ImageVerifierCode 换一换
格式:PDF , 页数:93 ,大小:2.10MB ,
资源ID:978026      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-978026.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(NAVY MIL-C-81774 A-1973 CONTROL PANEL AIRCRAFT GENERAL REQUIREMENTS FOR《航天飞机控制面板的总要求》.pdf)为本站会员(appealoxygen216)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

NAVY MIL-C-81774 A-1973 CONTROL PANEL AIRCRAFT GENERAL REQUIREMENTS FOR《航天飞机控制面板的总要求》.pdf

1、.-3 -9,;”“.+.?,-”IThis1. SCOPE1.1MILITARY SPECIFICATIONCONTROL PANEL, AIRCRAFT,GENERAL REQUIREMENTS FORMIL-C-81774A23 lfarrh 1973SUFESSEOIXllIL-c-81774s)1 July 1970spaclfication is approved for use by all Dapartmmtsand Agenciee of tha Department of Dafenee.purpose - This specification covers the gen

2、eral requirementsfor control panels for aircrew stations in military aircraft. The term “aircraft“i.mntrolpanel” as used herein includes the backing plate, the lighted panel,fasteners, markings, ffnish, nomenclature, controls, control guards, amldisplays.1.2 Application - l%is specification delineat

3、es documents forthe design of control panels; establishes display and control selectfon, utilizationand arrangement; end provfdes for verification data of these requirements2. APPLICABLE DOCUMENTS2.1 The following documents, of the fesue fn effect on date offnvttation for bide or request for proposa

4、l, form a part of thfe specificationto the extent specified herein.SPECIFICATIONSMilitaryMIL-S-3950 , Swftches, ToggleMIL-D-5480 Data, Engfneerfng and Technical,Reprocfuctfon Requfremente forMIL-S-5594 Swftch, Toggle, Electrically TrippableMIL-C-6781 Control Panel, Aircraft Equipment, Rack orConsole

5、 MountedMIL-E-7080 Electric Equipment, Aircraft, Selectionand Installation of-,II. Fsc 1680 - ._.-_Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SPECIFICATIONSMilitary (Continued)I MIL-G-7703MIL-P-7788I MIL-D-851O MIL-I-8700MIL-H-881OMIL-C-14806MIL

6、-M-18012MIL-S-22885MIL-S-24317MIL-K-25049MIL-C-25050MIL-S-3S039MIL- however,differences in design shall be limited to changes required by reach, manipula-tion and visibility. All markings, legends, and displays shall be visible andlegible to the operator under the range of ambient illumination condi

7、tions fnthe operational environment. The surtice (touch) temperature of all displays,pushbuttons, knobs, etc. that the crew members operate shall conform to therequirements of MIL-STD-454.3. 1.1 Approval - The design (as represented by the data package(3. 2) shall be reviewed and approved hy the hum

8、an factors and engineeringpersonnel of the procuring agency. Only the approved design shall be fabricatedfor aircraft use.3.2 R.,.:17Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-LifL-C-81774Athe knob to provide a gmeping su.face for tumfng. A pull

9、-to-turn knob shallbe knurled.3.8.10 Thumhwheel selectors. discrete - Thumbwheel controle-Y be wed when the function reqree a compact digital fnput device. Thedbnensione for these controle are epecifled to Table IL3.8.10.1 Number of positions - Discrete rotary thurnbwbeel selectorsshall have no mom

10、than 10 positions (O-9).3.8. 10; 2 Thuxnbwheel ehape - The digtta or legends on the drum partof the thnyibwheel shall be in ltne with the raised control tip of the thnmbwheelso that the control tip center line ie perpendicular to the panel sufice when anydigtt or legend is betng read. Thumbwheels sh

11、all not be capable of betngstopped between digits or legends.3.8.11 Continuous rotary control knobs - Conthmoue rotary knobsshall be eelected for control functions requiring manual adjustment over a rangeof values. Knobe shall be deeigned to the requirements of MIL-K-25049 and aespecified herein.3.8

12、.11.1 Shspe - For adjustments where more then one full turn is m)required, a round knob shell be need. For adjustment of less than one full turn,and where the radial position of the knob is not a source of information, othershapes may be used to increase discrimination. Controls having more than 360

13、degreee of rotation (Type A) shall be distinguishable from thoee having lese than360 degrees of rotation (Type B). See Figure 5.3. 8.11.2 Knob skirte - A knob ekirt with a potnter or a slotted sktrtOISyhe used to indicate the rridial position of the knob. The pointer or slot shallbe visible from the

