NAVY MIL-C-6781 B-1960 CONTROL PANEL AIRCRAFT EQUIPMENT RACK OR CONSOLE MOUNTED《机架或控制台架设飞机设备控制面板》.pdf
《NAVY MIL-C-6781 B-1960 CONTROL PANEL AIRCRAFT EQUIPMENT RACK OR CONSOLE MOUNTED《机架或控制台架设飞机设备控制面板》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-C-6781 B-1960 CONTROL PANEL AIRCRAFT EQUIPMENT RACK OR CONSOLE MOUNTED《机架或控制台架设飞机设备控制面板》.pdf(11页珍藏版)》请在麦多课文档分享上搜索。
1、1.andandMIL-c-6781B(ASCJ13 September 1960SupersedingMIL-C-6781 A(ASG)3 Februcry 1958MILITARY SPECIFICATIONCONTROL PANEL: AIRCRAFT EQUIPMENT , RACK OR CONSOLE MOUNTEDThis specification has been approved by che Department of theAir Force and by the Navy Bureau of Naval Weapons.SCOPE1.1 - l%is apecific
2、acion covers general requirements for the designconstruction of two typea of concrol panels for uae with airborne equipment,ia intended pritirily for mounting on a rack or concrol console in thepilota cockpit.1.2 Claasiffcation Control panels shall be of the following types:2.forType 1 Standard dime
3、nsion control panelType II - Nonstandard control panelAPPLICABLE DOCUMENTS2.1 The following documents, of che issue in effeetbids, form a part of this specification to the excencSPECIFICATIONSMilitaryon date of invitationspecified herein:MIL-C-5015HIL-W-5088HIL-E-5272PIIL-E-5600tiIL-E-5556NIL-E-5557
4、HIL-P-7788UIL-P-8585!IIL-P-17555flIL-C-18012t41L-K-250f19MIL-F-25173flIL-C-26Lg2Conneccora, Electric, “AN” TypeWiring, Aircraft, Installation ofEnvironmental Testing, Aeronautical andAaabciated Equipment, General Specification forElectronic Equipment, Aircraft, GeneralSpecification forEnamel, Camouf
5、lage, Quick DryingEnamel; Heat-Resisting, Clyceryl-Phchalate, BlackPlate, Plastic, LightingPrimer Coating, Zinc Chromate, Lov-floisture-SenaicivityPreparation for Delivery of Electronic Equipment:t4iscellaneous Electrical Equipment (ExceptRotacing Electrical Equipment) and AssociatedRepair PartsCont
6、rol Configuration and Markings; (for PlasticLighting Platea, Control Panels and Placards)Knobs, Control, Equipment, AircrafcFastener, Control Panel.,Aircraft EquipmentConncccore, Electric, Circular, Miniature,Quick Disconnect1.”s(;ImlriI(Jr!)Provided by IHSNot for ResaleNo reproduction or networking
7、 permitted without license from IHS-,-,-xll.-,.-l,7xllil;,sl:)ISTAWARUSMilitaryHIL-STO-129 Narking for Shipment and StorageMIL-STO-130 Identification Harking for U.S. t4ilicaryPropertyMS2501O Light, Panel, Plastic plate LightingMS25176 Shnft, Control KnobMS25212 Control Panel, Coneole Type. Aircraft
8、 Equipment.Basic DimensionHS25213 Control Panel, Aircraft Equipment, TypicalInstallationsAir Force-Navy AeKOnautiCOlAN3502 Light Assembly-Control panel. PlasticLighting Plate(Copies of specificotions, acandards, drawings, and publfcaclons required byconcractora in connection with specific procuremen
9、t functions should be obtainedfrom the procuring activicy or aa direcced by the contracting officer.)3. REQUIRRIENTS3.1apply as3.2General specification - The requirements of Specification klIL-E-5400requirements of this specification, excepc aa otherwise apeclfied herein.D- 3.2.1 Type I control pane
10、l - Type I control panels shall be designed inaccordance with Standard )4S25212so chat inacallation can be made in accordancewith Standard MS25213. The complece control panel shall consist of a plasticlighting place, built-in red lighting, mounting place, the necessary ponents. and associated intern
11、al wiring, electrical receptacles, and s coverbox. The design shall be such chac several control panela can be mounted im-mediately adjacent to each other on a unilevel surface to preaenc a consoleappearance and percnfcstondardizacion of arrangement.3.2.2 Tvpe II control panel Type 11 concrol panels
12、 are designed to beinstalled in specific aircraft where apace”precludes installation of the type Icontrol panel or for use in equipment which cannot ecnplythe type I control panel.Type II control panels shall be similar to type I concrol panels, except for width.length, panel depth, eaae of removal,
