EN 2018:1984
(Main)Bearings, airframe rolling, single row, self aligning roller bearings in steel, diameter series 3 and 4 - Dimensions and loads - Aerospace series
Bearings, airframe rolling, single row, self aligning roller bearings in steel, diameter series 3 and 4 - Dimensions and loads - Aerospace series
This standard specifies the characteristics, of rigid single row ball bearings of diameter series 3 and 4 1) designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms.
Luft- und Raumfahrt - Flugwerklager, einreihige Tonnenlager aus Stahl, Durchmesserreihen 3 und 4 - Maße und Belastungen
Roulements pour structures d'aéronefs, roulements en acier, à rotule sur une rangée de rouleaux, séries de diamètres 3 et 4 - Dimensions et charges - Série aérospatiale
Bearings, airframe rolling, single row, self aligning roller bearings in steel, diameter series 3 and 4 - Dimensions and loads - Aerospace series
General Information
Standards Content (sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Bearings, airframe rolling, single row, self aligning roller bearings in steel, diameter series 3 and 4 - Dimensions and loads - Aerospace seriesLuft- und Raumfahrt - Flugwerklager, einreihige Tonnenlager aus Stahl, Durchmesserreihen 3 und 4 - Maße und BelastungenRoulements pour structures d'aéronefs, roulements en acier, a rotule sur une rangée de rouleaux, séries de diametres 3 et 4 - Dimensions e
...This May Also Interest You
This European standard specifies the characteristics of inch based spherical plain bearing, metal to metal, in corrosion resisting steel, narrow series.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
They shall be used in the temperature range as determined by the grease capability as below:
- code A: grease as per MIL PRF 23827 Type I, operating temperature range −73 °C to 121 °C;
- code B: grease as per MIL PRF 81322, operating te...view more
- Standard17 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, narrow series for aerospace applications.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings ...view more
- Standard15 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of spherical plain bearing in corrosion resistant steel, with self-lubricating liner, wide series, elevated load under low oscillations applications.
They shall be used in the temperature range −55 °C to 163 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for×1 day
This European Standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions.
This standard applies whenever referenced.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircra...view more
- Standard42 pagesEnglish languagesale 10% offe-Library read for×1 day
This European Standard specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, wide series for aerospace applications.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings ar...view more
- Standard14 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265);
- a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a self aligning ball bearing with self lubricating liner (EN 4614);
- a rod end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a self-aligning spherical plain bearing with self-lubricating liner per EN 6096;
- a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of adjustable rod ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, extra wide series (EN 6097);
- a rod–end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies general characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, extra wide inner ring, inch series.
They are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the characteristics of inch based spherical plain bearings, metal to metal, in corrosion resisting steel, extra wide inner ring inch series.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
The slide hole treatment either at the outer ring or inner ring.
- Standard17 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self- lubricating liner, wide series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range -55° C to +163° C.
- Standard12 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self lubricating liner, narrow series, for elevated load. at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range −55 °C to +163 °C.
- Standard12 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies preferred test fluids for evaluating the resistance of non-metallic and related materials to the action of fluids.
The aim of this document is to rationalise the choice of fluids used for qualification and batch testing of materials.
In some cases, the test fluid and conditioning temperatures may closely simulate in-service conditions. However, no direct behaviour with service conditions shall be implied.
- Standard9 pagesEnglish languagesale 10% offe-Library read for×1 day
This European standard specifies the dimensions, mass, tolerances and static values of spring clamps for use in fuselage interior equipment and non-structural or secondary structural area. This standard part shall be used in conjunction with EN 4710-06 and EN 4710-07 as described in EN 4710-02.
The applicable temperature range is −55 °C to 85 °C.
- Standard8 pagesEnglish languagesale 10% offe-Library read for×1 day
This European Standard specifies the required characteristics, inspections, tests, quality assurance requirements, conditions for qualification acceptance and delivery of quick release fastening systems.
This European Standard applies to all fastening systems for use in fuselage interior equipment and non-structural or secondary structural area.
It may be applied when referred to in the product standard or in a design specification.
- Standard13 pagesEnglish languagesale 10% offe-Library read for×1 day
This European Standard presents the construction kit of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range −55 °C to 85 °C.
- Standard12 pagesEnglish languagesale 10% offe-Library read for×1 day
- Draft12 pagesEnglish languagesale 10% offe-Library read for×1 day
This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for rod assemblies with two adjustable ends with integrated bolts, designed to withstand static and dynamic loads possible for interior and substructure in the temperature range from − 55 °C to 85 °C. It is applicable whenever referenced.
For a complete overview see EN 4691-2.
- Standard55 pagesEnglish languagesale 10% offe-Library read for×1 day
- Draft55 pagesEnglish languagesale 10% offe-Library read for×1 day
This European Standard specifies the dimensions and tolerances of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range -55 °C to 85 °C. The rod ends should not be screwed completely apart.
- Standard23 pagesEnglish languagesale 10% offe-Library read for×1 day
- Draft22 pagesEnglish languagesale 10% offe-Library read for×1 day
This standard shows the locking clips for the construction kit of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range −55 °C to 85 °C (EN 4691-2).
- Standard13 pagesEnglish languagesale 10% offe-Library read for×1 day
- Draft13 pagesEnglish languagesale 10% offe-Library read for×1 day
Questions, Comments and Discussion
Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.