Skip Nav Destination
Close Modal
Search Results for
Alloy 713LC
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Subjects
Journal
Article Type
Date
Availability
1-2 of 2 Search Results for
Alloy 713LC
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (10): Ni-118.
Published: 01 October 1966
... ALLOY 713LC is a nickel-base alloy possessing high stress-rupture strength up to 1700 F combined with excellent resistance to thermal fatigue. It is recommended for turbine wheels. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties...
Abstract
View article
PDF
ALLOY 713LC is a nickel-base alloy possessing high stress-rupture strength up to 1700 F combined with excellent resistance to thermal fatigue. It is recommended for turbine wheels. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Ni-118. Producer or source: Austenal Microcast Division, Howmet Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1983) 32 (7): Ni-288.
Published: 01 July 1983
... -7.27 Alloy 713LC As cast -2208 Alloy IN-738C Heat treated** -49.5 I *Process A. **205fPF (I IZI C) 1% hour + 155oOF (843°C) 24 hours Table 5 BURNER-RIG PROPERTIES AT 1700°F (927OC) (Tested In JP-5 fuel with 0.3pc sulfur and 5 nom seawater. Air-to-fuel ratio: 30 to I. Thermal cycle: 58 minutes at 1700°F...
Abstract
View article
PDF
INCONEL Alloy MA 6000 is a nickel-base alloy produced by mechanical alloying. It is strengthened by both oxide dispersion strengthening and precipitation hardening for high creep and rupture properties at 2000 F (1095 C) as well as at 1400 F (760 C). The alloy's composition also gives it excellent resistance to oxidation and sulfidation. Alloy MA 6000 was developed as a blade material for advanced gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-288. Producer or source: Huntington Alloy Products Division, An INCO Company.
