SAE AS 18276B-2014 Lighting Aircraft Interior Installation of《飞机内部照明 安装》.pdf

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1、_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 particular use, including any patent infringement arising theref

2、rom, 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.Copyright 2014 SAE International All rights reserved. No part of this pub

3、lication 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: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970

4、(outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS18276BAEROSPACESTANDARDAS18276 REV. BIssued 1999-07 Revised 2014-01Superseding AS1

5、8276A Lighting, Aircraft Interior, Installation of FSC 6220 RATIONALEUpdated Applicable Documents; added consideration for non incandescent/halogen lighting; added alternate to NVIS goggle for observation of light leaks; removed some “redundant” information. 1. SCOPE 1.1 This specification covers th

6、e installation of aircraft interior lighting for military aircraft. 2. APPLICABLE DOCUMENTS The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effec

7、t on the date of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1 SA

8、E Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.AS18012 Markings for Aircrew Station Displays, Design and Configuration of AS25027 Light Assembly, Cockpit, Fixed A

9、S25050 Colors, Aeronautical Lights and Lighting Equipment, General Requirements for Copies of specifications, standards, drawings, and publications required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting

10、 officer. SAE INTERNATIONAL AS18276B Page 2 of 8 2.2 Specifications Military MIL-C-6781 Control Panel: Aircraft Equipment, Rack or Console Mounted MIL-M-8650 Mockups, Aircraft Construction of MIL-L-25467 Lighting, Integral, Red, Aircraft Instrument, General Specification for MIL-DTL-25866 Light, Eme

11、rgency Exit, Aircraft LEU-1/A MIL-DTL-7788 Panels, Information, Integrally Illuminated 2.3 Standards Military MIL-STD-203 Aircrew Station Controls and Displays; Location, Arrangement and Actuation of, for Fixed-Wing AircraftMIL-STD-411 Aircrew Station Alerting Signals MIL-STD-810 Environmental Engin

12、eering Considerations and Laboratory Tests MIL-STD-3009 Lighting, Aircraft, Night Vision Imaging System (NVIS) Compatible MIL-STD-7080 Selection and Installation of Aircraft Electrical Equipment AIR FORCE-NAVY AERONAUTICAL AN3037 Light Assembly, Cabin Dome Copies of the above specifications and stan

13、dards are available from DLA Document Services, Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6396, http:/quicksearch.dla.mil/.3. REQUIREMENTS 3.1 General Requirements 3.1.1 Installation Interior lighting equipment shall be installed in accordance with MIL-STD-7080. 3.1

14、.2 Mockup The lighting mockup shall conform to MIL-M-8650 and as noted in 3.5.4 herein. 3.1.3 Locations of Lighting Fixtures The locations of lighting fixtures shall be given careful consideration in order to provide satisfactory illumination, to preventundesirable reflections in windshields, canopi

15、es and other enclosures, and to prevent glare from a direct or reflected view of lamps, lenses and surfaces. Lighting installation shall conform to MIL-STD-203.3.1.4 Reflections Reflections of instruments and consoles in windshields and other enclosures shall be avoided. If necessary, a suitable non

16、rigid shield shall be provided around the instrument panel or console. SAE INTERNATIONAL AS18276B Page 3 of 8 3.1.5 Lighting Colors and NVIS Radiance 3.1.5.1 Instrument Panel Light (IPL) Red or White The light emitted by the illumination source (either lamp, lamp-filter or LED or LED-filter combinat

17、ion), to illuminate the panel, shall conform to AS25050 if red or white. 3.1.5.2 Instrument Panel Light (IPL) - NVG If NVG colors are required to illuminate the panel, the chromaticity limits and NVIS radiance requirements shall conform to MIL-STD-3009, not only on the panel but as reflected from an

18、y surrounding components. 3.1.6 Lighting Power All lights shall operate from a power source compatible with the aircraft power bus noted in 3.5.10.3.3. 3.1.7 Explosive Atmosphere Whenever a light is installed in an area normally containing an explosive vapor, the light shall be a vapor proof light c

