engine inlet 中文意思是什麼

engine inlet 解釋
發動機通氣口
  • engine : n. 1. 機械，機器。2. 引擎，蒸汽機，發動機。3. 機車，車頭。4. 工具；〈古語〉方法，手段。vt. 給…安裝發動機。
  • inlet : n. 1. 進口，入口。2. 【電學】引入，輸入，輸入線。3. 水灣，小港。4. 插入物，鑲嵌物。vt. （inlet, inletting）1. 引進。2. 嵌入，插入。
  1. The engine-feed system interface is at the turbopump inlet flanges.

    發動機與供應系統的交界是在渦輪泵的進口法蘭盤處。
  2. Unfortunately, the engine room was incommodious, resulting in the air inlet muffler too close to the generator unit and making it inconvenient for maintenance staff to perform operation. in a spirit to avoid such an awkward situation and save the investment on muffling treatment, we suggest the following solution be adopted in future construction of engine rooms

    例如我們以前治理過的某個油機房其進風口外為防火通道，不能佔用，進風消音器只能安裝在油機房內，而油機房內部空間設計又過小，就造成進風消音器距發電機組過近，維護人員操作起來很不方便。
  3. Experimental studies on s1a - 02 gas turbine with water injection into compressor interstage / inlet as well as that on turbocharger self - loop test rig with inlet water injection are introduced. test results are in good accordance with simulation results, wet compression can lower compression work and increase engine power output so engine performance is enhanced, if engine power output is not changed, efficiencies of compressor and this engine become higher and turbine inlet temperature and fuel consumption become lower and if keeping t4 the same as that before wet compression is used, efficiencies become furthermore higher and engine power output increases greatly

    實驗結果和計算結果同樣表明：濕壓縮減少了壓氣機所消耗的壓縮功，增加了燃氣輪機的輸出功率，提高了燃氣輪機性能，如果保持發動機輸出功率恆定，濕壓縮可以提高壓氣機和整個燃氣輪機機組的效率，與此同時，渦輪進口溫度t _ 3 ~ *和燃油消耗率下降；如果保持渦輪排氣溫度t _ 4 ~ *恆定，壓氣機和燃氣輪機機組效率進一步提高，燃氣輪機輸出功率增加。
  4. This engine consists of an inlet, a combustor, and a nozzle.

    這臺發動機由一個進氣道，一個燃燒室和一個尾噴管組成。
  5. Experimental study on the inlet total pressure distortion of a turbojet engine

    某型渦噴發動機進氣總壓畸變的試驗研究
  6. The best compression ratio and fuel injection advance angle are calculated through mess optimization calculation program of language c. on the basis, optimization simulation of inlet and exhaust timing has been carried with the diesel engine working model to increase diesel engine ' s volumetric efficient

    在此基礎上，利用柴油機工作過程模型，對進排氣正時進行了優化計算，以提高柴油機的充氣效率，改善燃燒性能，為進一步改善該機性能指明了方向。
  7. It is possible, by adopting " reverse engineering " to conduct digitized design of inlet and exhaust ports toolings of diesel engine, to improve the fineness of the toolings and castings, shorten toolings development duration

    摘要運用逆向工程進行柴油機進排氣道模具數字化設計，可以提高模具和鑄件的精度、縮短模具開發周期。
  8. Finally, the inlet port and combustion chamber designed and machined is tested on 4100qb. the paper mostly investigates the change of performance targets of the engine that three different grooved chambers including two different re - entrant model and one w model match with various intake port and nozzles, in order to realize the influence of chamber geometry on combustion process. the results analyzed have indicated that re - entrant grooved chambers can enhance the turbulent intension in the chamber, improve the combustion proces of diesel engine on the altiplano, being groove, re - entrant and convex, and have the farther developing potential

    著重研究兩種縮口、一種直口矩形環槽燃燒室與不同進氣道、噴油嘴的組合方案發動機的動力性、經濟性及排放指標的變化，確定燃燒室的幾何形狀對燃燒過程的影響。分析結果表明，由於有矩形環槽、燃燒室縮口以及燃燒室底部凸臺，縮口矩形環槽燃燒室中的紊流得以加強，改善了高原柴油機的燃燒過程，這種燃燒室有進一步發展的潛力。
  9. Research on steady flow test rig for inlet port of an engine

    發動機進氣道穩流試驗臺的開發
  10. Relative to uniform inlet pressure, the distorted or actual profiles may have a rather profound effect on engine performance.

