ISO 24071:2022

Aircraft — Auto-transformer rectifier units (ATRUs) — General requirements

This document specifies the general requirements and test methods for auto-transformer rectifier units (ATRUs) for use in aircraft electrical systems. This document is mainly applicable to ATRUs of 18-pulse and 24-pulse types.

Aéronefs — Autotransformateurs-redresseurs (ATRU) — Exigences générales

General Information

• Status: Published
• Publication Date: 01-Aug-2022
• ICS: 49.060 - Aerospace electric equipment and systems
• Technical Committee: ISO/TC 20/SC 1 - Aerospace electrical requirements
• Drafting Committee: ISO/TC 20/SC 1/WG 13 - Characteristics of aircraft electrical systems (Revision of ISO 1540)
• Current Stage: 6060 - International Standard published
• Start Date: 02-Aug-2022
• Due Date: 10-Apr-2022
• Completion Date: 02-Aug-2022

Standards Content (Sample)

INTERNATIONAL ISO
STANDARD 24071
First edition
2022-08
Aircraft — Auto-transformer
rectifier units (ATRUs) — General
requirements
Aéronefs — Autotransformateurs-redresseurs (ATRU) — Exigences
générales
Reference number
ISO 24071:2022(E)
© ISO 2022

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ISO 24071:2022(E)
COPYRIGHT PROTECTED DOCUMENT
© ISO 2022
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on
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Published in Switzerland
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ISO 24071:2022(E)
Contents Page
Foreword .v
Introduction . vi
1 S c op e . 1
2 N ormative references . 1
3 T erms and definitions . 1
4 G eneral requirements . 1
4.1 Specification sheets . . 1
4.2 M aterials . 1
4.2.1 S election of materials . 1
4.2.2 M etal materials . 1
4.2.3 N on-metal materials . 2
4.3 D esign and construction . 2
4.3.1 General mechanical and electrical design . 2
4.3.2 E lectrical design . 2
4.3.3 Mechanical design . 3
4.4 S ize and mass . 4
4 . 5 C olou r . 4
4.6 P rocessing quality and appearance quality . 4
4.6.1 Processing quality . . 4
4.6.2 A ppearance quality . 4
4.7 M arkings . 4
4.7.1 C omponents and parts . 4
4.7.2 N ameplate of ATRUs . 4
4.8 Performance . 5
4 . 8 .1 I nput p ower . 5
4 . 8 . 2 O ut put p ower . 5
4.8.3 Efficiency . 7
4.8.4 Overload . 7
4 . 8 . 5 S hor t c i r c u it . 7
4.8.6 Soft starting . 7
4.8.7 Insulation resistance and dielectric strength . 8
4.8.8 I nfluence on the input power system. 8
4.8.9 E lectrical protection . 8
4.9 A coustical noise . 8
4.10 R eliability . 8
4.11 M aintainability . 8
4.12 Interchangeability . 9
5 E nvironmental conditions and test procedures . 9
6 Qualification inspection .10
6.1 General . 10
6.2 M ethods of inspection . 10
6.2.1 P rocessing quality and appearance quality . 10
6 . 2 . 2 C olou r . 11
6.2.3 M arkings . 11
6.2.4 S ize and mass. 11
6.2.5 I nsulation resistance and dielectric strength . 11
6.2.6 N ormal steady-state input voltage . 11
6.2.7 A bnormal steady-state input voltage . 11
6.2.8 I nput voltage spikes .12
6.2.9 I nput power interruptions .12
6.2.10 I nput frequency transients .12
6.2.11 Output voltage ripple .12
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ISO 24071:2022(E)
6.2.12 Output voltage frequency characteristics .12
6.2.13 Output voltage distortion factor .12
6.2.14 Output voltage transients.12
6.2.15 Output power interruptions. 13
6.2.16 Efficiency . 13
6.2.17 Overload .13
6 . 2 .18 S hor t c i r c u it . 13
6.2.19 Soft starting . 13
6.2.20 Influence on the input power system. 13
6.2.21 E lectrical protection . 13
6.2.22 A coustical noise . . 13
6.2.23 Reliability . 13
6.2.24 Maintainability . 14
6.2.25 Interchangeability . 14
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ISO 24071:2022(E)
Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards
bodies (ISO member bodies). The work of preparing International Standards is normally carried out
through ISO technical committees. Each member body interested in a subject for which a technical
committee has been established has the right to be represented on that committee. International
organizations, governmental and non-governmental, in liaison with ISO, also take part in the work.
ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of
electrotechnical standardization.
The procedures used to develop this document and those intended for its further maintenance are
described in the ISO/IEC Directives, Part 1. In particular, the different approval criteria needed for the
different types of ISO documents should be noted. This document was drafted in accordance with the
editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/directives).
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of
any patent rights identified during the development of the document will be in the Introduction and/or
