . 63

4.13 Observation results of ship bottom during operation (VS=abt.7kn). . . 64

4.14 Observation results of ship bottom during operation (VS=abt.7kn and 10kn). 65

4.15 Comrarison of the void fraction distribution. . . 66

4.16 Situatuin of bubble flow. . . 67

4.17 Results of propeller observation (OFF). . . 68

4.18 Results of propeller observation (ON). . . 68

4.19 Trend data shear stress and water speed (Results of ship bottom observation). 69 4.20 Results of ship bottom observation at Point 6 (Vs=9.8 kn, ONOFF). . . . 70

4.21 Local skin friction reduction with operation. . . 71

4.22 Correlation between drag reduction and air layer thickness(NMRI)) [86]. . . . 72

4.23 Results of propeller pressure fluctuation measurements at 3.500 kW. . . 73

4.24 Results of propeller pressure fluctuation measurements at 5.000 kW. . . 73

4.25 Results of hul vibration measurements at 3500 kW. . . 75

4.26 Results of Speed Trial. . . 77

4.27 Comparison of F.O. consumption. . . 78

5.1 Photograph of the 15 m flat plate model. . . 82

5.2 Top and side views of the 15 m long model with shear force sensors and void fraction sensors. . . 82

5.3 Side views of the stern part of 15 m long model. . . 83

5.4 Photograph of the void fraction sensor. . . 83

5.5 Top, side and front views of the round model with shear force sensors and void fraction sensors. . . 85

5.6 Photograph of hull posture suppression guide. . . 86

5.7 Photographs of 15 m long model towing test at 9 m/s. . . 88

5.8 Comparison of local skin friction effect in slope angle of 5 deg model due to change in distance from air injector. . . 89

5.9 Comparison of local skin friction effect in slope angle of 10 deg model due to change in distance from air injector. . . 89

5.10 Distribution of pressure coefficientCp at port side bottom of 15 m long model by double model flow CFD. . . 90

5.11 Comparison of local void fraction distribution near wall surface in slope angle of 5 deg and 10 deg model. . . 91

5.12 Photographs of round model towing test at 9 m/s. . . 92

5.13 Streamlines near port side bottom of round model by double model CFD. . . 92

5.14 Distribution of pressure coefficient Cp at port side bottom of round model by double model flow CFD. . . 93

5.15 Comparison of local skin friction effect in round model due to change in

dis-tance from air injector. . . 93

5.16 Comparison of local void fraction distibution near wall surface at 7 m/s and 9 m/s in round model due to change in equivalent air layer thicknees. . . 94

5.17 Comparison of local void fraction distibution near wall surface at 7.5 mm equiv-alent air layer thicknees in round model due to change in towing speed. . . . 95

6.1 “Ferry NAMINOUE 8,072GT cargo-passenger ship and car ferry. . . 98

6.2 Blower for air lubrication system. . . 99

6.3 Path of ship during typical speed/power maneuver. . . 101

6.4 Comparison of ALS OFF and ON wakes. . . 101

6.5 Speed-Power curves for verification of power savings. . . 102

6.6 Propeller-induced pressure increase ratio of ALS ON to OFF. . . 103

6.7 Hull vibration increase ratio of ALS ON to OFF. . . 104

6.8 Comparison of specific fuel oil consumption. . . 105

6.9 Correlation of ship speed and BHP (Kagoshima-Naze Route). . . 107

6.10 Correlation of propller speed and BHP (Kagoshima-Naze Route). . . 107

6.11 Comparison between fuel consumption and engine output. . . 108

6.12 Comparison of mean propeller speed between F. Naminoue and F. Akebono. . 109

6.13 Correlation of propller speed and fuel oil consumption (Kagoshima-Naze Route).110 6.14 Correlation of propller speed and fuel oil consumption (Naze-Kametoku Route).110 6.15 Correlation of propller speed and fuel oil consumption (Kametoku-Wadomari Route). . . 110

6.16 Correlation of propller speed and fuel oil consumption (Wadomari-Yoron Route).111 6.17 Correlation of propller speed and fuel oil consumption (Yoron-Motobu Route). 111 6.18 Correlation of propller speed and fuel oil consumption (Motobu-Naha Route). 111 6.19 Relation between total electoric power and fuel flow rate. . . 113

7.1 Structual drawing of MTA. . . 117

7.2 Operation range of MTA. . . 117

7.3 Location of air outlets. . . 118

7.4 Example of chamber configuration. . . 119

7.5 Arrangement and shape of opening(bottom plan). . . 119

7.6 Outline arranegement of air lubrication system. . . 120

7.7 Example of installation of air lubrication system on a ferry. . . 121

7.8 Example of installation study of air lubrication system on mega container ship. 122 7.9 Example dry-dock schedule of retorofitting air lubrication system. . . 123

ドキュメント内 九州大学学術情報リポジトリ (ページ 163-170)