发明名称 PISTONS
摘要 1,254,697. Making pistons; casting composite pistons; welding by fusion. ASSOCIATED ENG. Ltd. 6 March, 1969 [15 March, 1968], No. 12834/68. Headings B3A, B3F and B3R. [Also in Division F2] A piston is reinforced in the region of the or each gudgeon pin bore 4 by a filamentary reinforcement consisting of a metal matrix in which filaments are embedded and bonded to the matrix. The filaments may be metal wires of, e.g., stainless steel, carbon steel, tungsten, molybdenum, nickel alloy or beryllium or fibres of, eg., asbestos, glass or silica. In the light alloy piston shown in Figs. 1 and 2, the gudgeon pin bosses 3 are supported from the crown 1 by webs 8 and the filamentary reinforcement consists of stainless steel wires 11 extending from the crown, through the webs and around the bore 4. The reinforcement is formed by winding the stainless steel wire on a mandrel 12, Fig. 3, and then spraying the wire, either by flame or plasma spraying, with molten aluminium so that the winding is covered and bonded together by the aluminium 13. The composite of wire and aluminium is then cut to the required axial length and hot pressed and parted off at 14 to provide the reinforcement, which is preferably cast in to the piston. Alternatively, the reinforcement may be inserted in suitable slots in the piston casting and then electron beam welded to the piston body. The reinforcement may be formed by surrounding the filaments with powdered material and sintering the powder or, alternatively, by hot pressing aluminium-coated wires to cause the aluminium to coalesce. In a modification, Fig. 6 (not shown), in which the webs (8) are substantially radial to the boss (3), each reinforcement comprises a circular section (21A) in the gudgeon pin boss and two linear sections (21B) in each web. The sections (21A) and (21B) may be united, e.g. by electron beam welding, before insertion in the piston. In another modification, Fig. 7, the reinforcement 23 extends through each web 8 from the crown 1 to opposite sides of the gudgeon pin bore 4. In a still further modification, Fig. 8 (not shown), the reinforcement (24) is similar to those shown in Fig. 1 except that it also extends through the piston crown.
申请公布号 GB1254697(A) 申请公布日期 1971.11.24
申请号 GB19680012834 申请日期 1968.03.15
申请人 ASSOCIATED ENGINEERING LIMITED 发明人 JOHN ANTHONY CATHERALL
分类号 F02F3/00;B23P15/10;F16J1/00;F16J1/14 主分类号 F02F3/00
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