EN 2290-1:1998
(Main)Aerospace series - Rod bodies, flight control in aluminium alloy, for adjustable end fittings - Part 1: Dimensions and loads
Aerospace series - Rod bodies, flight control in aluminium alloy, for adjustable end fittings - Part 1: Dimensions and loads
This standard specifies the characteristics of flight control rod bodies for adjustable end fittings. They may be used within the temperature range of - 55°C to + 120°C.
Luft- und Raumfahrt - Rohrkörper für Flugsteuerungen aus Aluminium-Legierung für einstellbare Stangenköpfe - Teil 1: Maße und Belastungen
Diese Norm legt die Eigenschaften der Rohrkörper für Flugsteuerungen für einstellbare Stangenköpfe fest. Sie können im Temperaturbereich von - 55°C bis + 120°C eingesetzt werden.
Série aérospatiale - Corps de bielles de commandes de vol en alliage d'aluminium pour embouts réglables - Partie 1: Dimensions et charges
La présente norme spécifie les caractéristiques des corps de bielles de commandes de vol pour embouts réglables. Ils peuvent être utilisés dans l'intervalle de température de - 55°C à + 120°C.
Aerospace series - Rod bodies, flight control in aluminium alloy, for adjustable end fittings - Part 1: Dimensions and loads
General Information
Overview
EN 2290-1:1998 is a European standard developed by CEN that defines the specifications for aerospace rod bodies used in flight control systems. Specifically, it covers flight control rods made from aluminium alloys designed for adjustable end fittings. These components are critical in ensuring the precise and reliable operation of aircraft control surfaces.
This standard focuses on the dimensions and load requirements for these rod bodies, ensuring their performance under varying operational conditions. It applies to materials expected to perform consistently within a temperature range of -55°C to +120°C, accommodating the rigorous environments encountered in aerospace applications.
Key Topics
- Material specification: Rod bodies made from aluminium alloy tailored for aerospace flight control applications.
- Adjustable end fittings compatibility: Standardized interface dimensions to accommodate various adjustable fittings used in flight control assemblies.
- Dimensional requirements: Detailed measurements that ensure interchangeability, precision, and compliance with aerospace engineering standards.
- Load capacities: Defined mechanical load limits critical for maintaining safety and functionality during flight operations.
- Temperature performance: Ensures rod bodies maintain structural integrity and mechanical properties from extreme cold (-55°C) to high heat (+120°C).
Applications
EN 2290-1:1998 is essential for manufacturers, engineers, and quality assurance teams working within the aerospace industry who deal with:
- Design and production of flight control mechanisms such as ailerons, elevators, and rudders.
- Manufacturing of adjustable rod assemblies to allow fine-tuning and maintenance of aircraft control surfaces.
- Ensuring compliance with aerospace safety regulations by adhering to prescribed load and dimensional standards.
- Maintenance and overhaul operations where replacement rod bodies must match exact specifications for continued airworthiness.
- Research and development of new aluminium alloy materials optimized for lightweight yet durable aerospace components.
Related Standards
To fully implement EN 2290-1:1998 within aerospace projects, the following related standards and guidelines may be referenced:
- EN 2290-2: Covers additional technical requirements or testing methods related to rod bodies and end fittings.
- ISO 683-11: Specifications for heat-treatable aluminium alloys used in aerospace applications.
- EN 9100: Aerospace quality management systems standards applicable to manufacturing processes.
- FAA and EASA regulations: Provide regulatory frameworks governing flight control component certification.
- Other Aerospace Series Standards (AS): Further define components and materials used in flight control systems for interoperability and safety assurance.
Adhering to EN 2290-1:1998 ensures that aerospace aluminium alloy rod bodies meet stringent quality, safety, and dimensional criteria, enhancing the reliability and precision of flight control systems. This contributes to safer and more efficient aircraft design and operation.
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Rod bodies, flight control in aluminium alloy, for adjustable end fittings - Part 1: Dimensions and loadsLuft- und Raumfahrt - Rohrkörper für Flugsteuerungen aus Aluminium-Legierung für einstellbare Stangenköpfe - Teil 1: Maße und BelastungenSérie aérospatiale - Corps de bielles de commandes de vol en alliage d'aluminium pour embouts réglables - Partie 1: Dimensions et chargesAerospace series - Rod bodies, flight control in alumini
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Frequently Asked Questions
EN 2290-1:1998 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Rod bodies, flight control in aluminium alloy, for adjustable end fittings - Part 1: Dimensions and loads". This standard covers: This standard specifies the characteristics of flight control rod bodies for adjustable end fittings. They may be used within the temperature range of - 55°C to + 120°C.
This standard specifies the characteristics of flight control rod bodies for adjustable end fittings. They may be used within the temperature range of - 55°C to + 120°C.
EN 2290-1:1998 is classified under the following ICS (International Classification for Standards) categories: 49.035 - Components for aerospace construction. The ICS classification helps identify the subject area and facilitates finding related standards.
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