13、 fastening provisiona, cover box, and adja-cent installation. Where practicable, capcive fasteners as specified hereinshall be used./2Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-C-6781E(ASC)3.2.3 Controls Each concrol panel shall incorporate
14、a careful arran6-ment of che individual controls. All controls not required during a flightmission shall be omitted from the front face of the control panel. Test pointsand controls required for general maintenance shall be separated from the in-flighc controls and made available on the control pane
15、l (but nOt On the frOncof che panel).3.3 Consccuction -3.3.1 Eaee of removal - Each control panel shall be so constructed asco be easily rindquickly removable from its mounting position.3.3.2 Interconnectingcabling Each control panel shall operate satis-factorily, ueing open wires for external inter
16、connecting wiring in accordancewith Specification MIL-W-5088. The use of shielded wire shall be held to theminimum necessary to comply with the applicable interference control require-ments.3.3.3 Lighting -3.3.6 Plastic place The plastic lighting place, plus the method offastening it to che a75ouncl
17、ng place, shall be in accordance with SpecificationMIL-P-7788. Where possible, all components shall be removable without removingthe plastic lighcicigplace.3.3.5 Light assemblv - The light assembly shall be in accordance withStandard HS2501O. Transparent red caps shall be used only with approval of
18、theprocuring activity. Where components behind the a75ounting plate precludeinstallation of the I4S2501Olight, the light assembly in accordance withStandard AN3502 may be employed.3.3.6 Panel lifthtin Panel 1ighting shall be integral with each panelin accordance with SpecifIcation MIL-P-7788. The po
19、wer to the illuminatinglampa shall be controlled by an external awicch with the brilliance controlon a separate lighting control panel. No lighting concrols shall be mountedon individual equipment control panels. The ON-OFF power -itch for the equip-ment controlled by the individual concrol panel sh
20、all not control the illumina-ting lamp circuit. One side of che light assemblies circuit shall be connectedto the power syacem through a single connection. The ocher side of the lightassemblies circuit shall be grounded co the mounting plate of the cOntrOl Paneland to a connection. The panel design
21、shall permit the use of either alternatingcurrent (AC) or direct current (DC) power for the lighting Circuit.3.3 Indicator lights - Indicacor lights shall not be included on thecontrol panel, except when specifically approved by the procuring accivity.The necessity for the use of any proposed indica
22、tor light and the color ofsuch lights shrillbe determined by che procuring activity after full con-sideration of ench parciculor case in which use of on indicacor light isproposed.:1Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-:.111.-.-(,7H:!i(,:i
23、!:)3.4 Performance Control panels SMI11 uperatc under CIW f,)uwinxcmdicions.3.4.1 Environmental conditions - TIM?ZIPPIicable cnvironmcncal require-ments of Specification tsIL-E-5600for the C1OSS stated in the detail specifi-cation shall apply as requirements of this specification. Additions orexcept
24、ions to che general specification may be required by the detailspecification.3.4.2 Explosive decompression - control panels shall withstand exPlOsivedecompression as follows:(a) From 30,000 feet to 50,000 feet pressure altitude ac a rateof change of 300 pounds per square inch (PSI) per second.(b) Fr
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- NAVYMILC6781B1960CONTROLPANELAIRCRAFTEQUIPMENTRACKORCONSOLEMOUNTED 机架 控制台 架设 飞机 设备 控制 面板 PDF

链接地址:http://www.mydoc123.com/p-977930.html