US2013213528A1PendingUtilityA1

Magnesium-Alloy Member, Compressor for Use in Air Conditioner, and Method for Manufacturing Magnesium-Alloy Member

Assignee: HIRAWATARI SUEJIPriority: Oct 29, 2010Filed: Oct 28, 2011Published: Aug 22, 2013
Est. expiryOct 29, 2030(~4.3 yrs left)· nominal 20-yr term from priority
F05C 2201/028F04B 39/122C22F 1/00F04B 39/121B21C 23/002C22F 1/06F04B 39/0005C22C 23/02B21J 1/02B21C 23/00C22F 1/04C22C 23/00
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Claims

Abstract

A magnesium alloy member capable of achieving a mechanical strength and a high-temperature fatigue strength sufficient for a compressor for in automotive air conditioners The magnesium alloy member is formed by subjecting a cast material of a magnesium alloy containing, on the basis of mass %, from 0.3% to 10% calcium (Ca), from 0.2% to 15% aluminum (Al), and from 0.05% to 1.5% manganese (Mn), and containing calcium (Ca) and aluminum (Al) at a calcium/aluminum mass ratio of from 0.6 to 1.7, with the balance being magnesium (Mg) and inevitable impurities to plastic working (extrusion processing) at from 250° C. to 500° C. This makes it possible to obtain a magnesium alloy member having a room-temperature 0.2% proof stress of 300 MPa or more and a 150° C. fatigue strength of 100 MPa or greater.

Claims

exact text as granted — not AI-modified
1 . A magnesium alloy member obtained by subjecting a cast material of a magnesium alloy containing, on the basis of mass %, from 0.3% to 10% calcium, from 0.2% to 15% aluminum, and from 0.05% to 1.5% manganese, and containing calcium and aluminum at a calcium/aluminum mass ratio of from 0.6 to 1.7, with the balance being magnesium and inevitable impurities to plastic working at from 250° C. to 500° C. 
     
     
         2 . The magnesium alloy member according to  claim 1 , wherein the plastic working is followed by solution heat treatment and artificial aging treatment. 
     
     
         3 . The magnesium alloy member according to  claim 2 , wherein after the plastic working, the magnesium alloy member is subjected to solution heat treatment to retain the magnesium alloy member for at least 0.08 hour at a treatment temperature of from 450° C. to 510° C., and then, the resulting member is subjected to artificial aging treatment to retain the resulting member for at least 0.3 hour at a treatment temperature of from 150° C. to 250° C. 
     
     
         4 . A magnesium alloy member obtained by subjecting a cast material of a magnesium alloy containing, on the basis of mass %, from 0.3% to 10% calcium, from 0.2% to 15% aluminum, and from 0.05% to 1.5% manganese, and containing calcium and aluminum at a calcium/aluminum mass ratio of from 0.6 to 1.7, with the balance being magnesium and inevitable impurities to plastic working; and having a room-temperature 0.2% proof stress of 300 MPa or greater and a 150° C. fatigue strength of 100 MPa or greater. 
     
     
         5 . The magnesium alloy member according to  claim 1 , wherein the plastic working is extrusion processing. 
     
     
         6 . A compressor for air conditioners using, as a mechanical part thereof, the magnesium alloy member as claimed in  claim 1 . 
     
     
         7 . A method for manufacturing a magnesium alloy member, comprising subjecting a cast material of a magnesium alloy containing, on the basis of mass %, from 0.3% to 10% calcium, from 0.2% to 15% aluminum, and from 0.05% to 1.5% manganese, and containing calcium and aluminum at a calcium/aluminum mass ratio of from 0.6 to 1.7, with the balance being magnesium and inevitable impurities to plastic working at from 250° C. to 500° C. 
     
     
         8 . The method for manufacturing a magnesium alloy member according to  claim 7 , wherein the plastic working is followed by solution heat treatment and artificial aging treatment. 
     
     
         9 . The method for manufacturing a magnesium alloy member according to  claim 8 , further comprising, after the plastic working, subjecting the magnesium alloy member to solution heat treatment to retain the member for at least 0.08 hour at a treatment temperature of from 450° C. to 510° C., and then, subjecting the resulting member to artificial aging treatment to retain the resulting member for at least 0.3 hour at a treatment temperature of from 150° C. to 250° C. 
     
     
         10 . The method for manufacturing a magnesium alloy member according to  claim 7 , wherein the plastic working is extrusion processing.

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