Yayayana yiINJIN NASARAaikin damfara mai centrifugal?
Ana jan iska zuwa tsakiyar wani abu mai juyawa da ruwan wukake masu kama da radial kuma ana tura ta zuwa tsakiya ta hanyar ƙarfin centrifugal. Wannan motsi na iska mai kama da radial yana haifar da hauhawar matsin lamba da kuma samar da kuzarin motsi. Kafin a kai iska zuwa tsakiyar abin, makamashin motsi kuma ana canza shi zuwa matsin lamba ta hanyar wucewa ta cikin mai watsawa da volute.
Kowane mataki yana ɗaukar wani ɓangare na ƙaruwar matsin lamba na na'urar compressor. Dangane da matsin lamba da ake buƙata don aikace-aikacen, ana iya shirya matakai da dama a jere don cimma matsin lamba mafi girma. Irin wannan aikace-aikacen matakai da yawa galibi ana amfani da shi a masana'antar mai da iskar gas da sarrafawa. A madadin haka, a cikin masana'antun sarrafa ruwan shara, ana amfani da ƙarancin matsin lamba, aikace-aikacen matakai ɗaya don cimma rabon matsin lamba da ake so.
A cikin saitunan zamani naINJINAR NASARAAna amfani da injinan centrifugal air compressor, da injinan lantarki masu saurin gaske don tuƙa impellers. Wannan yana haifar da ƙaramin compressor ba tare da akwatin gearbox da tsarin shafa mai da ke da alaƙa ba, don haka ya sa ba shi da mai kuma ya dace da aikace-aikacen da ke buƙatar iska mai ƙarancin mai kashi 100.
| Ƙarfin Shigarwa na yau da kullun | 150 zuwa 6000 kW | 202.5 zuwa 8,100 hp |
| Matsi daga Fitowa | Bar 1 zuwa 25 | 14.5 zuwa 362.5 psig |
| Gudun Shiga | 40 zuwa 800 m3/min | 1,412 zuwa 28,240 CFM |
| Samfuri | Ƙarfi (KW) | Yawan Gudun Girma (M3/minti) | Ƙarshen injin tsabtace kPa(G) | Haɗi | Nauyi (KG) | Girma (L x W x H) mm |
| SEV5A-100 | 5.5 | 6.5 | -100 | DN40 | 430 | 1200X1100X1250 |
| SEV5A-080 | 6.3 | -80 | ||||
| SEV7A-100 | 7.5 | 9.6 | -100 | DN40 | 600 | 1200X1100X1250 |
| SEV7A-080 | 9.5 | -80 | ||||
| SEV11A-100 | 11 | 12.5 | -100 | DN50 | 760 | 1400X1100X1450 |
| SEV11A-080 | 12.0 | -80 | ||||
| SEV15A-100 | 15 | 15.0 | -100 | DN50 | 900 | 1500X1200X1650 |
| SEV15A-080 | 14.6 | -80 | ||||
| SEV18A-100 | 18.5 | 18.0 | -100 | DN65 | 960 | 1500X1200X1650 |
| SEV18A-080 | 17.6 | -80 | ||||
| SEV22A-100 | 22 | 22.5 | -100 | DN80 | 1100 | 1850X1450X1800 |
| SEV22A-080 | 22.0 | -80 | ||||
| SEV30A-100 | 30 | 27.5 | -100 | DN100 | 1600 | 2150x1600x2100 |
| SEV30A-080 | 27.0 | -80 | ||||
| SEV37A-100 | 37 | 30.5 | -100 | DN100 | 1850 | 2350x1700x2154 |
| SEV37A-080 | 30.0 | -80 | ||||
| SEV45A-100 | 45 | 45.0 | -100 | DN125 | 1900 | 2350x1700x2154 |
| SEV45A-080 | 44.5 | -80 | ||||
| SEV55A-100 | 55 | 60.0 | -100 | DN150 | 2200 | 3200x2150x2645 |
| SEV75A-100 | 75 | 76.0 | -100 | DN200 | 3500 | 3200x2150x2645 |
| SEV90A-100 | 90 | 85.0 | -100 | DN200 | 3600 | 3300x2250x2700 |
Na'urar hura iska da kuma matse iska ta centrifugal
SUCCESS ENGINE ta ƙware a fannin injinan tuƙi na farar hula, tana mai da hankali kan manyan buƙatu guda biyu na "rabo mai inganci na makamashi" da "aminci mai inganci", kuma ta tattara injiniya na farko a cikin gida kan wutar lantarki ta jiragen sama, injinan tuƙi da kuma bearing na dakatarwa. Ta amfani da kayan aiki na zamani, software da kayan aiki, ta hanyar ci gaba da haɓaka kai da ƙirƙira, tana jagorantar masana'antar injinan tuƙi na farar hula don inganta ƙwarewarta ta ƙirƙira.
Na'urar ƙwanƙwasa mai ƙarfin gaske (SuCCESS ENGINE) tana da babban kwarara, tare da ingantaccen aiki kuma babu fitar da mai. Kayan aikin injiniya ne mai saurin gudu wanda aka keɓance shi bisa ga buƙatun aikin mai amfani.
Matsewar centrifugal: Guduwar ruwa: 40~1500 m3/min, Matsi: 2~25bar
Ana amfani da na'urorin compressors na centrifugal na GDC jerin kayan aiki, da kuma na'urorin busa iska na centrifugal a masana'antu daban-daban waɗanda ke da buƙatar babban kwarara da ci gaba da aiki.


