A study of hydrogen embrittlement of various alloys Annual summary report, 24 Jun. 1966 - 23 Jun. 1967
Hydrogen embrittlement of stainless steel, nickel maraging steel and Ti-6Al-4V alloy
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Hydrogen embrittlement of stainless steel, nickel maraging steel and Ti-6Al-4V alloy
Prior cold reduction effect on precipitation and embrittlement of cobalt base alloy /L-605/
Neutron irradiation effects on embrittlement of polycrystalline tungsten
Hot salt stress corrosion of titanium alloys - generation of hydrogen and its embrittling effect
Hydrogen embrittlement and stress cracking studied on 14 selected high strength alloys
Hydrogen embrittlement mechanism in steel based on modified pressure theory, discussing crack propagation mechanisms and stress corrosion cracking
Hot salt stress corrosion of Ti alloy, discussing hydrogen generation during elevated temperature exposure and embrittlement as manifestation of strain rate
Iron base and nickel base alloys susceptibilities to internal hydrogen and hydrogen environment embrittlements, studying crack initiation inside and at metal surface
Hardened steel embrittlement in low pressure hydrogen caused by crack growth as function of temperature
Quenched and tempered steel, investigating embrittlement as function of temperature in partially dissociated atomic hydrogen environment
Reversible hydrogen embrittlement mechanism in hydrogenated steels
Metal embrittlement by gaseous hydrogen, discussing countermeasures against hydrogen metal interaction and cracking
An investigation was performed to determine to what extent typical flight connector solder joints may be embrittled by the presence of gold. In addition to mapping of gold content in connector solder joints by an electron microprobe analyzer, metallographic examinations and mechanical tests (thermal shock, vibration, impact and tensile strength) were also conducted. A description of the specimens and tests, a discussion of the data, and some conclusions are presented.
A disc pressure test has been used to study the influenced of a hydrogen gas environment on the mechanical properties of three high strength superalloys, Inconel 718, L-605 and A-286, in static and dynamic conditions. The influence of the hydrogen pressure, loading rate, temperature, mechanical and thermal fatigue has investigated. The permeation characteristics of Inconel 718 have been determined in collaboration with the French AEC. The results complemented by a fractographic study are consistent either with a stress-sorption or with an internal embrittlement type of mechanism.
The results are presented of an investigation into the availability and performance capability of measurement components in the area of cryogenic temperature, pressure, flow and liquid detection components and high temperature strain gages. In addition, technical subjects allied to the components were researched and discussed. These selected areas of investigation were: (1) high pressure flange seals, (2) hydrogen embrittlement of pressure transducer diaphragms, (3) The effects of close-coupled versus remote transducer installation on pressure measurement, (4) temperature transducer configuration effects on measurements, and (5) techniques in temperature compensation of strain gage pressure transducers. The purpose of the program was to investigate the latest design and application techniques in measurement component technology and to document this information along with recommendations for upgrading measurement component designs for future S-2 derivative applications. Recommendations are provided for upgrading existing state-of-the-art in component design, where required, to satisfy performance requirements of S-2 derivative vehicles.
Technical abstracts for about 90 significant documents relating to hydrogen embrittlement of structural metals and alloys are reviewed. Particular note was taken of documents regarding hydrogen effects in rocket propulsion, aircraft propulsion and hydrogen energy systems, including storage and transfer systems.
This bibliography is comprised of approximately 1,600 reference citations related to four problem areas in the mechanics of failure in aerospace structures. The bibliography represents a search of the literature published in the period 1962-1976, the effort being largely limited to documents published in the United States. Listings are subdivided into the four problem areas: Hydrogen Embrittlement; Protective Coatings; Composite Materials; and Nondestructive Evaluation. An author index is included.
Technology survey reviews information covering three types of hydrogen embrittlement on structural metals and three specific hydrogen effects. Literature from 1962 to 1975 is summarized.