ASTM F945-22 PDF
Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials
Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 5
- Дата публикации:
- 1 сентября 2022 г.
- Издание:
- F945
- ICS:
- 49.025.30
SIGNIFICANCE AND USE 3.1 Because of the tendency of prestressed titanium alloy parts to crack if heated while in contact with certain chemical reagents, it is necessary to ensure that cleaning and maintenance materials will not initiate stress corrosion of titanium alloys under controlled conditions. For test specimens, two common titanium alloys are selected, one that is very susceptible (AMS 4916 or AMS 4919) and one that is not very susceptible (AMS 4911) to stress corrosion cracking. SCOPE 1.1 This test method establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress corrosion cracking of titanium alloy parts. 1.2 The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of prestressed titanium alloys to crack when subsequently heated to elevated temperatures. 1.3 Test conditions are based upon manufacturer's maximum recommended operating solution concentration. 1.4 Units—The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific precautionary statements, see 5.3 and 5.6. 1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM F945-22: Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials is a crucial international standard developed by ASTM International. This specification provides laboratories, aerospace manufacturers, and maintenance professionals with a defined test procedure to determine whether aircraft turbine engine cleaning and maintenance materials have the potential to cause stress-corrosion cracking (SCC) of titanium alloy parts. Stress corrosion cracking is a critical failure mode, especially for titanium alloys under stress and exposed to chemical agents at elevated temperatures. This standard is vital for aircraft engine safety, reliability, and long-term component performance.
Key Topics
- Stress-Corrosion Cracking (SCC) of Titanium Alloys: Focuses on the risk of cracking in prestressed titanium alloys when in contact with certain cleaning chemicals, particularly during heating cycles.
- Representative Alloys: Specifies the use of both highly susceptible (AMS 4916, AMS 4919) and less susceptible (AMS 4911) titanium alloys for testing to ensure a comprehensive assessment.
- Testing Procedures: Outlines detailed steps for specimen preparation, cleaning, exposure to candidate solutions, controlled heating, and evaluation through visual and metallographic inspection.
- Solution Concentrations: Emphasizes testing at the manufacturer’s maximum recommended operating concentrations of cleaning agents to simulate worst-case exposure.
- Acceptance Criteria: Defines clear guidelines for acceptance or rejection of cleaning compounds based on presence or absence of cracking in test specimens.
- Documentation and Reporting: Requires comprehensive documentation, including chemical identification, test outcomes, and any observed corrosion phenomena.
Applications
ASTM F945-22 is widely used in the aerospace industry to qualify and approve cleaning and maintenance products for use on titanium components in aircraft turbine engines. Its applications include:
- Qualification of Cleaning and Maintenance Chemicals: Ensures that compounds do not induce stress-corrosion cracking in titanium engine parts.
- Aerospace Component Safety: Supports the safety protocols of manufacturers and operators by preventing premature failures due to SCC.
- Material Selection and Quality Control: Assists material engineers and maintenance facilities in selecting compatible cleaning products for titanium parts.
- Regulatory Compliance: Fulfills requirements for chemical qualification as mandated by aerospace OEMs and the U.S. Department of Defense.
- Extended Equipment Life: Contributes to longer component service life and reduced maintenance costs by preventing stress-corrosion failures.
Related Standards
- ASTM D740: Specification for Methyl Ethyl Ketone, a reagent sometimes used in cleaning or testing.
- ASTM D841: Specification for Nitration Grade Toluene, used as a solvent in laboratory testing.
- ASTM D1193: Specification for Reagent Water, ensuring water purity in preparation and cleaning procedures.
- SAE AMS 4911 / AMS 4916 / AMS 4919: Aerospace Material Specifications for titanium alloys used in stress-corrosion susceptibility testing.
Practical Value
Adopting ASTM F945-22 delivers several practical advantages for aerospace operators and suppliers:
- Risk Mitigation: Minimizes the likelihood of catastrophic failures in flight by ensuring cleaning materials are SCC-safe for titanium alloys.
- Consistent Testing: Provides repeatable, standardized procedures for qualifying engine maintenance products and materials.
- Industry Confidence: Helps establish trust in the safety and durability of products used in critical aerospace systems.
- International Recognition: Aligns with global best practices in standardization, supporting compliance in diverse regulatory environments.
Use of ASTM F945-22 is a proactive measure for managing stress corrosion risk and sustaining the integrity of modern aerospace materials.
Технические детали
- Технический комитет
- F07 - Aerospace and Aircraft
- SKU
- ASTM F945-22
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