EN 4591:2005

Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1 550 MPa (at ambient temperature) / 315 °C

This standard specifies the characteristics of  self-locking, floating, self-aligning barrel nuts, in heat resisting nickel alloy, MoS2 lubricated.
Classification: 1 550 MPa / 315 °C

Luft- und Raumfahrt - Selbsteinstellende, freibewegliche, selbstsichernde Tonnenmuttern, aus hochwarmfester Nickelbasislegierung, MoS2-geschmiert - Klasse: 1 550 Mpa (bei Raumtemperatur) / 315 °C

Diese Norm legt die Merkmale von selbstsichernden, beweglichen, selbsteinstellenden Tonnenmuttern aus hochwarmfester Nickellegierung, MoS2-geschmiert, fest.
Klasse: 1 550 MPa )/315 °C )

Série aérospatiale - Écrous à portée cylindrique, à freinage interne, flottants, orientables, en alliage résistant à chaud à base de nickel, lubrifiés MoS2 - Classification : 1 550 MPa (à température ambiante) / 315 °C

Aeronavtika – Matice, sodčkaste, samonaravnalne, prosto gibljive, samovarovalne, zlitine, odporne proti toploti, na nikljevi osnovi, namazane z MoS2 – Klasifikacija: 1 550 MPa (pri temperaturi okolice) / 315 °C

General Information

• Status: Published
• Publication Date: 06-Dec-2005
• Withdrawal Date: 29-Jun-2006
• ICS: 49.030.30 - Nuts
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 07-Dec-2005
• Completion Date: 07-Dec-2005
• Ref Project: SIST EN 4591:2006 - Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1 550 MPa (at ambient temperature) / 315 °C

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1 550 MPa (at ambient temperature) / 315 °CSérie aérospatiale - Écrous a portée cylindrique, a freinage interne, flottants, orientables, en alliage résistant a chaud a base de nickel, lubrifiés MoS2 - Classification : 1 550 MPa (a température ambiante) / 315 °CLuft- und Raumfahrt - Selbsteinstellende, freibewegliche, selbstsichernde Tonnenmuttern, aus hochwarmfester Nickelbasislegierung, MoS2-geschmiert - Klasse: 1 550 Mpa (bei Raumtemperatur) / 315 °CTa slovenski standard je istoveten z:EN 4591:2005SIST EN 4591:2006en49.030.30ICS:SLOVENSKI
STANDARDSIST EN 4591:200601-september-2006







EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4591
December 2005 ICS 49.030.30 English Version
Aerospace series - Nuts, barrel, self-locking, floating, self-aligning, in heat resisting nickel base alloy, MoS2 lubricated - Classification: 1 550 MPa (at ambient temperature) / 315 °C
Série aérospatiale - Écrous à portée cylindrique, à freinage interne, flottants, orientables, en alliage résistant à chaud à base de nickel, lubrifiés MoS2 - Classification : 1 550 MPa (à température ambiante) / 315 °C
Luft- und Raumfahrt - Selbsteinstellende, freibewegliche, selbstsichernde Tonnenmuttern, aus hochwarmfester Nickelbasislegierung, MoS2-geschmiert - Klasse: 1 550 Mpa (bei Raumtemperatur) / 315 °C This European Standard was approved by CEN on 26 October 2005.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
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B-1050 Brussels © 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4591:2005: E



EN 4591:2005 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Required characteristics.5 4 Designation.7 5 Marking.7 6 Technical specification.7



EN 4591:2005 (E) 3 Foreword This European Standard (EN 4591:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by June 2006, and conflicting national standards shall be withdrawn at the latest by June 2006. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement
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