Author: A. GIUNTOLI
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The effect of 25 F variation in solution heat treatment and 20 F variation in aging temperatures upon the mechanical properties of a 0.20 to 0.25% oxygen Ti 6Al-4V heat were determined. As a result of tests yield and ultimate strength variations between 164.2 to 176.1 ksi and 176.4 to 191.0 ksi, respectively, with no significant variation in ductility was found. Elevated temperature mechanical properties tests showed that the room temperature strength advantage found in the high oxygen Ti 6Al-4V diminished as temperatures rose to 750 F where the advantages began to disappear. Stress stability tests conducted at 750 for 1000 hours in the presence of 50 ksi stress indicated the high oxygen Ti 6Al-4V to be stable under these conditions. (Author).
Effect of Heat Treating Variables and Elevated Temperatures on the Mechanical Properties of High Oxygen 6a1-4v Titanium Alloy
Author: A. GIUNTOLI
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The effect of 25 F variation in solution heat treatment and 20 F variation in aging temperatures upon the mechanical properties of a 0.20 to 0.25% oxygen Ti 6Al-4V heat were determined. As a result of tests yield and ultimate strength variations between 164.2 to 176.1 ksi and 176.4 to 191.0 ksi, respectively, with no significant variation in ductility was found. Elevated temperature mechanical properties tests showed that the room temperature strength advantage found in the high oxygen Ti 6Al-4V diminished as temperatures rose to 750 F where the advantages began to disappear. Stress stability tests conducted at 750 for 1000 hours in the presence of 50 ksi stress indicated the high oxygen Ti 6Al-4V to be stable under these conditions. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The effect of 25 F variation in solution heat treatment and 20 F variation in aging temperatures upon the mechanical properties of a 0.20 to 0.25% oxygen Ti 6Al-4V heat were determined. As a result of tests yield and ultimate strength variations between 164.2 to 176.1 ksi and 176.4 to 191.0 ksi, respectively, with no significant variation in ductility was found. Elevated temperature mechanical properties tests showed that the room temperature strength advantage found in the high oxygen Ti 6Al-4V diminished as temperatures rose to 750 F where the advantages began to disappear. Stress stability tests conducted at 750 for 1000 hours in the presence of 50 ksi stress indicated the high oxygen Ti 6Al-4V to be stable under these conditions. (Author).
U.S. Government Research Reports
Effect of Oxygen Content on Strength on Materials - Titanium Alloy-ti 6a1-4v
Author: A. GIUNTOLI
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
After heat treatment consisting of solution treatment at 1700 F and aging at 1000 F for 3 hours, high oxygen material displayed consistently good mechanical properties up to 500 F, the highest temperature investigated. After heat treatment consisting of solution treatment at 1650 F and aging at 900 F for 6 hours the high oxygen material displayed consistently good mechanical properties up to 650 F, the highest temperature investigated. The oxygen contents of the nominal and high materials were 0.13 and 0.19%, respectively, and their hydrogen contents were 0.0250 and 0.0094%, respectively. The consistently higher ductility of the high oxygen content material was chiefly attributed to its low hydrogen content. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
After heat treatment consisting of solution treatment at 1700 F and aging at 1000 F for 3 hours, high oxygen material displayed consistently good mechanical properties up to 500 F, the highest temperature investigated. After heat treatment consisting of solution treatment at 1650 F and aging at 900 F for 6 hours the high oxygen material displayed consistently good mechanical properties up to 650 F, the highest temperature investigated. The oxygen contents of the nominal and high materials were 0.13 and 0.19%, respectively, and their hydrogen contents were 0.0250 and 0.0094%, respectively. The consistently higher ductility of the high oxygen content material was chiefly attributed to its low hydrogen content. (Author).
Keywords Index to U.S. Government Technical Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160
Book Description
Keywords Index to U.S. Government Technical Reports (permuted Title Index).
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 836
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 836
Book Description
Scientific and Technical Aerospace Reports
Titanium for the Chemical Engineer
OTS Selective Bibliography
Author: United States. Dept. of Commerce. Office of Technical Services
Publisher:
ISBN:
Category :
Languages : en
Pages : 450
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 450
Book Description
Fatigue Data Book
Author: ASM International
Publisher: ASM International
ISBN: 9781615031658
Category : Technology & Engineering
Languages : en
Pages : 412
Book Description
Publisher: ASM International
ISBN: 9781615031658
Category : Technology & Engineering
Languages : en
Pages : 412
Book Description