一、飛機發動機的推重比是什么意思
推力重量比(英語:Thrust weight ratio)簡稱推重比(TWR),是飛機和航空發動機重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)要的(de)技術性能指標。飛機(ji)(ji)發(fa)動(dong)(dong)(dong)機(ji)(ji)推力(li)與(yu)(yu)發(fa)動(dong)(dong)(dong)機(ji)(ji)重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)量(liang)或飛機(ji)(ji)重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)量(liang)之比,它表示飛機(ji)(ji)發(fa)動(dong)(dong)(dong)機(ji)(ji)或飛機(ji)(ji)單位重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)量(liang)所產(chan)生(sheng)的(de)推力(li)。飛機(ji)(ji)發(fa)動(dong)(dong)(dong)機(ji)(ji)在海平面靜(jing)止條(tiao)件下于最大狀(zhuang)態(加(jia)力(li)發(fa)動(dong)(dong)(dong)機(ji)(ji)為全加(jia)力(li)狀(zhuang)態)所產(chan)生(sheng)的(de)推力(li)與(yu)(yu)發(fa)動(dong)(dong)(dong)機(ji)(ji)結構重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)量(liang)之比稱(cheng)為飛機(ji)(ji)發(fa)動(dong)(dong)(dong)機(ji)(ji)推重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)比,與(yu)(yu)飛機(ji)(ji)重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)量(liang)之比稱(cheng)為飛機(ji)(ji)推重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)比。一(yi)般來說(shuo),戰斗(dou)機(ji)(ji)的(de)推重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)比較高,轟炸機(ji)(ji)等飛機(ji)(ji)的(de)推重(zhong)(zhong)(zhong)(zhong)(zhong)(zhong)比較低。
二、飛機發動機的推重比怎么計算
推重(zhong)(zhong)比(bi)(bi)(bi)(bi)有(you)兩種:飛機推重(zhong)(zhong)比(bi)(bi)(bi)(bi)和飛機發動(dong)(dong)機推重(zhong)(zhong)比(bi)(bi)(bi)(bi)。計(ji)算飛機推重(zhong)(zhong)比(bi)(bi)(bi)(bi)用發動(dong)(dong)機產(chan)生(sheng)的(de)(de)最(zui)大(da)值的(de)(de)推力除以飛機的(de)(de)最(zui)大(da)起飛重(zhong)(zhong)量,計(ji)算飛機發動(dong)(dong)機推重(zhong)(zhong)比(bi)(bi)(bi)(bi)用發動(dong)(dong)機產(chan)生(sheng)的(de)(de)最(zui)大(da)值的(de)(de)推力除以發動(dong)(dong)機重(zhong)(zhong)量。
由于(yu)噴氣發動機(ji)產生的(de)(de)推力會隨高度的(de)(de)改變而(er)改變,飛機(ji)在攜帶(dai)不(bu)(bu)同載荷時(shi)重(zhong)(zhong)量(liang)不(bu)(bu)同,因(yin)此(ci)推重(zhong)(zhong)比的(de)(de)值在使用(yong)不(bu)(bu)同的(de)(de)推力或重(zhong)(zhong)量(liang)下會產生不(bu)(bu)小的(de)(de)差異。譬如說,當(dang)使用(yong)飛機(ji)的(de)(de)最大起飛重(zhong)(zhong)量(liang)或者是只有50%燃料的(de)(de)重(zhong)(zhong)量(liang)分別計算推重(zhong)(zhong)比時(shi),計算出來的(de)(de)數字差別很(hen)大。
三、航空發動機推重比越大越好嗎
顯然不是。
對于民航客機而言,發動機的推重比過(guo)(guo)大會導致金屬疲勞加速(su),噪音過(guo)(guo)大,燃油消耗(hao)過(guo)(guo)高,整個(ge)機型的安全性(xing)和經濟性(xing)都降低。
對于(yu)軍用飛機而言,推(tui)重(zhong)比大(da)是一個很(hen)不(bu)錯的(de)(de)優(you)勢,但是飛行(xing)員的(de)(de)身(shen)體承受能力(li)是有(you)限的(de)(de),當推(tui)重(zhong)比過高(gao),推(tui)力(li)過剩,飛行(xing)員無法(fa)在自己身(shen)體允許的(de)(de)范(fan)圍內繼續實施(shi)加速,機動等等,這樣過高(gao)的(de)(de)推(tui)重(zhong)比也形同虛設。