19、onforming to the test requirements of MIL-STD-810, Method 511.5, Procedure II, explosion and flame arresting characteristics of equipment designed for that purpose. Lights installed in areas which may contain explosive vapors shall be equipped with covers to prevent inadvertent breakage of the lamp(

20、s). 3.1.8 Mechanical Damage Whenever a light is installed so as to be subject to damage from cargo, passenger, or crew normal movement, it shall be protected by a cover to prevent breakage of the lamp(s). 3.1.9 Control Configuration and Markings Control configuration and markings for information pan

21、els, control panels, and placards shall be chosen, arranged and marked in accordance with AS18012.3.2 Aircrew Station Signals Visual aircrew station signals, illuminated aircrew station signals shall conform to MIL-STD-203, MIL-STD-411, or MIL-STD-3009 as required. 3.3 Circuit Breaker Panels Circuit

22、 breaker panels shall be lighted when the aircraft is designed for in-flight maintenance. 3.4 Chart Board Lighting Chart boards not self-lighted shall be provided with lighting sufficient for reading maps and charts, and for navigation. 3.5 Cockpit Lighting 3.5.1 Instrument Lighting The instrument l

23、ighting shall conform to this specification, unless the contractor is authorized in writing by the procuring activity to install an alternate nonstandard instrument lighting system which does not conform to this specification. The request for authorization to install an alternate lighting system sha

24、ll be made before the lighting mockup inspection and shall include samples, photographs, drawings, or other data to indicate its superiority over the requirements of this specification for installation in the particular aircraft under consideration. The right is reserved to require the contractor to

25、 mock up both the alternate and the standard installations. SAE INTERNATIONAL AS18276B Page 4 of 8 3.5.2 Installation of Equipment All items of lighting equipment specified for installation shall conform to their respective drawings, specifications, or both,and shall be installed without modificatio

26、n, except for electrical leads. 3.5.3 Selection of Lights When specified by the procuring activity, as soon as possible after each instrument panel design or design change has been determined, the contractor shall furnish the procuring activity with one sample of each instrument panel, the instrumen

27、t panel drawings involved, or both, for use by the procuring activity for lighting studies before making recommendations relative to the types of lights to be used. The drawings shall show the layout of each instrument panel and the relative position of the crew members normal eye level with respect

28、 to the instrument panel under his observation.3.5.4 Mockup In order to determine the adequacy of the instrument lighting systems for each new model aircraft, or modification thereof, which would affect the design of the instrument panel layout or the lighting system, a complete mockup or a 3 D ligh

29、ting simulation (if agreed with procuring activity) of the instrument lighting system involved shall be prepared by the aircraft contractor for inspection and approval by the procuring activity. The mockup shall be provided with the actual lighting equipment and instruments or models of instruments

30、to be illuminated, insofar as practicable, which will afford a reasonable indication of the effectiveness of the lighting involved. Cardboard templates of instrument dials will not be satisfactory for this mockup. 3.5.5 Instrument Lighting Systems The instruments shall be provided with primary and s

31、econdary lighting systems. 3.5.5.1 Primary Lighting System The primary lighting system shall consist of integrally lighted instruments using MIL-L-25467 as a guide. The color of the instrument lighting shall be IPL - Red or IPL - White as dictated by operational requirements. When NVG lighting is sp

32、ecified then the requirements of MIL-STD-3009 shall apply. 3.5.5.2 Secondary Lighting System The secondary instrument lighting system shall be provided with lights in accordance with AS25027 or as agreed with the procuring activity. Sufficient lights shall be employed to provide adequate illuminatio

33、n subject to the mockup approval. Where practicable, these lights shall be installed under the glare shield of the instrument panel, as far away from the instrument panel as practicable. 3.5.6 Console Lighting System The consoles shall be provided with primary and secondary lighting systems. 3.5.6.1

34、 Primary Lighting System The primary console lighting system shall consist of integrally lighted information panels conforming to MIL-DTL-7788. The color of the panels shall be black when IPL - Red lighting is employed and may be either black or gray when IPL - White lighting is employed. 3.5.6.2 Se

