ISO 7481:2023
Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 °C — Test methods
Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 °C — Test methods
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 19
- Дата публикации:
- 2 ноября 2023 г.
- Издание:
- ISO IS 7481 edition 3 version 1
- ICS:
- 49.030.30
This document specifies test methods for metric self-locking nuts with MJ threads intended for use in aerospace construction at maximum operating temperatures less than or equal to 425 °C. It describes the test device and the method for each test. It applies to self-locking nuts as defined above, provided that the relevant documents (dimensional standard, drawing, procurement specification, etc.) refer to this document.
Abstract
Overview - ISO 7481:2023 in brief
ISO 7481:2023 specifies test methods for metric self‑locking nuts with MJ threads intended for aerospace use at a maximum operating temperature ≤ 425 °C. The standard describes the required test devices and step‑by‑step methods for each inspection, and applies when referenced by a dimensional standard, drawing or procurement specification. This third edition (2023) updates normative references and editorial content and supersedes ISO 7481:2000.
Key technical topics and requirements
ISO 7481:2023 defines a comprehensive test suite focused on the performance and safety of high‑temperature self‑locking nuts used in aircraft and spacecraft assemblies. Key topics include:
- Hardness test (Rockwell, Vickers, microhardness) - measurement zones, specimen preparation and ambient test conditions.
- Bearing surface squareness - test device (mandrel and sliding collar) and feeler‑gauge method for out‑of‑squareness evaluation.
- Axial load test - test arrangement, bearing plate, conical washer for countersunk nuts and bolt requirements.
- Wrenching feature test - verification of wrench engagement and dimensions in line with ISO kits.
- Stress embrittlement test - device and method to detect hydrogen/thermal‑induced embrittlement risks.
- Torque‑out and self‑locking torque tests - ambient and post‑heat‑soak procedures to measure locking performance before and after exposure to maximum operating temperature.
- Permanent set, push‑out, vibration and captive washer rotation tests - mechanical integrity checks under service‑representative loads and environments.
The standard references related ISO documents such as ISO 5855‑2 (MJ thread limits), ISO 6507‑1/6508‑1 (hardness tests), ISO 691 (wrench/sockets) and ISO 7403 (spline drives).
Practical applications and who uses ISO 7481:2023
ISO 7481:2023 is practical for organizations involved in the aerospace supply chain, including:
- Fastener manufacturers - to qualify and batch‑test self‑locking nuts for high‑temperature aerospace applications.
- Aircraft and spacecraft OEMs and integrators - to specify test methods in procurement documents and ensure component compatibility and traceability.
- Quality assurance and test laboratories - to perform standardized mechanical, thermal and vibration tests required for certification.
- Maintenance, repair and overhaul (MRO) providers - to assess used fasteners for re‑use or replacement after exposure to high temperatures.
- Design and materials engineers - to select appropriate locking hardware for assemblies operating up to 425 °C.
Related standards and keywords
Related standards: ISO 5855‑2, ISO 6507‑1, ISO 6508‑1, ISO 691, ISO 7403.
SEO keywords: ISO 7481:2023, aerospace self‑locking nuts, MJ threads, test methods, maximum operating temperature 425 °C, torque‑out test, axial load test, hardness test, vibration test, fastener qualification.
For procurement or compliance, include a direct reference to ISO 7481:2023 in drawings and specifications to ensure the prescribed test methods are applied.
Технические детали
- Технический комитет
- ISO/TC 20/SC 4 - Aerospace fastener systems
- SKU
- ISO 7481:2023
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