发明名称 SHOCK ABSORBING COCKPITS
摘要 A watercraft cockpit includes a floor, sidewalls and forward and rearward bulkheads. A frame assembly having four corners supports the cockpit and includes an upper frame and a lower frame that are rotatably connected to one another. A pair of shock-absorbing members is provided at each of the four corners of the frame so that the entire cockpit is isolated from shocks. By cushioning the entire cockpit as a whole, the need for individual shock-absorbing seats is obviated. The walls of the cockpit are spaced apart from the sidewalls of the watercraft and are interconnected to the sidewall of the watercraft by a flexible member so that the sidewalls of the watercraft move up and down in response to shocks independently of the walls of the cockpit. Each shock-absorbing member preferably includes an airbag and a dashpot but other shock-absorbing members are within the scope of the invention.
申请公布号 WO2010091254(A3) 申请公布日期 2010.12.02
申请号 WO2010US23321 申请日期 2010.02.05
申请人 WERNER, TODD, C. 发明人 WERNER, TODD, C.
分类号 B63B15/00;B63B17/00;B63B29/00;B63B35/73 主分类号 B63B15/00
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