螺旋發動機 的英文怎麼說
中文拼音 [luóxuánfādòngjī]
螺旋發動機
英文
screw engine-
The first modern torpedo ( 1866 ) carried an 18 - lb ( 8 - kg ) charge of dynamite in its nose and was powered by a compressed - air engine driving a single propeller ; its range was 200 - 700 yards ( 180 - 640 m )
第一枚現代魚雷( 1866 )在其頭部裝載了8公斤的炸藥,並用壓縮空氣發動機帶動單螺旋槳推進;射程為180 640公尺。Jet engines with which most modern high-speed aircrafts are equipped develop thrust on the same principle as the propellers of conventional aero-engines.
大多數現代高速飛機裝備的噴氣發動機產生推力的原理,與普通航空發動機的螺旋槳相同。Disigning coolant channel on the firebox of liquid rocket engine to loxodrome ( equal - angle helix ) groove can improve firebox coolant capability greatly. because the width dimension of loxodrome groove is narrow and the depth is deep, some machining methods are incapable, such as end - milling or electrochemistry. according to the peculiarities, a cnc disk - cutter - milling method which is composed of five motion axes with four simultaneously interpolated ones is researched. because most firebox generatrix is composed of complex curves, it is very difficult to get cnc cutting program with manual means. in order to deal with the problem, the loxodrome mathematics model is studied, and an auto - programming software system is developed. the software system can generate cnc cutting program of loxodrome on many kinds of turned surface. the constriction - distension segment of firebox is the most representative workpiece. the sharp changing of its generatrix slope makes loxodrome milling difficult. with the theory analyzing and practice cutting experiment, some applied techniques, which include milling mode and direction, choosing cutter diameter and cutting start point setting, are developed. adopting the technology above, tens regular workpiece have been manufacturing. the two - year manufacture practice has confirmed the validity and feasibility of developed loxodrome coolant channel milling method. the developed technology is also worth to be referenced to other similar workpiece
將液體火箭發動機燃燒室的冷卻通道設計為斜航線(等傾角螺旋線)槽形,可以大幅度改善燃燒室的冷卻性能.斜航線冷卻槽的槽寬尺寸較小而槽深尺寸較大,所以無法使用棒銑刀銑削、電化學等加工方式.針對這些特點,提出了五軸控制、四軸聯動的數控片銑刀銑削加工方法.由於燃燒室外表面的母線輪廓復雜,手工編制數控加工程序難度大.為了解決數控加工程序的編制問題,研究了斜航線的數學模型,開發了自動編程軟體系統.使用該系統,可以生成多種母線輪廓回轉體外表面上的斜航線數控加工程序.燃燒室收斂-擴張段的母線斜率變化大,加工難度大,是斜航線冷卻通道加工的最典型工件.經過理論分析和實際切削實驗,研究了針對該類型工件的片銑刀直徑選擇、銑削方式和方向、刀具調整和起刀點的設置等多項實際的加工方案.採用上述的一系列技術,已經成功地加工了數十個合格工件.經過兩年多的實際生產過程應用,驗證了所開發的斜航線冷卻通道加工方法的正確性和可行性.這些加工技術的研製成功,對其他相似類型零件的加工亦具有參考意義Different nacelle with deeper ross - section and intake over propeller shaft
發動機艙、螺旋槳軸處的進氣口有一些不同。The turboprop engine is very much like the turbojet. it has an additional part, a propeller.
渦輪螺槳發動機與渦輪噴氣發動機十分相似。它多了一個螺旋槳部件。Article 10 the rights to a civil aircraft as referred to in this chapter include the rights to the airframe, engines, propellers, radio apparatus of the civil aircraft and all other articles intended for use in such civil aircraft, no matter whether they are installed thereon or separated temporarily therefrom
第十條本章規定的對民用航空器的權利,包括對民用航空器構架、發動機、螺旋槳、無線電設備和其他一切為了在民用航空器上使用的,無論安裝于其上或者暫時拆離的物品的權利。General specification of turboshaft and turboprop engines for aircraft
飛行器渦輪軸和渦輪螺旋槳發動機通用規范The two astazou turboprops are mounted in slender nacelles in the leading edges of the wings and drive three - blade propellers
兩臺發動機安裝在機翼上小巧的發動機艙內,各驅動一個三葉螺旋槳。In this thesis hydraulic experimental studies and theoretical analyses on the vortex - flow drop shaft were conduced and the following results were accomplished : ( 1 ) in the model test some hydraulic characteristics including the shape of air core in the center of the drop shaft, the radial distribution of water flow velocity and the distribution of pressure on the wall of the drop shaft were measured under the condition of high water head above 250m and large discharge above 1400m3 / s. ( 2 ) a kind of computational method for the spiral water flow in the air core region of drop shaft was discussed and applied and the results agree the experimental data well. ( 3 ) the total ratio of energy dissipation in the drop shaft can reach 90 % and the energy dissipation in every region was discussed quantitatively
