SAE AS95234-13A-2025

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史蒂文 2026-04-02 10 150.33KB 3 页 20星币
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AEROSPACE STANDARD
CONNECTOR RECEPTACLE,
REVERSE BAYONET COUPLING,
BULKHEAD FEED-THRU
AS95234
™/13
Copyright © 2025 SAE International
All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, transmitted, in any form or by any means, electronic, mechanical, photocopying, recording,
or otherwise, or used for text and data mining, AI training, or similar technologies, without the prior written permission of SAE.
TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA)
Fax: 724-776-0790 Email: CustomerService@sae.org SAE WEB ADDRESS: http://www.sae.org
ISSUED 2014-02 REAFFIRMED 2019-03 STABILIZED 2025-09
THIRD ANGLE PROJECTION
CUSTODIAN: AE-8C1
REV.
A
FEDERAL SUPPLY CLASS
5935
™/13 REV.
A
PROCUREMENT SPECIFICATION: AS95234
SAE Executive Standards Committee Rules provide that: “ This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is
entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement
arising therefrom, is the sole responsibility of the user.”
SAE reviews each technical report at least every five
years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.
For more information on this standard, visit
https://www.sae.org/standards/content/AS95234/13A/
RATIONALE
AS95234/13A IS BEING STABILIZED BECAUSE THE PROCESSES/PRODUCT IS CONSIDERED MATURE AND THE
COMMITTEE DOES NOT ANTICIPATE FUTURE TECHNICAL CHANGES. STABILIZATION DOES NOT IMPLY THE
PROCESS OR PRODUCT IS UNACCEPTABLE FOR APPLICATIONS FOR WHICH IT IS DESIGNED. ANY TECHNICAL
CHANGES NOTED BY A SUPPLIER OR USER WHICH RESULTS IN A PRODUCT OR REQUIREMENT CHANGE WILL
BE ADDRESSED BY A NEW REVISION. A QUALIFIED SUPPLIER IS STILL MAINTAINED.
STABILIZED NOTICE
THIS DOCUMENT HAS BEEN DECLARED "STABILIZED" BY SAE AE-8C1 CONNECTORS COMMITTEE AND WILL NO
LONGER BE SUBJECTED TO PERIODIC REVIEWS FOR CURRENCY. USERS ARE RESPONSIBLE FOR VERIFYING
REFERENCES AND CONTINUED SUITABILITY OF TECHNICAL REQUIREMENTS. NEWER TECHNOLOGY MAY EXIST.
AEROSPACE STANDARD
AS95234™/13
SHEET 1 OF 2
REV.
A
CONNECTOR RECEPTACLE,
REVERSE BAYONET COUPLING,
BULKHEAD FEED-THRU
NOTICE
THE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS
DOCUMENT AND THE LATEST ISSUE OF AS95234.
FIGURE 1 - CONNECTOR RECEPTACLE, BULKHEAD FEED-THRU
AEROSPACE STANDARD
AS95234™/13
SHEET 2 OF 2
REV.
A
CONNECTOR RECEPTACLE,
REVERSE BAYONET COUPLING,
BULKHEAD FEED-THRU
TABLE 1 – FIGURE 1 DIMENSIONS
SHELL
SIZE
FRONT VIEW SIDE VIEW
R
±.004 (±0.1) S
±.012 (±0.3)
T1
+.004/-.000
(+0.1/-0.0)
A
+.000/-.006
(+0.00/-0.15)
K
±.008
(±0.2) L
MAXIMUM
M
+.016/-.000
(+0.4/-0.00
10SL .717 (18.2) 1.000 (25.4) .126 (3.2) .717 (18.2) .110 (2.8) .807 (20.5) .559 (14.2)
14S .906 (23.0) 1.181 (30.0) .126 (3.2) .969 (24.6) .126 (3.2) .791 (20.1) .559 (14.2)
16S .969 (24.6) 1.280 (32.5) .126 (3.2) 1.079 (27.4) .126 (3.2) .791 (20.1) .559 (14.2)
16 .969 (24.6) 1.280 (32.5) .126 (3.2) 1.079 (27.4) .126 (3.2) 1.150 (29.2) .748 (19.0)
18 1.063 (27.0) 1.378 (35.0) .126 (3.2) 1.213 (30.8) .157 (4.0) 1.118 (28.4) .748 (19.0)
20 1.157 (29.4) 1.496 (38.0) .126 (3.2) 1.346 (34.2) .157 (4.0) 1.118 (28.4) .748 (19.0)
22 1.252 (31.8) 1.614 (41.0) .126 (3.2) 1.472 (37.4) .157 (4.0) 1.118 (28.4) .768 (19.5)
24 1.374 (34.9) 1.752 (44.5) .146 (3.7) 1.610 (40.9) .157 (4.0) 1.055 (26.8) .811 (20.6)
28 1.563 (39.7) 2.000 (50.8) .146 (3.7) 1.839 (46.7) .157 (4.0) 1.055 (26.8) .811 (20.6)
32 1.752 (44.5) 2.244 (57.0) .169 (4.3) 2.102 (53.4) .157 (4.0) .992 (25.2) .874 (22.2)
36 1.937 (49.2) 2.500 (63.5) .169 (4.3) 2.346 (59.6) .157 (4.0) .992 (25.2) .874 (22.2)
REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS95234.
1. DESIGN:
CONNECTORS SHALL BE DESIGNED IN ACCORDANCE WTH FIGURE 1 AND TABLE 1. DIMENSIONS ARE IN INCHES. METRIC
EQUIVALENTS ARE GIVEN FOR INFORMATION ONLY AND ARE BASED ON 1 INCH = 25.4 MM. UNLESS OTHERWISE SPECIFIED,
TOLERANCES ARE ±.016 INCHES. THIS THROUGH BULKHEAD RECEPTACLE IS FRONT MOUNTING AND FEATURES AN O-RING
SEAL AND A SOLID PIN/SOCKET FEED-THRU CONTACT CONFIGURATION.
2. FOR INSERT ARRANGEMENTS, SEE AS95234, APPENDIX B.
3. PART NUMBER:
THE PART NUMBER SHALL BE AS SHOWN IN THE EXAMPLE BELOW:
SPECIFICATION NOTES:
1. A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE
TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R)
SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING
TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT
CONTAIN EDITORIAL CHANGES ONLY.
摘要：

SAE AS95234-13A-2025 是由国际自动机工程师学会（SAE International）发布的航空航天领域关键标准，主要规范了高性能圆形连接器及其附件的设计、材料、性能和测试要求。该标准特别针对光纤与电混合传输系统，适用于极端环境下的机载设备、卫星通信及武器系统。版本13A在2025年更新中进一步强化了连接器的抗振动、抗冲击、耐高温及密封性能，并引入了更严格的电磁兼容性（EMC）和可靠性验证流程，以保障航空电子系统在严苛条件下的信号完整性与长期稳定性。该标准是航空航天系统集成、技术认证及质量管控的重要依据。

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作者：史蒂文 分类：国外协会 价格：20星币 属性：3 页 大小：150.33KB 格式：PDF 时间：2026-04-02

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