14、 design eye position defined in MIL-STD-1333 for any pointerpmition. All knobs or knob skirte with imlices ehall be illuminated in accord- 1ante with the requtremente of MIL- P-7788.3.8. 11.3 Concentric knobe - Concentrically stacked knobs may beused for related fnnctione. The rotation of one knob s

15、hall not affect tbe settfngof the other.3. 8.11.4 Knobe incorporate ng a switch position - If the continuouscontrol incorporates a discrete function, the radtal position of the knob shall be16 -,+ :1 II -.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,

16、-,-.,. - “ .-. .”91,9ivllL-b-OK-linmarked and indexed with the panel Iabcd in the detent position. The force toovercome the detent position shall not exceed 12 inch-ounces but shall be atleast twice the continuous reeistzmce. The starting position or OFF pckitionshatl be at the extreme counter-clock

17、wise poeition.3.8.12 Continuous rotary thumbwheels - Thumbwheels may beselected for continuously varfable control functions to coneeme panel epace.3.8.12.1 = - ThumbwheeIs ehafl be round with sermted edges.38. 12.2 Dimension - Thumbwheel dtmeneione are given fn Table II.3.8.13 -s- .3.8. 13.1 Levere

18、for finger opemtion - Levers for finger opexationshall meet tbe following requi remente.3.8.13.1.1 Limb SUpport - When levere for finger movement are usedto make fine or continuous adjnstmenta, arm euppert efmll be provided.3.8.13.1.2 - If a epherical handle is provtded, the diameter shellbe greater

19、 then 0.5 inch end shall not =ceed 0.75 inch. K a cylindrical handleis used (cylinder encircled by thumb and fingers), the cylinder shall be 0.375 inchmtnimurn and O.50 fnch maxfmum.3.8.13.1.3 Resistance - Nnger opemtton resistance shall be 32 ouncesminimum and 60 ounces maximum.3.8.13.2 fiand contr

20、ollers - Levers deeigned for hand control shallbe accordance with IwfL-H-8810 and shall meet the folfowfng requirements.3.8.13.2.1 Limb eupport - When hand control levere are used to makefine adjuetmente involvfng emsll hand movements, arm support shall be pro-vided.3.8.13.2.2 - The hand-grip of a c

21、ontroller may be either round oroval in crose-section. The diameter or major axte shall he 0.75 incbmfnimumand 1.50 inches maximum. The length of the lever should be at least 3.75 inches.3.8. 13.2,3 Resistance - Minimum resistance for a hand-controlled leveris two pounds. Maximum allowable resistanc

22、e depende upen actuation sensitivitypjacenlent and direction of control movement. Fore-aft movement: 10 inchee19 -.,. . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-81774A.Ia71 1forward of Neutral Seat Reference Point (NSRP) -30 pounds; 16-2

23、4 inchesforward of NSRP -50 pounds. I.ateral movement: IO-19 inchee forward ofNSRP -20 p0UUd8.3.9 Dieplays - Selection and application of displays for thecontrol panel ehall be baeed on the dieplay requirements enalyaie and theperformance requirements of MIL-H-46855 and ehall be in accordance withth

24、e criterta of MIL-STD-1472. In the eelection and application of displaycomponents, consideration shall be given to the wie capabiltttee ad limits- -1.tions of the operator and to the operational environment in wbtch the dieplayewill be used.3.9.1 Information - Tbe limits, epecifici and, accuracy, fo

25、rm,redundant y, and combining of information ehall be as followe:(a)(M(c)(d)(e)The information dieplayed to an operator eball belimited to that information neceeeary for tie operatorto perform the epeciftc actions or make tbe requtreddecieions.The information shall be however, care shell also be t d

26、ownie the direction from head to foot. Right is the direction from the operatorsmidline toward his rtght band. L for controls installed in26 I1 :,.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I:,1“j.I “.I1MIC-81774A ,rotary-wing aircraft, MfI.=STD

27、-250 shall apply. For controls not treated in theabove, the fokwing shall apply.3.11.12.1 Diec release: OFF.Holding or reset function actuation shell be depress: ON; release: no change;depress: OFF; release; no change. Momentary pushbuttons shall be discrimtnablefrom holding pushbuttons.3.11.12.7.1

28、Positive indication - Positive indications of control actuation(momentary and continuous), shall he provided, e. g., snap feel, integral lighting,visible displacement or eimple indicator.3.11.12.7.2 Multlsfation pushbuttons - A multistation pushbutton in-corporates *O or more pushbuttons tn a single

29、 frame. Either lockfng or inter-leeldng features or both eball be incorporated in multistation pushbuttons toassure error-free operation. Locking or interlocking actuation shall be basedon functional requirements of the system. The type of lock or interlock &dshall be selected from those described i

