ABS 61 NOTICE 1-2017 RULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT 2017.pdf
《ABS 61 NOTICE 1-2017 RULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT 2017.pdf》由会员分享,可在线阅读,更多相关《ABS 61 NOTICE 1-2017 RULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT 2017.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、 RULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT 2017 NOTICE NO. 1 July 2017 The following Rule Changes were approved by the ABS Rules Committee on 30 May 2017 and become EFFECTIVE AS OF 1 JULY 2017. (See http:/www.eagle.org for the consolidated version of the Rules for Building and Classing High-S
2、peed Craft 2017, with all Notices and Corrigenda incorporated.) Notes - The date in the parentheses means the date that the Rule becomes effective for new construction based on the contract date for construction, unless otherwise noted. (See 1-1-4/3.3 of the ABS Rules for Conditions of Classificatio
3、n High-Speed Craft (Part 1).) PART 3 HULL CONSTRUCTION AND EQUIPMENT CHAPTER 2 HULL STRUCTURES AND ARRANGEMENTS SECTION 8 RUDDERS AND STEERING EQUIPMENT 17 Double Plate Rudder (Revise Paragraph 3-2-8/17.1 and add new 3-2-8/Figures 5, 6, and 7, as follows:) 17.1 Strength (1 July 2017) The section mod
4、ulus and web area of the rudder mainpiece are to be such that the stresses indicated in the following Subparagraphs are not exceeded. In calculating the section modulus of the rudder, the effective width of side plating is to be taken as not greater than twice the athwartship dimension of the rudder
5、. Bolted cover plates on access openings to pintles are not to be considered effective in determining the section modulus of the rudder. In order for a cover plate to be considered effective, it is to be closed using a full penetration weld and confirmed suitable by non-destructive testing method. G
6、enerous radii are to be provided at abrupt changes in section where there are stress concentrations, including in way of openings and cover plates. When inspection windows are located in the panel below the rudder hub, the stress is to be as permitted in way of cutouts. Moments, shear forces and rea
7、ction forces are to be as given in 3-2-8/7.7 and 3-2-8/13.5. For spade rudders and rudders with horns, the section modulus at the bottom of the rudder is not to be less than one-third the required section modulus of the rudder at the top of the rudder or at the center of the lowest pintle. Special a
8、ttention is to be paid in design and construction of rudders with slender foil sections in the vicinity of their trailing edge (e.g., hollow foil sections, fishtail foil sections). Where the width of the rudder blade at the aftermost vertical diaphragm, w, is equal or less than 1/6of the trailing ed
9、ge length measured between the diaphragm and the trailing edge, , finite element vibration analysis of the rudder blade is also to be submitted for review. See 3-2-8/Figure 5. ABSRULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT .2017 1 Notice No. 1 July 2017 FIGURE 5 (1 July 2017) wSpade rudders wit
10、h an embedded rudder trunk are to have a trailing edge with dimensions that satisfy the following requirements: i) For a rudder trailing edge having a monotonous transition to a rounded end with a finite thickness or diameter (see 3-2-8/Figure 6), the vortex shedding frequency calculated using the e
11、quation given below is to be higher than 35 Hz. fs= TDUSTDt +where fs= vortex shedding frequency, in Hz U = flow velocity, in m/s (ft/s), which is taken as crafts design speed with craft running ahead at the maximum continuous rated shaft rpm and at the summer load waterline St= nominal Strouhal num
12、ber = 0.18 D= 0.27 C = minimal chord length of rudder cross section profile, in m (ft) D = nominal boundary layer thickness at trailing edge = 0.01C T= 0.77 T = thickness or diameter of rounded end, in m (ft) FIGURE 6 (1 July 2017) Thickness or Diameter of Rounded End2 ABSRULES FOR BUILDING AND CLAS