on the ISO list of patent declarations received (see www.iso.org/patents).
Any trade name used in this document is information given for the convenience of users and does not
constitute an endorsement.
For an explanation of the voluntary nature of standards, the meaning of ISO specific terms and
expressions related to conformity assessment, as well as information about ISO’s adherence to
the World Trade Organization (WTO) principles in the Technical Barriers to Trade (TBT), see
www.iso.org/iso/foreword.html.
This document was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles,
Subcommittee SC 1, Aerospace electrical requirements.
Any feedback or questions on this document should be directed to the user’s national standards body. A
complete listing of these bodies can be found at www.iso.org/members.html.
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ISO 24071:2022(E)
Introduction
This document provides general requirements for auto-transformer rectifier units (ATRUs) installed in
aircrafts.
ATRUs can convert electrical power from alternating current (AC) to direct current (DC) by using
multipulse phase shifting auto-transformers to provide cancellation of certain harmonic currents.
ATRUs have been shown to be the most cost-effective harmonic solution in aviation industry with
minimum mass, simpler structure and higher reliability, compared with conventional harmonic
suppression devices. ATRUs are emerging among aircraft application, especially in more electrical
aircraft and all electrical aircraft power supply system.
There are no International Standards on ATRUs, and standardization is needed for aircraft electrical
systems. This document provides the basis for manufacturers and users that develop and utilize ATRUs
installed in aircrafts.
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INTERNATIONAL STANDARD ISO 24071:2022(E)
Aircraft — Auto-transformer rectifier units (ATRUs) —
General requirements
1 S cope
This document specifies the general requirements and test methods for auto-transformer rectifier
units (ATRUs) for use in aircraft electrical systems.
This document is mainly applicable to ATRUs of 18-pulse and 24-pulse types.
2 Normat ive references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
ISO 1540:2006, Aerospace — Characteristics of aircraft electrical systems
ISO 7137:1995, Aircraft — Environmental conditions and test procedures for airborne equipment
3 T erms and definitions
For the purposes of this document, the terms and definitions given in ISO 1540 and ISO 7137 apply.
ISO and IEC maintain terminology databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at https:// www .iso .org/ obp
— IEC Electropedia: available at https:// www .electropedia .org/
4 Gener al requirements
4.1 Specification sheet s
The individual item requirements shall be as specified in an applicable specification sheet. In the event
of any conflict between the requirements of this document and the specification sheet, the latter shall
govern.
4.2 Mat erials
4.2.1 Selection of materials
The materials used shall enable the ATRU to meet all of the operational and environmental performance
requirements of this document and the applicable specification sheet.
The materials used shall pass the requested certification in accordance with the applicable specification
sheet.
4.2.2 Metal materials
All metals used in ATRUs construction shall be processed and protected to resist corrosion. The use of
magnesium is prohibited unless specifically approved for each application by the qualifying activity.
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ISO 24071:2022(E)
Dissimilar metals should not be used in intimate contact with each other. If really necessary to be
used in contact with each other, dissimilar metals shall be protected against electrolytic corrosion in
accordance with the applicable specification sheet.
4.2.3 Non-metal materials
Non-metal materials, including plastics, ceramics, fabrics, and protective finishes, shall:
— be moisture-resistant;
— be fungus-proofing;
— be resistant for salt spray environment;
— be flame-resistant;
— not support combustion;
— be non-toxic when exposed to flame as well as when used under all operating and environmental
conditions herein.
4.3 Design and c onstruction
4.3.1 General mechanical and electrical design
The ATRU shall be constructed with parts and materials to provide the specified performance,
reliability and service life under all environmental and operating conditions specified herein. Dielectrics
used for electrical isolation shall be adequate to prevent breakdown under all specified environmental