    與均勻的壓力分佈比較起來，畸變的或真實的壓力場對發動性能具有相當大的影響。
  11. These variable geometry components include high pressure - compressor, high - pressure turbine, low - pressure turbine, inlet area ratio of mixer and main nozzle throat area. the results of calculation show that the adjusting of low - pressure turbine and mixer has a remarkable effect on the performance of engine and bypass ratio

    計算結果表明，低壓渦輪和混合器的調節對發動機的性能和涵道比的影響尤為顯著；在其它部件幾何結構不同時，單個部件幾何調節后，發動機性能的變化趨勢是不同的。
  12. This paper investigates the structural parameters of air inlet pipe, air compensating pipe and air compensating valve which influence the air compensation of air compensating valve for motorcycle catalytic converter, the position of air compensating hole, and the relationship of air compensating pressure with engine speed

    本文就影響摩托車催化轉化器補氣閥補氣量的進氣管、補氣管、補氣閥的結構參數，以及補氣孔的位置、補氣壓力隨轉速的變化關系等進行了探討。
  13. Influence of inlet air noise on engine noise

    進氣噪聲對內燃機整機噪聲的影響
  14. For one same engine, the noise level is highly dependent on the rotation speed. when the rotation speed doubles, the air inlet noise can increase by 10 to l5db ( a )

    對于同一臺發動機來說，受轉速的影響最大，轉速提高一倍可導致進氣噪聲增加10 ~ l5db （ a ） 。
  15. This paper involves the refrigeration principle and technology, the thermodynamics principle, the exergy analyses principle and its applications, the sensor principle and its applications, the microcomputer testing technique, the auxiliary engine of the ship etc. at the same time, to realize the measuring of cold store running parameters so that the main equipment of this system can run safely and reliably, measuring points are disposed at inlet and outlet of main devices, and computer detecting technology is used to measure the real time data at every point

    內容涉及到製冷原理與技術，熱力學原理，火用分析原理及應用，傳感器原理與應用，微型計算機檢測技術，船舶輔機等諸多方面的知識。同時，為了實現對冷庫系統運行參數的全程檢測，以利於系統主要設備的安全可靠運行。在系統的主要設備進出口均布置了測量點，同時利用計算機檢測技術對各測量點數據進行在線檢測，檢測軟體是基於魯班組態軟體平臺而開發的，可以實時動態顯示檢測數據及數據的趨勢圖，還可以完整保存歷史數據，以利於分析系統常年運行工況，進一步制定改進措施。
  16. Research on tufftriding technology for inlet valve of 150 series diesel engine

    150系列柴油機進氣門軟氮化工藝研究
  17. The helicopter has more flexibility than any other aircraft, and it ’ s easier to get fod. inlet particle separator is a special device designed for helicopter engine to prevent foreign object be ingesting. it ’ s worth to study fod of the turbine engines

    粒子分離器是用於直升機的渦輪軸發動機的一種專門的進氣凈化裝置，它使外物進入到發動機前分離到機外，以避免被吸入發動機的外來物對發動機構件的損傷。
  18. Numerical simulation of air flow in an engine inlet port

    發動機進氣門處氣體流動數值模擬
  19. Numerical simulation of effect of disturbing on starting state of ramjet engine inlet

    擾動對超聲速進氣道起動狀態影響的數值模擬
  20. The dominating scattering of the aircraft is from the engine inlet, so the analysis and reduction of the electromagnetic scattering from the interior of jet engine inlet cavity have been an important research area

    進氣道終端為發動機渦輪，結構非常復雜，在波長或更小的量級上有復雜的幾何尺寸變化，一般的高頻技術不再適用。
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