发明名称 Liquid or gas flow regulating valve e.g. for aircraft has flexible toroid element controlled by series of rollers with cam surfaces
摘要 The regulating valve (1) consists of a hollow housing (4) with two cylindrical ends (5A, 5B) for connecting to a pipe, and having a through passage (6) inside a toroid element controlled by a series of external rollers (8). The rollers are thirty-six in number and have identical cam surfaces (8B) that restrict or increase the passage through the toroid element; they are rotated by a motor through a gear and friction mechanism.
申请公布号 FR2835901(A1) 申请公布日期 2003.08.15
申请号 FR20020001812 申请日期 2002.02.14
申请人 FOATA ANTOINE 发明人 FOATA ANTOINE
分类号 F16K1/16;F16K3/03;(IPC1-7):F16K7/02;F16K31/48 主分类号 F16K1/16
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