SAE AIR 5354-2000 History of the SAE A-10 Aircraft Oxygen Equipment Committee《SAE A-10飞机氧气设备委员会的历史》.pdf
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1、AEROSPACEINFORMATIONREPORTAIR5354Issued 2000-12History of the SAE A-10 Aircraft Oxygen Equipment Committee1. SCOPE:The following is the history of SAE Committee A-10.2. HISTORY:The SAE Committee A-10, Aircraft Oxygen Equipment, started its existence in the early to mid-1950s as a subcommittee of the
2、 A-9 Aerospace Environmental Control Systems Group. It was during this period that Boeing, Douglas, and later Convair announced the development of their new jet-transports which were for the first time to regularly fly to the “horrendous“ altitude of 40,000 ft. de Havillands “Comet“ Transport was al
3、ready flying at these altitudes, but with disastrous explosive-decompression consequences.Because of concerns that cabin pressure decompression in these new transport aircraft could be a recurring hazard, a mid-1950s meeting of Industry and Government Regulatory Agencies resulted in the decision tha
4、t emergency standby oxygen equipment for passengers would be provided. The Federal Aviation Administration (FAA) then recognized the lack of commercial oxygen systems rules for crew and passenger hypoxia protection covering these altitudes. Therefore, they were going to have to promulgate new Civil
5、Aviation Regulations for these new aircraft. They asked for help from the Society of Automotive Engineers. An SAE A-9 Subcommittee, then known as “Aircraft Air Conditioning,“ responded to FAAs request. This group formed a central forum of industry experts. In an all-night session at Denvers Brown Pa
6、lace Hotel, an ad-hoc subcommittee of A-9 produced a “minimum physiological requirements“ proposal, which was subsequently adopted by FAA.Concurrent with this effort, A-9 labored over what was to later become AIR505, “Oxygen Equipment, Provisioning and Use in High Altitude (to 40,000 ft) Commercial
7、Transport Aircraft“, a system performance specification.Recognizing the need for a separate Oxygen Committee in early 1957, the SAE split-off the group from A-9 and designated it A-10. Later in 1957, they met as the newly-formed A-10 Committee to revise and finalize AIR505. It was completed and pres
8、ented to FAA, who wrote their jet-transport CAR (Civil Air Regulation) around it. Inexplicably, AIR505 did not finally “issue“ until 1961. The reason for this delay is lost. Issued or not, it was acknowledged to be “the only authoritative guide“ of the time.Reaffirmed 2011-06SAE Technical Standards
9、Board 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 responsi
10、bility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2011 SAE International All rights reserved. No part of this publication may be reproduced, stored i
11、n a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) Fax: 724-776-0790 Email:
12、CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AIR5354SAE AIR5354- 2 -2. (Continued):Some of the principals (and early A-10 members) who participated in the drafting of AI
13、R505 were: Art Miller (Scott Aviation), Vince Blockley (North American), D. R. Good (USAF), W. P. Hannan (American Airlines), Carl Jonasson (Boeing), R. Maddock (Douglas), Bob Stringer (Firewel), A. C. Princeau (United Airlines), and others. Guidance on physiological needs was provided by Dr. Charle
14、s Barron (Lockheed), and Dr. Thrift Hanks (Boeing).AIR505 established the physiological requirements and operating rules for passengers and crew members to 40,000 ft. Still needed were crew and passenger mask-equipment specifications.Concurrent with the AIR505 effort, Aeronautical Standard AS452 for
15、 the commercial transport flight deck crew masks (demand and pressure-demand) was developed and published.Until then, continuous flow systems for the passenger were generally limited to below 30,000 ft.Therefore, it was realized that a standard for an extremely lightweight “get-me-down“ passenger ma
16、sk from 40,000 ft was needed. Many of the A-10 experts who were responsible for AIR505 undertook the writing of an equipment specification for commercial continuous flow masks. NAS 1179, a National Aerospace Standard published by Aerospace Industries Association, was the result, and the efficient “p
17、hased-dilution“ mask system was introduced to provide short-term hypoxia protection to 40,000 ft.The jet-transport manufacturers later wrote their passenger mask specifications around NAS 1179.Later on, the SAE A-10 Standard AS8025 superseded NAS 1179 as the basis for FAA TSO C-64a (TSO meaning: Tec
18、hnical Standard Order).The completion of these basic documents provided the FAA and the oxygen equipment manufacturer with the oxygen specifications necessary for the commercial jet age.The highly respected Art Miller (a Scott Aviation Vice President) was made “permanent“ Chairman of the new A-10 Ai
19、rcraft Oxygen Equipment Committee. Under Arts leadership, the committee was off to a flying start. His interesting meetings were punctuated with real oxygen equipment demonstrations of especially slow opening oxygen shut-off valves the need for which he was totally committed. He even demonstrated th
20、e explosive results of mixing oxygen with oil. Under Art a period of prolific committee activity followed. Several of the early documents were:AIR822: Oxygen Systems for General AviationAIR825: Oxygen Systems for Aircraft (This document covered not only systems, but outlined physiological requiremen
21、ts which the oxygen systems are designed to meet. Through the years it has become the standard for the industry.)AS845: Smoke Protection for Crew MembersSAE AIR5354- 3 -2. (Continued):In 1962, after chairing the committee for five years, Art Miller handed the reins over to Dick Coulter (United Airli
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