SAE ARP 4102 7 APPENDIX C-1993 Appendix C Electronic Display Symbology for Engine Displays《附件C用于发动机显示器的电子显示符号[代替 SAE ARP 1068B]》.pdf

《SAE ARP 4102 7 APPENDIX C-1993 Appendix C Electronic Display Symbology for Engine Displays《附件C用于发动机显示器的电子显示符号[代替 SAE ARP 1068B]》.pdf》由会员分享，可在线阅读，更多相关《SAE ARP 4102 7 APPENDIX C-1993 Appendix C Electronic Display Symbology for Engine Displays《附件C用于发动机显示器的电子显示符号[代替 SAE ARP 1068B]》.pdf（20页珍藏版）》请在麦多课文档分享上搜索。

1、AEROSPACERECOMMENDEDPRACTICEARP4102-7Issued 1993-09Reaffirmed 2007-07Appendix CElectronic Display Symbology for Engine DisplaysFOREWORDChanges in this reaffirm are format/editorial only.This document is an Appendix to ARP4102-7 - Electronic Displays issued July 1988.Appendix CRATIONALEThis document

2、has been reaffirmed to comply with the SAE 5-Year Review policy.SAE Technical Standards 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 p

3、articular 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2007 SAE In

4、ternational All rights reserved. No part of this publication may be reproduced, stored in 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: 877-60

5、6-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA)Fax: 724-776-0790 Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE ARP4102-7- 49 -APPENDIX CELECTRONIC DISPLAY SYMBOLOGY FOR ENGINE DISPLAYSC.1 SCOPE:This appendix recommends display symbology for Electronic Engine Displ

6、ays (ED) used on the flight deck of turbofan power transport aircraft.C.2 GENERAL:C.2.1 EDs should incorporate only that symbology appropriate for the installed engine.C.2.2 EDs should at all times be appropriate to the phase of flight, the type of operation (normal versus non-normal) and the automa

7、tic monitoring capability of the aircraft relative to engine parameters.The goal should be to limit displays at a given time to those required by the pilot to control the aircraft, to observe operating limits and to analyze the current status of the engines. For example, for aircraft with extensive

8、automatic monitoring and alerting capability, it may be desirable to provide the pilot with continuous display of the thrust parameter only; all other engine parameters would be available on an exception basis; i.e., automatically called up for a particular phase of flight or a malfunction/exceedanc

9、e or manually called up by the pilot.C.2.3 Displays may vary in size and shape. The total symbology content of a display should not result in clutter. Thus, small display formats should not be designed to contain all the symbology that can be satisfactorily included in larger displays.C.2.4 Symbols

10、should be grouped so that pertinent information is presented clearly and unambiguously; for example, actual, reference and redline value symbols should be presented so that they interact properly.C.2.5 Each engine should be readily identifiable and its parameters easily compared with those of other

11、engines.C.2.6 Displays shall be evaluated in a dynamic environment to ensure they perform their intended function throughout the entire operating envelope, that there is proper integration between individual symbols and displays and that displays do not contain human factor deficiencies.C.2.7 Recomm

12、endations for display element features should be observed whenever possible; however, symbols may be refined or tailored to specific installations as a result of dynamic testing.:C.3 ENGINE DISPLAY SYMBOLOGY:C.3.1 The matrix on the following page shows, for each engine parameter, the “elements“ that

13、 should be included in that parameters display. Note that the last two columns are “continuous“ and “conditional“. Except for the primary thrust parameter, which should be “continuous“, the recommendation for continuous or conditional depends on the automatic monitoring and pilot alerting capability

14、 of the aircraft systems.SAE ARP4102-7- 50 -C.3.2 The charts following the Display Requirements matrix show examples of typical existing configurations of each display element along with verbal recommendations for the “ideal“ configuration.Pages 51 to 67 show examples of typical existing symbology f

15、or each display element with remarks and recommendations pertaining to the “ideal“ symbology.PREPARED BY SAE COMMITTEE S-7,FLIGHT DECK AND HANDLING QUALITIES STANDARDS FOR TRANSPORT AIRCRAFTSAE ARP4102-7- 51 -SAE ARP4102-7- 52 -SAE ARP4102-7- 53 -SAE ARP4102-7- 54 -SAE ARP4102-7- 55 -SAE ARP4102-7- 56 -SAE ARP4102-7- 57 -SAE ARP4102-7- 58 -SAE ARP4102-7- 59 -SAE ARP4102-7- 60 -SAE ARP4102-7- 61 -SAE ARP4102-7- 62 -SAE ARP4102-7- 63 -SAE ARP4102-7- 64 -SAE ARP4102-7- 65 -SAE ARP4102-7- 66 -SAE ARP4102-7- 67 -