conditions for the life of the equipment.
4.3.2 Electrical design
4.3.2.1 Derating design
Derating shall be implemented for the ATRU design by reducing the level of stress for components used
in the ATRU, including electrical, thermal and mechanical stresses on components.
4.3.2.2 Electric connections
Electric connections of the ATRU, including terminals, connectors and wires, shall be designed to give
protection against short-circuit, reverse polarity, incorrect installation, electrical contact with people
or other unrelated conductors, and to conform with the following requirements.
a) Electrical wiring shall be neat and stable, meeting the requirements of the applicable specification
sheet.
b) Where terminals are used for connection to the ATRU, they shall be of the stud-type and shall be so
designed that the current is conducted by means of surface-to-surface contact, and not through the
stud threads. All studs shall be steel and corrosion-resistant.
c) The mark and preventative measures of incorrect wiring shall be provided in electrical connection
of the ATRU.
d) Grounding shall be designed to metallic shell surfaces of the ATRU according to the requirements of
the applicable specification sheet.
e) The equipment structure shall not be used as a current path except for electromagnetic (radio
noise) shielding.
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ISO 24071:2022(E)
f) The terminal block shall be so designed that it can be removed and replaced on the ATRU without
the necessity of rebrazing or soldering. Barriers affording a positive separation of leads and
terminals shall be provided on the terminal block. Durable, reusable and non-conductive terminal
covers shall be provided. Terminal designations shall be durably, legibly and prominently marked
on the terminal block.
4.3.2.3 Adjustments
No adjustments or alignments shall be required during installation or during the life of the ATRU.
4.3.2.4 Static dischar ge protection and control
The ATRU shall be designed to provide static discharge protection for electronic devices during
assembly and handling. Static discharge protection and control shall conform to the applicable
specification sheet.
4.3.3 Mechanical design
4.3.3.1 S crew thread standard
Screw threads of mechanical connections and fasteners in the ATRU shall conform to the requirements
of the applicable specification sheet.
4.3.3.2 Loosening pr evention
Effective anti-loosening measures should be taken for fasteners, such as stud bolts and nuts, used in the
ATRU.
4.3.3.3 V entilation openings
All ventilation openings shall be designed to prevent passage of foreign objects. Their structural form
and size shall conform to the requirements of the applicable specification sheet.
4.3.3.4 Oper ating position
The ATRU shall operate in any position, unless otherwise specified in the applicable specification sheet.
4.3.3.5 Assembl y and disassembly
The ATRU shall be assembled and disassembled with bolts and nuts, unless otherwise specified in the
applicable specification sheet.
4.3.3.6 C ooling
4.3.3.6.1 Natur al cooling
The ATRU is cooled by modular heat sink. When the radiator is exposed, the insulation failure and
excessive temperature rise of the exposed radiator should be effectively prevented.
4.3.3.6.2 Int ernally mounted fan cooling
An internally mounted, integral cooling fan may be used for ATRUs. Explosion-proof fan should be
selected for cooling fan.
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ISO 24071:2022(E)
4.3.3.6.3 F orced-air or forced-fluid cooling
Pressure drop through forced-air or forced-fluid cooled ATRUs shall not exceed the values specified in
the applicable specification sheet.
For forced-air or forced-fluid cooled ATRUs, the direction of air and fluid flow shall be as required by
the applicable specification sheet and depicted by an arrow that is visible on the ATRU exterior.
4.3.3.7 Installation
The aircraft manufacturer should allow a clearance of at least 25 mm at each end of the ATRU in
addition to the maximum dimensions shown on the applicable specification sheet for installation and
ventilation.
4.4 Size and mass
The dimensions and mass shall include the dimensions and mass of all auxiliary apparatus of the ATRU
and shall meet the requirements of the applicable specification sheet.
4.5 C olour
The ATRU shall be finished as identified in the applicable specification sheet. Colouring has no influence
on performance of the ATRU.
4.6 Pr ocessing quality and appearance quality
4.6.1 Processing quality
The machined parts shall be free of burrs and sharp edges. The metal castings shall be free from blisters,
looseness, cracks and other defects. The welds shall be clean and free of void-welding. The riveting shall
