US2020198008A1PendingUtilityA1

Method for the powder-metallurgical production of components from titanium or titanium alloys

Assignee: Element 22 GmbHPriority: Apr 14, 2016Filed: Apr 4, 2017Published: Jun 25, 2020
Est. expiryApr 14, 2036(~9.7 yrs left)· nominal 20-yr term from priority
B22F 1/05Y02P10/25B22F 2999/00B22F 2003/248B22F 3/24B22F 3/12B22F 2998/10B22F 2301/205C22F 1/183C22F 1/02B22F 3/1007C22C 1/0458B22F 1/0011
41
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

A method for the powder-metallurgical production of a component from titanium or a titanium alloy is disclosed. In this method, following the customary procedure, first a green part is formed by using metal powder formed from titanium or the titanium alloy and is densified and compacted in a subsequent sintering step. Metal powder of titanium or the titanium alloy with an average grain size of <25 μm is used for producing the green part and the sintering step is carried out at a sintering temperature of up to a maximum of 1100° C. for a sintering at a sintering duration of ≤5 hours in an atmosphere that is under a reduced pressure in comparison with normal pressure. These measures achieve the effect that the grain structure of the material obtained, and consequently also the material properties, can be selectively influenced.

Claims

exact text as granted — not AI-modified
1 . A method for the powder-metallurgical production of a component from titanium or a titanium alloy, wherein first, using metal powder from titanium or the titanium alloy, a green part is formed and the green part is densified and compacted in a subsequent sintering step, wherein for producing the green part, metal powder from titanium or titanium alloy with a mean grain size of <25 μm, measured using laser diffraction according to ASTM B822-10, is used and the sintering step is performed at a sintering temperature up to a maximum of 1100° C. in an atmosphere under a reduced pressure in comparison with normal pressure. 
     
     
         2 . The method according to  claim 1 , wherein the maximum grain size of the metal powder from titanium or the titanium alloy is <30 μm. 
     
     
         3 . The method according to  claim 1 , wherein the sintering step is performed under a vacuum with a pressure of ≤10 −3  mbar. 
     
     
         4 . The method according to  claim 1 , wherein the sintering step is performed in an inert gas atmosphere at a pressure of ≤300 mbar. 
     
     
         5 . The method according to  claim 1 , wherein for producing the green part, metal powder from titanium or the titanium alloy with a mean grain size of <20 μm is used. 
     
     
         6 . The method according to  claim 1 , wherein the sintering duration is ≤3.5 h. 
     
     
         7 . The method according to  claim 1 , wherein the sintering duration is at least 1 h. 
     
     
         8 . The method according to  claim 1 , wherein the sintering temperature is up to a maximum of 1050° C. 
     
     
         9 . The method according to  claim 1 , wherein the sintering temperature amounts to at least 860° C. 
     
     
         10 . The method according to  claim 1 , wherein in the sintering step, the sintering temperature is adjusted in the range below a p-transition temperature of the titanium or titanium alloy material. 
     
     
         11 . The method according to  claim 1 , wherein the component after the sintering step has a material density of >97%. 
     
     
         12 . The method according to  claim 1 , wherein in the sintering step, a sintering temperature of below 950° C. is selected and that to achieve a material density in the component of >97%, after the sintering step the component is exposed to an additional step with pressure and optionally a temperature. 
     
     
         13 . The method according to  claim 1 , wherein the component, following the sintering step, is subjected to a thermal aftertreatment. 
     
     
         14 . The method according to  claim 13 , wherein the thermal aftertreatment is conducted in the form of one or more of the following treatment procedures: hot isostatic pressing (HIP), quench, and uniform rapid quench (URQ). 
     
     
         15 . A component produced according to  claim 1  from titanium or a titanium alloy having a globular α-structure with a grain size of <30 μm. 
     
     
         16 . A component produced according to  claim 1  from titanium or a titanium alloy having a grain structure with globular α-structure with mean grain size of <30 μm and lamellar (α+β) grain structure with a mean primary β-phase grain size of <90 μm. 
     
     
         17 . A component produced according to  claim 1  from titanium or a titanium alloy having a lamellar (α+β) grain structure with a mean primary β-phase grain size of <120 μm. 
     
     
         18 . The method according to  claim 3 , wherein the sintering step is performed under a vacuum with a pressure of ≤ 10   −5  mbar. 
     
     
         19 . The method according to  claim 4 , wherein the sintering step is performed in an argon atmosphere. 
     
     
         20 . The method according to  claim 5 , wherein metal powder from titanium or the titanium alloy with a mean grain size of <10 μm is used. 
     
     
         21 . The method according to  claim 20 , wherein metal powder from titanium or the titanium alloy with a mean grain size of <5 μm is used. 
     
     
         22 . The method according to  claim 6 , wherein the sintering duration is ≤3 h. 
     
     
         23 . The method according to  claim 22 , wherein the sintering duration is ≤2.5 h. 
     
     
         24 . The method according to  claim 7 , wherein the sintering duration is at least ≤2 h. 
     
     
         25 . The method according to  claim 8 , wherein the sintering temperature is up to a maximum of 1000° C. 
     
     
         26 . The method according to  claim 25 , wherein the sintering temperature is up to a maximum of 950° C. 
     
     
         27 . The method according to  claim 11 , wherein the component after the sintering step has a material density of >98%. 
     
     
         28 . The method according to  claim 28 , wherein the component after the sintering step has a material density of ≥99%. 
     
     
         29 . The method according to  claim 12 , wherein the additional step with pressure comprises one of cold isostatic pressing (CIP) and hot isostatic pressing (HIP). 
     
     
         30 . The method according to  claim 1 , wherein the sintering step is performed for a sintering duration of ≤5 h.

Join the waitlist — get patent alerts

Track US2020198008A1 — get alerts on status changes and closely related new filings.

We store only your email — no account needed. See our privacy policy.