wind-cooled 中文意思是什麼
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Research on the wind guide facilities of light air - cooled diesel engine
輕型風冷柴油機導風裝置的試驗研究 -
Fluid experiment ; buff body aerodynamics ; wind engineering ; wind loading on buildings and structures ; modeling wind in an atmospheric boundary wind tunnel ; pedestrian - level wind environment ; wind effects on the efficiency of air - cooled condenser in a large power plant
實驗流體力學，鈍體空氣動力學，風工程， 、建築物和結構物的風荷載研究，大氣邊界層風洞模擬，行人高度風環境，大型電站空冷系統風效應風洞模擬。 -
Frozen the wind spee air - cooled condensation aircrew of the indoor type
室內型風冷式冷凝機組 -
Main technical parameter wind cooled
風冷式冷水機主要技術參數 -
The operating situation of heller style air - cooling steam turbine - generator set is introduced in this paper, and the performance characteristics of the air - cooling system and the steam turbine are analyzed, especially some factors which are important for safely and economically running of the air - cooled steam turbine - generator system such as the back pressure safeguard of the air - cooling steam turbine system, the environmental temperature and environmental wind speed which are influential to the load of the air - cooling steam turbine - generator set, and some experimental investigations of a domestically made air - cooling steam turbine - generator set are introduced in this paper too
=本文介紹了海勒式空冷機組的運行狀況，對空冷機組的運行特性進行了分析，特別是對影響空冷機組安全、經濟運行的幾個主要因素進行了研究，即空冷汽輪機的背壓保護、環境溫度和環境風速對空冷機組出力的影響，並對國產化空冷機組的運行特性進行了實驗研究。 -
According to field testing data analysis, the author find out that buried pipe - in - pipe heat exchanger, which act as a important part of gshp system, can supply sufficient heat flow and its operation performance is better than that of a wind cooled - - heat pump. the author also finds out the self - equilibrium mechanism gshp system operated with buried pipe - in - pipe heat exchanger, which give experiences for design and operation of a gshp system
通過實驗測試與分析，證明了地下埋管換熱器作為地源熱泵系統的重要一環能夠為熱泵提供良好的熱源，使地源熱泵的性能參數優于風冷熱泵，發現了埋管換熱器匹配熱泵運行時獨特的自平衡規律，為設計和運行地源熱泵技術提供了經驗。 -
Film cooling of the surface of a gas turbine blade was studied in a large - scale low - speed opening wind tunnel according to actual requirement of the design of aero - engine. the surface of a gas turbine blade was cooled by cylindrical holes in the experiment, with the hole number of fifteen in stator and eight in rotor
應航空發動機設計的要求，在大尺寸低速葉柵傳熱風洞中分別對發動機渦輪導向葉片和動葉表面的氣膜冷卻特性進行了研究，具體研究在不同氣膜孔出流時，在不同主流雷諾數和吹風比情況下葉片表面局部換熱系數的分佈規律。
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