30、n MIPS-24317. One pushbutton stationin a multistation switch shall always be in a down or active position with itsassociated circuitry activated. Depressing any other pushbutton station shall notcause deactuation of activated. circuitry until the pushbutton station befng depressedis positively commi

31、tted to activating ite associated circuitry.:3.11.12.7.3 Interacting pushbutton stations - H two panels contain thesame functions controlled by multistation pushbuttons, the pushbuttons on eachel shall fnteract to present the same indication of actuation. Panels withinteracting puehbuons shall indic

32、ate which crew station has control. Provisionto lock out one set of pushbuttons may be made upon approval of the procuringagency. ff lock-out of one panel is provided, the lock-out mafe eball be dleplayedon both panels.3.11.13 Arrang ement of markings -3.11.13.1 Orientation - Nomenclature shall be o

33、riented left to rightwith respect tn the operator except for the title which will be arrtmged top tobottom.3.11.13.2 LaCation - Nomenclature for controls shall be arranged asindicated in Figure 3. Nomenclature shall not be dbacured by controls whenviewed from the operating position. ,.a71)- “.,I128.

34、, ,Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-IIIMI C-8177U3.11.13.3 Control position nomenclature arrange ment - Nomenclature. .which indicate control position shall be placed to relate clearly the position to thecontrol. At leaet O.375 inoh sh

35、all separate control position labels from adjacentcontrol markings.3.12 - Coding shall be used to facilitate identification,enhance discrimination and mfnfmize error with respect to the location of panels,legibility of dieplays, and operation of controls within the full range of opera-tional and env

36、ironmental conditions. In a new aircraft design, ceding methodologyshall be established for the complete crew station end applied to individual panele.3.12.1 Special coding applications - Where advantages are to hegained in terms of human performance, the contractor shall recommend specialapplicatio

37、ns of ceding pficiples to tie procuring agency. Approval for specialcoding methods may be obtained in accofiance with the procedures establishedby 3.2.4.2 of this specification.4. QUALITY ASSUR4NCE PROVISIONS4.1 Responsibility for inspection - Unlese otherwise specified0)fn the contract or purchase

38、order, the supplier is responsible for the performanceof all inspection requirements as spectfied herein. Except as otherwise specifiedin the contract or order, tie eupplfer may use his own or any other facflittessuttable for the perfomna.nce of the inepedon requirement epeoified herein,unless dieap

39、proved by the Gwernment. The Govement reserves the right toperform any of the tnepections eet forth in the specification where such inspectionsare deemed necessary to assure supplies and cervices conform to prescribed re-quirements. When required, the supplier wtll provide the Government with testda

40、te.4.2 Inspection end teeting requirements - The. methods by whichepecitication compliance will be determined are listed for each requirement inthe specification. The metheds are: component testing, inspection, mock-upreview, demonstration, end data review. The contractor shall present evidencethat

41、the required compliance has been achieved in the design. The records ofthe tests, tnspectione, end reviews eball be available for inspection by the pro-curing agency. The teetlog and inspection performed under this specificationshall not duplicate but, as necessary, shsll be fn addition to the teats

42、 and in-spections performed against other contract requirements.29.+ . .- - _. . . . -Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-81774AThe Inspection and Teeting Requirements List is coded to indicate one of thecategories defied belowCT Co

43、mponent te8tiUg - All components used in the air-craft control panel shall be teeted in accorckuice withthe applicable military or contractor specification.Contractor specifications must be approved by theprocuring agency Pllo? to testing,I Inspection - Inspection includes the visual inspectionof th

44、e panel end measurements of dfmeneions. Theinspection shall also be performed on tbe film negatfveor film positive, which ebrdl be a true copy of thepanel.1“DDRM Mock-up revtew - T%review ie an hi33ctton Of a three-dimenefoml mmk-up of the panel defdgn and “dl controls,dteplays, swltdme, ewitch guar

45、ds, and markings onthe panel. The panel will be viewed with the designeye relationship as specified to determtne the legibilityand visibility of all markInge and legends, the control-dlsplay pcsitton relatbnehipe, and the adequacy of thepanel layout and arrangement.Demonstration - A demonetratlon sh

46、all establish that thepanel or component can perform the functions for whtchit was designed when installed on an aircraft andoperated by approved procedures. When requested, .alighting mock-up review skill be%onduct%d to demonstratethat the lighting provides suitable vielbilt and legibilityunder the levels of illmnlnatIon specified.Review of data - Thte category includes revtew endapproval by the procuring agency of the data eubmittedin reepcnse to the requtremente of 3.2.90Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1