发明名称 Rotary piston engine with radially oscillating blade seals - has cylindrical recesses, curved blades and force resultants through blade pivots
摘要 <p>The rotary piston engine with radially oscillating blade seals has a rotor with cylindrical section blade recesses (3) in the periphery. Blades (5) are curved, carried on a one-piece web (6) from a pivot (7) at the end of a bracket (4) projecting transversely into the recess. Blades swing parallel to rotor axis; unit CG (8) lies between pivot and blade. Blade shape is such that resultant of all steady forces, which are normal to the surface, passes through the pivot axis. A strip (9) of low friction wear material along recess edge seals rotor-blade gap. Blade, or portion (10) in contact with stator, is made of material with low coefficient of friction against stator material.</p>
申请公布号 FR2414119(A1) 申请公布日期 1979.08.03
申请号 FR19780000103 申请日期 1978.01.04
申请人 TAT AERO EQUIPMENT IND LTD 发明人 SHLOMO OSTERSETZER ET EUGENIUS BROCHSTEIN;BROCHSTEIN EUGENIUS
分类号 F01C1/44;(IPC1-7):01C19/02;04C15/00;04C29/00 主分类号 F01C1/44
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