Section 3 Local hull loads and strength
Clasification Society 2024 - Version 9.40
Clasifications Register Rules and Regulations - Rules for the Classification of Air Cushion Vehicles, July 2022 - Chapter 3 Hull Structures - Section 3 Local hull loads and strength

Section 3 Local hull loads and strength

3.1 Impact loads on the bottom and side shell

3.1.1 The peak pressure at any point along the length of the bottom structure is given by:

p peak = 0,62K 2 V v V kN/m2

where

K 2 = – 2 for x/L > 0,75
K 2 = 1,0 for x/L ≤ 0,75
x = distance from aft end to the point at which K 2 is required, in metres

V, V v as defined in Ch 3, 2.2 Acceleration due to wave impact 2.2.2

L is defined in Ch 1, 1.2 Definitions and symbols.

3.1.2 The distributed pressure, p dist, along the length of the bottom structure is taken as 0,44 times the peak pressure, ppeak.

3.1.3 The peak pressure, p peak, is generally to be applied to plating and secondary stiffeners. The distributed pressure p dist, is generally to be applied to primary frames, girders and large unstiffened panels of plating, and over an impact area, Aw,i, taken as:

where

Fw,i is defined in Ch 3, 2.3 Structural response to wave impact 2.3.2.

3.1.4 Both the peak pressure and distributed pressure are to be applied to the bottom structure to the transverse extent of the outermost chine. Above this point both pressures may be reduced linearly to pressure, p gun, at the gunwale.

p gun = kN/m2

where

K 3 = – 0,5 for x/L > 0,75
K 3 = 1,0 for x/L ≤ 0,75
x = distance from aft end to the point at which K 3 is required, in metres

L is defined in Ch 1, 1.2 Definitions and symbols

a v,i is defined in Ch 3, 2.2 Acceleration due to wave impact 2.2.2 for the longitudinal centre of gravity impact case and is not to be taken less than 1,0.

3.2 Floating loads

3.2.1 In addition to the loads given in Ch 3, 3.1 Impact loads on the bottom and side shell, local loads acting on the bottom and side shell when the ACV is off-cushion and floating whilst underway at the maximum towing speed will be specially considered in accordance with Pt 5, Ch 4, 3 Hull envelope design criteria of the SSC Rules.

3.3 Deck loads

3.3.1 Local loads acting on the decks are to be specially considered in accordance with the requirements of Pt 5, Ch 4 Local Design Criteria for Craft Operating in Displacement Mode of the SSC Rules.

3.4 Machinery loads

3.4.1 Machinery foundation reactions resulting from collision accelerations, torque and dynamic loads are to be provided by the designer.

3.4.2 The loadings mentioned in Ch 3, 3.4 Machinery loads 3.4.1 are to be used additionally to assess the attachment of resilient mounts where fitted.

3.5 Slinging and jacking loads

3.5.1 The supporting structure, such as lifting posts and struts, is to be designed to carry the slinging and jacking loads at each lifting point and is to have adequate buckling capacity to withstand the concentrated loads. Allowance is to be made for the inclination of any lifting wires which may give rise to longitudinal, transverse and vertical loads.

3.6 Collision loads

3.6.1 The strength of supporting structure and attachments of masses greater than 50 kg are to be able to withstand design accelerations without fracturing. Force magnitudes and directions are to be taken as follows:

  • 6g forward direction.
  • 3g after direction.
  • 3g transverse direction.
  • 3g vertical upward direction.
  • 4g vertical downward direction.

The vertical acceleration cases include the self-weight component.

3.7 Local strength

3.7.1 When applying the loads given in this Section, strength models based on simple plate bending, beam theory, or other recognised methods will generally be acceptable. Where longitudinal and transverse stiffeners form grillage structures providing mutual support, or where the structural arrangement is complex, finite element or alternative methods may have to be used and are to be agreed with LR prior to submission. Consideration is to be given to assumptions regarding end fixity and load application as appropriate for the selected method.

3.7.2 Laterally loaded thin skins designed to support the design pressure by membrane action with associated large deflections will be specially considered, see also 2.7.5. For guidance, the thickness of thin skins, t skin, may be derived as follows:

t skin = mm

3.7.3 where

p = design pressure, in kN/m2
a = longest dimension of the skin, in m
b = shortest dimension of the skin, in m
σa = 0,2 per cent proof stress of the aluminium, in N/mm2
η = 0,0085α2 – 0,1025 α + 0,5
α = a/b
E = modulus of elasticity, in N/mm2

3.7.4 Structural geometry is to be arranged and detailed to ensure a smooth transfer of loads throughout the structure. Concentrated or point loads are to be transmitted into the supporting structure by a series of stiff supporting members. In no case are concentrated or point loads to land on unsupported plating.

3.7.5 The longitudinal girders forming the machinery foundations are to extend as far forward and aft as practicable and be adequately supported by transverse primary structure.

3.7.6 Integration of lift fans and associated supporting structure will be specially considered.

3.7.7 In areas where fluctuating pressure (panting) occurs e.g. fan bays, inlets, volutes etc. design details will be specially considered.

3.7.8 Openings in the structure are to be suitably framed and have well-rounded corners to minimise stress concentrations.


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