本文通過試驗研究與理論分析對旋流式豎井泄洪洞應用於高水頭、大泄流量情況時存在的一些水力學問題進行了研究和探討,取得以下主要成果:一、結合小灣工程導流洞改建,對高水頭( 252m ) 、大泄流量( 1400m ~ 3 s )條件下旋流式豎井中的水流運動特徵進行了比較全面的測量,包括空腔形態、徑向流速分佈及井壁壓強等;二、提出了豎井空腔段螺旋水流水力計算方法,其計算結果與實測值吻合良好;三、利用試驗與計算結果,對旋流式豎井的消能機理進行了探討,對豎井各部分的消能能力有了總體認識;四、對豎井下部消力井的合理井深進行了優化試驗研究,發現消力井合理深度為0 . 9d左右;五、通過試驗研究,歸納出豎井水流總摻氣量估算方法,為導流洞排氣方案的設計提供了參考依據;六、在高水頭、大流量條件下,豎井空腔段下部流速很高,盡管水流螺旋運動引起的離心力可以確保井壁壓強保持正壓,但空化數依然較低,因此豎井的空化空蝕始終是工程界關注的重大問題。Application shall be filed with the competent civil aviation authority under the state council by the manufacturer for export airworthiness certificate with respect to the export of civil aircraft and its engines, propellers and on - board equipment
出口民用航空器及其發動機、螺旋槳和民用航空器上設備,製造人應當向國務院民用航空主管部門申請領取出口適航證書。Specification for propeller shaft ends and bosses for inboard - engined pleasure craft
內列發動機船舶的螺旋漿軸端和螺旋槳轂規范According to the requirements of propeller aerocraft model test in wind tunnel, specifications of the driven motor is presented by aerodynamic analysis, and a short - term operated high power density three - phase induction motor is developed with reasonably designing the motor, such as electromagnetism load, heat checkout and high - efficiency heat exchanger
摘要針對螺旋槳飛機模型帶動力風洞實驗要求,通過氣動性能分析提出驅動電機的技術指標,在滿足結構約束的條件下,通過合理設計電機的電磁負荷、校核發熱、採用高效冷卻裝置等,研製出短時工作制高功率密度三相異步電機。Abstract : specific analysis of developing prospect and application of clutch type spiral press with heavy duty ( 25mn or more ) has been done to promote application spread in die forging process
文摘:針對大噸位離合器式螺旋壓力機(主要指噸位在25mn以上的壓力機)的開發前景及應用情況,作出了一些具體分析,以推動該類設備在模鍛工藝上的廣泛應用。By adjusting the fuel rectifying screw and then increasing the fuel quantity per cycle, the loss of the maximum power of e30 engine ca n ' t exceed 10 % of the maximum power of diesel, and the loss of the maximum torque can be controlled within 2 percent
通過旋出油量校正螺釘,增大燃料供給量,可以使e30混合燃料發動機的最大功率損失控制在10以內,最大轉矩損失控制在2以內。Hydraulic turbines, storage pumps and pump - turbines - tendering documents - part 4 : guidelines for technical specifications for kaplan and propeller turbines
液壓水輪機,蓄水泵和水泵水輪機.報價文件.第4部分:轉漿式水輪機和渦輪螺旋漿發動機的技術規范導則Article 35 application shall be filed with the competent civil aviation authority under the state council for production certificate and maintenance certificate for the production and maintenance of civil aircraft and its engines, propellers and on - board equipment
第三十五條生產、維修民用航空器及其發動機、螺旋槳和民用航空器上設備,應當向國務院民用航空主管部門申請領取生產許可證書、維修許可證書。In order to solve it radically, making power assembly of bj1036e2f1 light truck the research object and through dynamic simulation analysis of power assembly, this thesis obtains the distribution rules of forces of the bolts linking three shells mentioned above and the relation between forces of the bolts and rotate speed of engine. after finite element mode analysis of these three shells, inherent frequency and vibration model of shell of power assembly are gained, and thus its dynamic character is realized. based on computer simulation analysis, experimental model of power assembly is acquired by vibration test and strength test of shell of power assembly, and the relation of forces of the shell and rotate speed of engine and imbalanced mass of rotate components is studied
為了從根本上解決該問題,本論文以bj1036e2f1輕卡動力總成為研究對象,通過動力總成的動力學模擬分析,找出了三殼之間聯接螺栓受力的分佈規律和螺栓受力與發動機轉速的關系;通過三殼的有限元模態分析,得到了動力總成殼體的固有頻率與振型,從而了解了動力總成殼體的動態特性;在計算機模擬分析的基礎上,通過動力總成殼體的振動測試和強度測試,得出了動力總成的試驗模態,並研究了殼體受力與發動機轉速和旋轉部件不平衡質量的關系。The thesis basically realizes the engine testbed using fuzzy pid controlling and loading according to the propeller characteristic
本文初步實現了模糊pid控制演算法並應用於發動機臺架試驗和按照螺旋槳特性模擬加載負荷。This thesis attempts to develop a automatic testbed. the testbed not only has general function, but has special function loading according to the propeller characteristic
本文嘗試開發的發動機臺架,不僅具有常規功能,而且具有模擬螺旋槳特性加載的功能。This should happen through a process called stochastic resonance : the spiralling molecules get preferential treatment, so to speak, because they stand out in what is otherwise an environment of random movements
這一切都是通過被稱為隨機共振的過程來發生:可以說,由於其脫離了隨機運動的環境,螺旋運動中的分子能獲得額外有利的運動環境。分享友人