be firm. The fasteners shall not be loose. There shall not be floating solder, metal fragments or other
unwanted materials inside the ATRU.
Each ATRU and its parts and components shall be inspected as required by the applicable specification
sheet.
4.6.2 Appearance quality
The appearance of ATRUs shall be free from defects such as cracks, crushing, scratches, deformation,
rust and paint peeling.
4.7 Mar kings
4.7.1 Components and parts
Unless otherwise specified, the ATRU parts and components shall be marked in accordance with the
applicable specification sheet.
4.7.2 Nameplate of ATRUs
The marking and nameplate of each ATRU shall be as required by the applicable specification sheet and
drawings.
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ISO 24071:2022(E)
4.8 Performance
4.8.1 Input power
4.8.1.1 St eady-state input power
The ATRU shall meet the requirements specified herein or the applicable specification sheet when it
applies to an aircraft electrical system and supplied with normal or abnormal steady-state AC power as
defined in ISO 1540.
4.8.1.2 T ransient input power
4.8.1.2.1 Input v oltage spikes
When AC input power (constant frequency or variable frequency) voltage spikes of the ATRU are within
the limitations specified in ISO 1540:2006, Figure 9, the ATRU shall not be damaged and shall meet the
requirements specified in 4.8.2.1.1.
4.8.1.2.2 Input po wer interruptions
When the duration of normal input power interruptions is within 200 ms, or the duration of abnormal
input power interrupt is within 7 s (constant frequency or variable frequency), the ATRU shall not
be damaged and shall not be required to demonstrate specific performance. After removal of the
interruptions and restoration of input voltage specified in 4.8.1.1, the ATRU output voltage shall be
automatically restored and shall meet the requirements specified in 4.8.2.1.
4.8.1.2.3 Input fr equency transients
When AC input power frequency transients (constant frequency), frequency step changes and rate of
change of frequency (variable frequency) are within the limits specified in ISO 1540, the ATRU shall
operate normally, without damage.
4.8.2 Output power
4.8.2.1 St eady-state output voltage
4.8.2.1.1 Normal st eady-state output voltage
Unless otherwise specified in the applicable specification sheet, with the normal input power specified
in 4.8.1.1 and the ATRU operating within full rated load, the output voltage characteristics of the ATRU
shall have the following performance.
a) The nominal steady-state DC output voltage of the two output terminals of ATRUs with respect to
the neutral of the system shall be +135 V DC and −135 V DC, respectively.
b) The output voltage shall remain between ±125 V DC and ±160 V DC.
c) The output voltage differential mode ripple amplitude of the ATRU shall not exceed 16 V (peak-to-
peak).
d) Individual frequency components of the output voltage ripple of the ATRU shall not exceed the
limits of Figure 1.
e) Output voltage distortion factor of the ATRU shall not exceed 3 % (measured with full load under
resistive load).
The voltage values for ±270 V DC system are the voltage ratio 270/135 times the values in a), b) and c).
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ISO 24071:2022(E)
AC ripple frequency limits
Frequency Voltage ripple
(kHz) (V rms)
0,01 0,2
1,0 2,0
10,0 2,0
150,0 0,16
Key
f frequency (kHz)
V voltage ripple (V rms) of each frequency component
Multiply voltage ripple values in this figure by the voltage ratio 270/135 for a ±270 V DC system.
Figure 1 — Frequency characteristics of ripple in DC output power
4.8.2.1.2 A bnormal steady-state output voltage
Unless otherwise specified by the applicable specification sheet, with the limits of input AC three-phase
abnormal voltage specified in 4.8.1.1 and the ATRU operating within full rated load, the output voltage
characteristics of the ATRU shall have the following performance.
a) The steady-state output voltage shall remain between ±120 V DC and ±178 V DC.
b) The output voltage differential mode ripple amplitude of the ATRU shall not exceed 25 V (peak-to-
peak).
After restoration of normal input voltage specified in 4.8.1.1, normal output voltage shall be
automatically restored and meet the requirements of 4.8.2.1.1.
The voltage values for ±270 V DC system are the voltage ratio 270/135 times the values in a) and b).
4.8.2.2 Output voltage transients
When subjected to transient input voltages, or during the starting period at full rated load, or if the full
rated load is applied and removed, the ATRU output shall remain within the limits of Figure 2.
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