版權(quán)說明:本文檔由用戶提供并上傳,收益歸屬內(nèi)容提供方,若內(nèi)容存在侵權(quán),請進(jìn)行舉報或認(rèn)領(lǐng)
文檔簡介
1、Thesummaryfthrustfcevecttechnology1.Outlihethrustfcevecttechnologyisreferstothemotpowerthethrustfcecomponentwhichproducesthroughthenozzleeitherthetailjetdeflectiontosubstitutetheiginalairplanethecontrolsurfacestrengthens
2、theairplanetheoperationfunctioncarriesontherealtimecontroltotheairplaneflightthetechnology.Toitsapplicationbutalsomustdependupontechnicalthesooncomputerelectronictechnologyautomaticcontroltechnologyenginemanufacturetechn
3、ologymaterialcraftintegrateddevelopment.Usingthethrustfcevecttechnologytothenewdesignonthemodificationnextcenturymilitaryairplaneindeedisaneffectivetechnicalbreachittothefighteraircraftstealthreducesantireducesweightextr
4、emelyisalleffective.ThethrustfcevecttechnologycanletthemotpowerapartturnthecontrolfcereplacespartiallyreplacesthecontrolsurfacethusgreatlyreducedtheradarreturnareaNomattertheangleofattackbigtheflyingspeedismuchlowtheairp
5、laneallmayusethispartofcontrolfcetocarryontheoperationthisincreasedtheairplanecontrolliability.Becausedirectlyhasthecontrolfcesizedirectioninstablealsoincreasedtheairplaneagilitythusmaysuitablyreduceremovetheverticalstab
6、ilizeralsocansubstituteothersomecontrolsurfaces.Thistoreducestheairplanetobepossiblethesurveytobeadvantageousalsocancausetheairplanetheresistancetoreducethestructurereducesagain.Therefetheusethrustfcevecttechnologysolves
7、thedesigncontradictybestchoice.HaspermittedfmanyyearscountrysoonAmericaRussiahasperfmedthemassiveperfmanceflighthadprovenusingthethrustfcevecttechnologyindeedcanachieveprearrangesgoal.AfterinApril1991theGulfWarendedthePe
8、ntagonputsout50billionUSdollarsthedevelopmentisdifferentwiththeF117newstealthairplanehasusedthethrustfcevecttechnologythereuponhadhasbasicallysatisfiedtheabovemanykindsofrequeststheF22fighteraircraft.TheRussiandevelopmen
9、tstealththethrustfcevecttechnologyappliedresearchincludestheMig1.44theaircurrentreactingfcewhichsendsouttothedifferentdirectionmayrapidlychangethedirectionusingtheengine.“JanesDefenseWeekly“in1992saidtheRussianhadalready
10、surmountedF117directlydevelopedthemodernsupersonicspeedattackairplanehasbecometheF22competit.2Technicalclassificationtoairplaneoverallperfmanceinfluenceeffuser(2DCDN)thepureinflationpitchnozzle(SERN)thedualwedgewritingst
11、ylenozzle(2DWN)skidsthethroattypenozzle(STVN)thesphericalsurfacerestrainsadjuststhenozzle(SCFN)soon.TheresearchconfirmedthatDualvectnozzlethrustvectiseasytoachieve.theendofthe80sAmericantwoadvancedresearchfighteraircraft
