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Trans RINA, Vol 157, Part C1, Intl J Marine Design, Jan - Dec 2015 


below the water line to give a 3 .5m clearance over the vessel’s 2m draft in a sea state of 2.5m Hs. The WFSV is driven onto the bollards under partial throttle to constrain vessel motion. The beam has a design factor of 5 against shearing under tors avoid excess deflection. Once the WFSV motion is constrained the lifting cradle will be raised into contact with underside of the catamaran hulls.


sion to


The FEA analysis of an initial proposal for a bollard beam is shown in Figure 24. Where the Design Factor of 4 has been achieved for UKB steel I-beam with Max stress = 63.6MPa. The horizontal b


beam in high sea states, combined wiith the


technical challenges of implementing a system in the demi-hulls to retract the bollard beam from th we water, brought the feasibility of the solution into question.


risk of hull impact on the


Figure 26: FEA of modified lifting frame design Weight =


Max stress


= 295kN s = 62MPa


Design factor = 4.2


4.1 LAUNCH/RECOVERY DESIGN SOLUTION This initial proposal highlighted two of the key design


challenges. The first being the need to hold the vessel sufficiently above the waterline in high sea state, the significant moment effect off suspending 120 tons at the ack of the SWATH require a significant amount of betwe en


ba ba


allast. This proposal was a compromise Figure 24: FEA of initial bollard beam proposal


The lifting cradle has a design factor of 2.5 and is constructed from universal beams. The initial design shown in Figure 25 with four lifting points had a weight of 45 tonnes, which is over 50% of the load initially required to be lifted. The modified design shown in Figure 26 increased the number of lifting points to six. This redistributed the loading enabling the weight of these beams to be significantly reduced, reducing the overall weight of the frame to 31 tonnes.


Figure 27: WFSV on approac ch to SOV


available height of the wet deck above waterline while maintaining ve ssel stability and the motion of the WFSV in 2.5mHs+ during lifting using the rear area. The revis ed design proposal shown in Figure 27 has a watertight loading bay from which vertically.


h the WFSV is launched


Figure 25:FEA of initial lifting frame design Weight = 437kN


Max stress = 106MPa Design factor = 2.4 7


Figure 28: View of lifting frame in loading bay © 2015: The Royal Institution of Naval Architects C-117


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