US2019381559A1PendingUtilityA1

PROCESS FOR PRODUCING A FORGED COMPONENT FROM A TiAl ALLOY AND COMPONENT PRODUCED THEREBY

Assignee: MTU Aero Engines AGPriority: Jun 19, 2018Filed: Jun 18, 2019Published: Dec 19, 2019
Est. expiryJun 19, 2038(~11.9 yrs left)· nominal 20-yr term from priority
C22C 14/00C22F 1/183B21J 9/022F01D 5/28F05D 2230/25B21K 3/04F05D 2230/40F01D 25/005F05D 2300/174B21J 1/06
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Claims

Abstract

A process for producing a component from a TiAl alloy by two-stage isothermal forging and to a component produced thereby. The process comprises a first isothermal forging of a component precursor at a temperature of at least about 1180° C., an intermediate annealing of the forged precursor at a temperature ranging from about 1130° C. to 1170° C. for about 1 to 8 hours and a subsequent second isothermal forging at a temperature of at least about 1180° C. with a degree of forming which is lower than the degree of forming in the first isothermal forging.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A process for producing a component from a TiAl alloy by two-stage isothermal forging, wherein the process comprises:
 (a) first isothermal forging of a component precursor at a temperature of at least 1180° C. and with a first total degree of forming;   (b) intermediate annealing of the forged precursor of (a) at a temperature ranging from 1130° C. to 1170° C. for 1 to 8 hours;   (c) second isothermal forging of the intermediately annealed precursor of (b) at a temperature of at least 1180° C. and with a second total degree of forming which is lower than the first total degree of forming.   
     
     
         2 . The process of  claim 1 , wherein the TiAl alloy is a TNM alloy. 
     
     
         3 . The process of  claim 1 , wherein the temperature in (a) is at least 1190° C. 
     
     
         4 . The process of  claim 1 , wherein the temperature in (a) is at least 1200° C. 
     
     
         5 . The process of  claim 1 , wherein the temperature in (c) is at least 1190° C. 
     
     
         6 . The process of  claim 4 , wherein the temperature in (c) is at least 1200° C. 
     
     
         7 . The process of  claim 1 , wherein the degree of forming in (a) is at least 0.55. 
     
     
         8 . The process of  claim 4 , wherein the degree of forming in (a) is at least 0.6. 
     
     
         9 . The process of  claim 1 , wherein the temperature in (b) ranges from 1135° C. to 1165° C. 
     
     
         10 . The process of  claim 4 , wherein the temperature in (b) ranges from 1140° C. to 1160° C. 
     
     
         11 . The process of  claim 1 , wherein (b) is conducted for at least 1.5 hours and/or for no longer than 7.5 hours. 
     
     
         12 . The process of  claim 1 , wherein after (c) at least one further heat treatment is conducted. 
     
     
         13 . The process of  claim 12 , wherein the further heat treatment is conducted at a temperature above a γ solvus temperature of the TiAl alloy. 
     
     
         14 . The process of  claim 12 , wherein the further heat treatment is conducted at a temperature below a γ solvus temperature of the TiAl alloy. 
     
     
         15 . The process of  claim 12 , wherein the further heat treatment is conducted at a temperature in the range from a γ solvus temperature to 30° C. above the γ solvus temperature of the TiAl alloy. 
     
     
         16 . The process of  claim 12 , wherein the further heat treatment is conducted at a temperature of from 10° C. to 50° C. below the γ solvus temperature of the TiAl alloy. 
     
     
         17 . The process of  claim 12 , wherein the further heat treatment is conducted for from 20 to 180 minutes. 
     
     
         18 . The process of  claim 12 , wherein the further heat treatment is followed by a cooling. 
     
     
         19 . The process of  claim 18 , wherein the cooling is followed by a further heat treatment. 
     
     
         20 . A component produced by the process of  claim 1 .

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