12、sYF22F119YF23F120haveusedthiskindofvectnozzle.Thedualvectnozzleshtcomingisthestructurequiteunwieldyflowsintheacteristictobewse.2.3AxialsymmetryvectnozzleThethrustfcevecttechnologyresearchconcentratesatfirstinthedualvectn
13、ozzlebutalongwithresearchthoughdiscoverytwodimensionalnozzlemeritalthoughmanybutshtcomingalsoveryobvioustransplantsinparticulartotheoperatingaircraftonisquitedifficult.Therefehasdevelopedtheaxialsymmetrythrustfcevectnozz
14、le.GECpationstartstheaxialsymmetrythrustfcevectnozzledevelopmentinthe1980sintermediatestagesitsdevelopmentnozzlechangestheadjustmentby3A94A8throatareaadjustment3adjustableringsconstitutionsoonsupptingganizationnozzlecont
15、rolvalveaswellasgroupofheatresistingsealspieces.2.4FlowfieldthrustfcevectnozzleTheflowfieldthrustfcevectnozzleiscompletelydifferenttothefrontseveralkindofmachineriesdoesmovesthetypethrustfcevectnozzleitsmainacteristiclie
16、sinthrough(SecondaryFluid)affectsthemainstreaminthenozzledivergentsectionintroductionlateralinferiaircurrenttheconditionachievesthechangethecontrolmainstreamareathedirectionthengainthrustfcevectgoal.Itsmostmainmeritwassa
17、vesthemachinerywhichthemassiveimplementationsthrustfcevectusedtotransptsimplifiedthestructurereducedtheairplaneweightreducedthemaintenancecost.Therealizationflowfieldthrustvectcontrolhasthemanykindsofwaysbelowatpresentst
18、udieshastheway:(1)jetthrustvectcontrol.Bytheaircurrentafterthenozzledivergentsectionmanyinjectionsthefcemainstreamattachesdependsonflowstoontheoppositesidewallsurfacethusproducestheside.?。?)regurgitationthrustvectcontrol
溫馨提示
- 1. 本站所有資源如無特殊說明,都需要本地電腦安裝OFFICE2007和PDF閱讀器。圖紙軟件為CAD,CAXA,PROE,UG,SolidWorks等.壓縮文件請下載最新的WinRAR軟件解壓。
- 2. 本站的文檔不包含任何第三方提供的附件圖紙等,如果需要附件,請聯(lián)系上傳者。文件的所有權(quán)益歸上傳用戶所有。
- 3. 本站RAR壓縮包中若帶圖紙,網(wǎng)頁內(nèi)容里面會有圖紙預(yù)覽,若沒有圖紙預(yù)覽就沒有圖紙。
- 4. 未經(jīng)權(quán)益所有人同意不得將文件中的內(nèi)容挪作商業(yè)或盈利用途。
- 5. 眾賞文庫僅提供信息存儲空間,僅對用戶上傳內(nèi)容的表現(xiàn)方式做保護(hù)處理,對用戶上傳分享的文檔內(nèi)容本身不做任何修改或編輯,并不能對任何下載內(nèi)容負(fù)責(zé)。
- 6. 下載文件中如有侵權(quán)或不適當(dāng)內(nèi)容,請與我們聯(lián)系,我們立即糾正。
- 7. 本站不保證下載資源的準(zhǔn)確性、安全性和完整性, 同時也不承擔(dān)用戶因使用這些下載資源對自己和他人造成任何形式的傷害或損失。
最新文檔
- 機(jī)電工程外文翻譯--推力矢量技術(shù)綜述
- 微推進(jìn)系統(tǒng)推力矢量控制及微推力測試技術(shù)的研究.pdf
- 射流推力矢量控制.pdf
- 矢量推力噴流數(shù)值模擬研究.pdf
- 雙力源推力矢量測試研究.pdf
- 小力值推力矢量測試研究.pdf
- 射流引射推力矢量數(shù)值計算研究.pdf
- 推力矢量飛行器容錯控制研究.pdf
- 帶推力矢量無人機(jī)的飛行控制.pdf
- ST-3型飛艇推力矢量的控制.pdf
- 逆流控制的推力矢量噴管氣動特性研究.pdf
- 推力矢量無人機(jī)的重構(gòu)控制策略.pdf
- summary
- summary
- 發(fā)動機(jī)噴管推力矢量控制研究.pdf
- 推力矢量飛機(jī)非線性控制律設(shè)計研究.pdf
- 三軸承推力矢量噴管結(jié)構(gòu)設(shè)計與研究.pdf
- force平臺基礎(chǔ)
- 書本+summary翻譯
- Summary.doc
評論
0/150
提交評論