35、condary Lighting Systems The secondary console lighting system shall provide visibility of switch handles, knobs, and controls. The fixtures employed shall be as approved by the procuring activity. Sufficient fixtures shall be employed to adequately light the switch handles, knobs, and controls. SAE

36、 INTERNATIONAL AS18276B Page 5 of 8 3.5.7 Emergency Lighting System An emergency lighting system shall be provided for use in the event of failure of the primary and secondary instrument lighting systems or the primary console lighting system. If the secondary console lighting fixtures can be remove

37、d from their bases for hand holding, these lights may be employed for the emergency lights. The emergency lights shall be readily changeable from red to white light while in use. At least one of the emergency lights shall be directable by hand or movable from its base to within 2 feet of all parts o

38、f the cockpit. 3.5.8 High Intensity Lighting System Aircraft which have a service ceiling higher than 40 000 feet or are designed to deliver nuclear weapons for air or surface burst, shall be provided with an additional system for illuminating the instrument panels and consoles with white light. The

39、 illumination provided shall be a minimum of 150 foot-candle for the primary flight instruments and a minimum of 75 foot-candle for other instruments and controls in the cockpit. Continuously variable manual control shall be provided. In addition, in aircraft equipped with an automatic thermal prote

40、ctive closure system, the light(s) shall be automatically turned on to full bright when the closure is closed. A momentary contact reset switch shall be provided to regain manual control.3.5.9 Thunderstorm/Utility Lighting System Except for fighter and interceptor aircraft, and aircraft which have h

41、igh intensity lighting systems in accordance with 3.5.8, one or more lights conforming to AN3037-8B, or other designs with similar performance, shall be installed in each cockpit for emergency maintenance and flight during lightning storms. The lights shall flood the instrument panel, controls, and

42、floor of the cockpit with at least 10 foot-candle. 3.5.10 Controls Standard control panels in accordance with MIL-C-6781 shall be provided for control of cockpit lights. 3.5.10.1 Locations Each crew station shall be provided with a lighting control panel, convenient for operation by that crewman, fo

43、r controlling all lights which are usually used by that crewman only. For lights which are usually used by two crewmen, one lighting control panel convenient for operation by both of those crewmen shall be provided. Where required for satisfactory control because of the great number of instruments,

44、consoles lit, or because some are overhead and some below eye level, etc., two lighting control panels shall be provided. Each lighting control panel which controls lighting of both flightand nonflight instruments of which the flight instruments constitute a total of more than four instruments, or m

45、ore than one quarter of the total number of instruments, or both, shall have separate controls for the primary lighting of the flight and nonflight instruments. All other lighting control panels which control lighting of both flight and nonflight instruments shallhave one control for the primary lig

46、hting of both the flight and the nonflight instruments. 3.5.10.2 Functions Each lighting control panel shall include, as applicable, one or two instrument primary lighting system controls marked “INST“, or “FLT INST“ and “NON-FLT INST“, as applicable, one console primary lighting system control mark

47、ed “CONSOLE“, and one instrument and console secondary lighting system control marked “FLOOD“. 3.5.10.3 Operation Each control shall operate as follows. SAE INTERNATIONAL AS18276B Page 6 of 8 3.5.10.3.1 Primary Lighting Controls Each primary lighting control shall be a rotary control, operated by a

48、standard control knob. When the knob is in its extreme counter-clockwise position, the lights shall be OFF. For incandescent/halogen lamp systems, rotating the knob clockwise from its “OFF“ position shall first turn the lights ON with between zero and one-seventh normal potential applied to the lamp

49、s, and then shall increase the potential applied to the lamps, either continuously or in at least seven steps, untilwhen the knob is in its extreme clockwise position, normal potential shall be applied to the lamps. For LED or other systems, the relationship between knob position and light output shall mimic those of an incandescent/halogen lamp system unless otherwise agreed with the procuring activity. 3.5.10.3.2 Secondary Lighting Cont