13、SING HIGH-SPEED CRAFT .2017 Notice No. 1 July 2017 ii) For a rudder trailing edge with a flat insert plate (see 3-2-8/Figure 7), the insert plate thickness, t0, is to be no larger than 1.5Vdin mm, where Vdis the design speed in ahead condition, in knots, as defined in 3-2-8/3.1. The extension beyond
14、 the weld to rudder plate, , is to satisfy the following 3-2-8/Figure 7 and with consideration of possible local vibratory bending of the insert plate. FIGURE 7 (1 July 2017) Insert Plate Thicknesst0Rudder Plate Thicknesst1 (t0+ 2t1)Alternatively, a vibration analysis is to be carried out to confirm
15、 that the natural frequency of the rudder is to be at least 20% away from the vortex shedding frequency preferably determined using either a detailed numerical analysis method such as CFD or testing for ballast and full draft at 85% and 100% Vdas defined in 3-2-8/3.1. (Renumber existing 3-2-8/Figure
16、s 5 and 6 as 3-2-8/Figures 8 and 9.) (Revise Subparagraph 3-2-11/17.1.2, as follows:) 17.1.2 In way of Cut-outs (1 July 2017) Allowable stresses for determining the rudder strength in way of cutouts (see 3-2-8/Figure 8) are as follows: Bending stress b= K/Q N/mm2(kgf/mm2, psi) Shear stress = K/Q N/m
17、m2(kgf/mm2, psi) Equivalent stress e= 223 +b= Ke/Q N/mm2(kgf/mm2, psi) where SI units MKS units US units K75 7.65 10,900 K50 5.1 7,300 Ke100 10.2 14,500 Q = as defined in 3-2-1/1.1.1 ABSRULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT .2017 3 Notice No. 1 July 2017 FIGURE 8 Z6r26r16r1r26r2XNote:r1=
18、corner radius of rudder plate in way ofportable bolted inspection holer2= corner radius of rudder plateIn way ofcutoutsr1The mainpiece of the rudder is to be formed by the rudder side plating (but not more than the effective width indicated above) and vertical diaphragms extending the length of the
19、rudder or the extension of the rudder stock or a combination of both. PART 4 CRAFT SYSTEMS AND MACHINERY CHAPTER 3 PROPULSION AND MANEUVERING MACHINERY SECTION 3 STEERING GEAR 11 Steering Gear Control System 11.3 General (Add new Subparagraph 4-3-3/11.3.5, as follows:) 11.3.5 System Response Under F
20、ailure (1 July 2017) The failures (as listed, but not limited to items in 4-3-3/11.9) likely to cause uncontrolled movements of rudder are to be clearly identified. In the event of detection of such failure, the rudder should stop in the current position. Alternatively, the rudder may be set to retu
21、rn to the midship/neutral position. Failure Mode and Effect Analysis methodology may be used to identify the failures. 4 ABSRULES FOR BUILDING AND CLASSING HIGH-SPEED CRAFT .2017 Notice No. 1 July 2017 11.9 Instrumentation and Alarms (Revise Subparagraph 4-3-3/11.9.7, as follows:) 11.9.7 Low Oil Lev
22、el Alarm (1 July 2017) A visual and audible alarm is to be given on the navigation bridge and engine room control station to indicate a low oil level in any power unit reservoir. The operation of this alarm is not to interrupt the power supply circuit. (Add new Subparagraph 4-3-3/11.9.12, as follows
23、:) 11.9.12 Earth Fault (1 July 2017) A visual and audible alarm is to be given on the navigation bridge to indicate an earth fault on AC and DC circuits (Add new Subparagraph 4-3-3/11.9.13, as follows:) 11.9.13 Deviation (1 July 2017) Where arrangements discussed in 4-3-3/11.9.8, 4-3-3/11.9.9, 4-3-3
24、/11.9.10 and 4-3-3/11.9.11 can lead to reduced or erroneous system performance of the commanded change in rudder angle, a deviation alarm visible and audible at the navigating bridge shall be initiated if the rudders actual position does not reach the set point within acceptable time limits for the
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
5000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- ABS61NOTICE12017RULESFORBUILDINGANDCLASSINGHIGHSPEEDCRAFT2017PDF

链接地址:http://www.mydoc123.com/p-400919.html