Kayan abin nadi na titin don abin nadi na titin XCMG

Takaitaccen Bayani:

Masoya XCMG na Sinanci, XCMG XS123 Fan na Sin, Masoyan XCMG na Sinawa XMR303
Masoya XCMG na Sinanci, XCMG XP303S Fan, Sinawa XCMG XS265H Fan
SHANTUI XS395 Fan na Sin, SHANTUI XS365 Fan na Sin, SHANTUI XS225JS Fan na Sin, SHANTUI XD143S na Sinanci


Cikakken Bayani

Tags samfurin

Masoyi

Domin akwai nau'ikan kayan gyara da yawa, ba za mu iya nuna su duka akan gidan yanar gizon ba. Da fatan za a ji daɗin tuntuɓar mu don takamaiman wasu.

Amfani

1. Muna samar muku da samfuran asali da na bayan gida
2. Daga masana'anta zuwa abokin ciniki kai tsaye, adana kuɗin ku
3. Stable stock ga al'ada sassa
4. A Lokacin Isar da Lokaci, tare da farashin jigilar kaya
5. Kwararren kuma akan lokaci bayan sabis

Shiryawa

Akwatunan kwali, ko bisa ga buƙatar abokan ciniki.

bayanin

Fan kuma aka sani da "injin turbofan". Yana nufin injin injin turbine wanda iskar gas ɗin da bututun ƙarfe ya hura da kuma iskar da fanka ke fitarwa ya haifar da motsin motsi. Ya ƙunshi na'ura mai ɗaukar hoto, ɗakin konewa, injin turbine mai ƙarfi (don fitar da kwampreso), injin turbine mai ƙarancin ƙarfi (don tuƙin fan) da kuma na'urar bushewa. Sassa uku na farko ana kiran su “injin core”. Ana amfani da makamashin da ake samu a cikin iskar gas ɗin da ke fita daga cikin injin ɗin don fitar da injin turbine mai ƙarancin ƙarfi don fitar da fanka, kuma ɗayan ɓangaren ana amfani da shi a cikin bututun ƙarfe don haɓaka iskar da aka fitar. Matsakaicin kewayawa yana da alaƙa da amfani da mai. Ƙarni na farko na injunan turbofan da suka bayyana a ƙarshen 1950s suna da ƙananan ƙarancin kewayawa, rabon haɓakawa na compressor da zafin jiki na gas kafin injin turbine.

Tsarin FAN shine ainihin cewa akwai injin turbojet 1-2 mara ƙarfi (ƙananan sauri) waɗanda aka ƙara a baya na injin turbojet. Wadannan injinan turbines suna fitar da wasu adadin magoya baya kuma suna cinye wani yanki na makamashin iskar iskar gas na injin turbojet (injin core). , Ta haka zai kara rage saurin fitar da iskar gas. Wani ɓangare na kwararar iska da fan ɗin ya tsotse ana aika shi zuwa ga kwampreso (wanda ake kira "internal duct" a cikin kalmomi), kamar injin jet na yau da kullun, ɗayan ɓangaren kuma yana fitar da shi kai tsaye daga gefen injin turbojet (" waje". duct"). Sabili da haka, ana rarraba makamashin iskar gas na injin turbofan zuwa magudanar iska guda biyu da aka samar da fan da ɗakin konewa bi da bi. A wannan lokacin, domin inganta thermal yadda ya dace da kuma ƙara yawan zafin jiki a gaban turbine, mafi man fetur makamashi gas za a iya canjawa wuri zuwa waje bututu iska iska ta hanyar low-matsa lamba turbine-kore fan ta dace turbine tsarin da kuma ƙara fan diamita. don haka guje wa karuwa mai yawa a cikin saurin shaye-shaye. Ta wannan hanyar, an daidaita ingancin zafin jiki da ƙarfin motsa jiki, kuma an inganta ingancin injin ɗin sosai. Mafi girman inganci yana nufin rage yawan man fetur da kuma tsayin kewayon jirgin. Duk da haka, babban fan diamita yana ƙara da iska yankin na engine, don haka turbofan injuna da kewayon rabo fiye da 0.3 ba su dace da supersonic cruise jirgin. Duk da cewa injin turbofan yana rage saurin shaye-shaye, amma ba ya rage yunƙurin, saboda rage saurin shaye-shaye yana ƙara kwarara (na waje). Daga hangen nesa na hanyar wucewa, injin turbofan shine sulhu tsakanin injin turbojet da injin turboprop.

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