Tsarin ƙirar jiragen sama - Impeller
Ta amfani da manhajar nazarin abubuwa masu iyaka ta NASTRAN, ANSYS, Abaqus, da sauransu, don aiwatar da ƙirar geometric da thermal mai girma ɗaya, ƙirar kwarara mai girma biyu, ƙirar ruwan wukake mai girma uku da kuma duba ƙarfi na masu tuƙi da ruwan wukake. Ta hanyar kwaikwayon kwaikwayo, ana iya tantance ko ƙirar mai tuƙi ta cika ƙa'idodin ƙira na injin-aero, kuma ana iya hasashen tsawon lokacin sabis na mai tuƙi. Ƙirƙiri masu tuƙi masu inganci na matakin jirgin sama tare da mafi kyawun "rabo mai inganci na makamashin wutar lantarki".

Bearing mai sauri mai sauri
Ɗauki bearing na kwance mai siffar karkata wanda aka yi da kayan ƙarfe na ISI 1040 na carbon (na ciki) da kuma babbitt alloy (surface), lokacin da nauyin saurin ya canza, tonon bearing diagonal yana tsakiya ta atomatik, wannan aikin daidaitawa na atomatik zai iya tabbatar da aikin injin ɗin cikin santsi.

Akwatin gear mai saurin gudu na yau da kullun na jirgin sama
Ana amfani da tsarin gearbox na kwance tare da sarrafa daidaiton jirgin sama, kera, gyara kurakurai da dubawa, tare da ginannen ƙarfe mai saurin gudu wanda aka ƙera daidai gwargwado na helical, cibiyar kwance tana raba silinda zuwa rabi na sama da na ƙasa kuma tana haɗawa ta hanyar ƙusoshi, ƙirar tsarin modular ta dace don gyarawa da gyara.

Ingantaccen mai sanyaya mai cirewa da daidaita iskar shaƙa
An raba mai sanyaya da akwatin gear, kuma tsarin shafawa ya rabu da iskar da aka matsa, yana tabbatar da cewa iskar da aka matsa ta kasance mai tsabta 100% kuma ba ta da mai. An daidaita bututun mai mai cirewa daidai da harsashin da aka gama, wanda zai iya inganta saurin musayar zafi tsakanin iska mai matsewa da ruwa da kuma rage yawan shan ruwan sanyaya.
Ta hanyar daidaita kusurwar shigarwa na vane na jagorar shigarwa na impeller, ana iya daidaita juyawar iska kafin juyawa tsakanin kewayon 70-105%.

Gwajin daidaiton motsi na Impeller
Ta amfani da kayan aikin gwajin daidaito na zamani, bisa ga buƙatun "SuCCESS ENGINE Dynamic Balance Test Procedure", ana gudanar da gwajin daidaito na ƙarfi a kan kowane haɗin impeller da shaft don tabbatar da daidaito da kwanciyar hankali yayin aiki mai sauri.