combustor

combustor

1. Research on 20 MW MHD Coal-fired Combustor Hot-tests

20MWMHD燃煤燃烧室热态试验研究

2. 8 MW_t CIRCULATING FLUIDIZED BED COMBUSTOR

8MW_t循环流化床燃烧装置

3. EXPERIMENTAL STUDY ON NON-UNIFORMITY OF FUEL-AIR PREMIXING IN A DLN COMBUSTOR

DLN燃烧室的燃料-空气预混均匀性研究

4. DEVELOPMENT OF HELMHOLTZ-TYPE PULSE COMBUSTOR

Hel mholtz型脉动燃烧器的研制

5. Appliication of Dense/Bright XWD Cyclone Combustor in 670t/h Boiler

XWD 型旋流浓淡燃烧器在 670t/h 锅炉上的应用

6. CO combustion model for circulating fluidized bed combustor

一氧化碳在循环流化床燃烧室中的燃烧模型

7. A new adjustment method of combustor outlet temperature field

一种新颖的燃烧室出口温度场调试方法

8. The location of the instability zones is dictated by the combustor geometry and the steady-state combustion characteristics.

不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。

9. Either stall or surge may result in combustor blowout

不管是喘振或者爆音，都将引起燃烧室的熄火。

10. The comparison indicates that the source term method can predict pressure distribution of the combustor and can meet the need of the vehicle configuration and integral design.

与直联式试车台实验数据对比表明，该方法能够较好地模拟冲压发动机内压力分布，能够满足飞行器气动／推进一体化构型方案设计及总体方案设计阶段的需求。

11. The challenge of adequately cooling the nozzle guide vane directly downstream of the combustor is compounded by a complex vortical secondary flow at the junction of the endwall and the airfoil.

为了使空气在管道中能克服更大的阻抗，本研究设计管道风扇出口导流叶片，试图将流出叶轮之流体由迴旋流动导为直接流出风机，以达到提升风机性能的目的。

12. An Energy-bypass system located parallel to combustor has been applied for the performance improvement at high flight speed and extension of flight envelop.

为了提高冲压发动机在更高速度区内的性能,扩展发动机的运行速度范围,需要在并行于发动机的燃烧室处附加一套能量旁路系统。

13. In order to improve the design of the swirler and flame tube，thereby to improve the performance of combustor, the structure of fuel spray in combustor needs to be investigated intensively.

为了改进燃烧室旋流器和火焰筒的设计，提高整个燃烧室的工作特性 ，需要深入研究燃烧室喷雾两相流场。

14. To investigate the mechanism of scalar transport, the methane fuel concentration and temperature transport and diffusion in ramjet dump combustor was simulated by large eddy simulation.

为弄清突扩燃烧室内标量输运机理,采用大涡模拟方法数值模拟了几何结构简化的冲压发动机突扩燃烧室内湍流流动中燃料浓度以及温度等标量的扩散和输运过程。

15. All these works done were hoped to be available for the combustor configuration design.

为燃烧室结构设计与设计参数选择提供了参考。

16. A new type of combustor,a double-chamber vaporizing combuster has been developed for heating apparatus of heating calibration tunnel.

介绍了一种用于热校准风洞作加热装置的新型蒸发式双腔高温燃烧室。

17. The application of Pentex combustor for aluminium melting and holding furnace is introduced.And some valid measures to prevent the problems appeared in using are given.

介绍了百特斯燃烧器在铝熔炼保温炉上的应用,并针对其在使用中出现的问题作了行之有效的改进。

18. Combustor parameter of all gas-phase iodine laser is studied using the power of HF fundamental laser as a test criterion.

以HF基频激光功率大小作为判断依据, 对燃烧驱动全气相碘激光的燃烧室参数进行了考察。

19. Researchers have done much research for different combustor configurations.The configuration with backwind step is widely adopted in the design of scramjet combustor.

以往国内外的研究工作者对不同结构的燃烧室进行了大量研究,其中突扩型结构是主流的设计思想之一。

20. Circulating ash is the heat carrier from the combustor to the gasifier to pyrolyze the coal, and the char is the fuel of the boiler.

以循环床锅炉循环灰为热载体、部分气化产生的半焦为锅炉燃料的煤的部分气化技术中，循环灰对降低焦油产率、提高煤气产率是有利的。

21. Repairing of Single-Cylinder Combustor of Low calorie value Gas Turbine

低热值燃气轮机单筒燃烧室修复

22. Full-Scalc Liquid Fuel Ramjet Combustor Tests.

全尺寸液体冲压发动机燃烧室试验。

23. The flow of fluid in the entrained slagging coal powder combustor are analysed.Specially, the center reflux area and its effects on the flow of fluid slag are analysed.

分析了液排渣粉煤燃烧器内的流体流动问题,着重分析了中心回流区及其作用。

24. In addition,the temperature distribute on radial and on exit field of combustor were presented.It is useful for the hot design of the turbine nozzle blades.

分析结论可以用于弹用涡喷发动机燃烧室出口温度场预测和涡轮导向器叶片热设计。

25. tangential trapped vortex combustor

切向驻涡燃烧室

26. Experiment results in a small capacity combustor and a diesel engine were introduced.

初步试验表明，精细水煤浆在该燃烧器中的燃烧热强度接近柴油；

27. Modeling approach of supersonic inlet,combustor and variable convergent nozzle were studied respectively by using the small deviation linear theory and piecewise-lumped parameter method.

利用小偏离线性化理论和分段集总参数法,分别研究了超声速进气道、燃烧室和可调收敛喷管的建模方法。

28. single trapped vortex combustor

单涡驻涡燃烧室

29. The compressed air is then delivered to the combustor where fuel is added, ignited and burned.

压缩后的空气被送入燃烧室，与喷入的燃料混合后被点燃并燃烧。

30. Refers to overall structure of the engine, designed test apparatus of the combustor and carried out the several performance experiments.

参照发动机的总体结构，设计了燃烧室的试验器，对燃烧室进行了一定的性能试验。

31. It was found that an increase in the stability of the combustor was obtained simply by gelling the hydrazine.

发现简单地通过肼胶化的方法可使燃烧室的稳定性提高。

32. For swirl combustor, the predicted temperature distribution of DO model were in good agreement with those measured by experiment and were better than those of the SHF model.

另外，DO模型在计算时间和边界处理等方面比区域法优越；

33. Compared with other natural gas combustor, this combustor can generate the second combustion and form circumfluence of smoke.

同一般天然气燃烧器相比,这种燃烧器既能产生二段燃烧,又能促进一定量的烟气回流。

34. NUMERICAL SIMULATION OF TURBULENT FLOWSIN SWIRL COMBUSTOR WITH COAXIAL JETS

同轴射流旋流燃烧室内湍流流动的数值模拟

35. co-axial swirl stratified flow combustor

同轴旋转分层流燃烧器

36. Effect of Nozzle and Swirler Number on Short Annular Combustor Performance

喷嘴和旋流器数目对短环形燃烧室燃烧性能的影响

37. Influence of Injection Mode on Flame Stability in Dual-mode Scramjet Combustor

喷注方式对双模态冲压发动机燃烧稳定性的影响

38. Therefore by regulating swirl number of combustor NO emission caw be reduced.

因此,适当调整燃烧室的旋流数可以降低NO排放.

39. Computation of ablation of thermal-protection layer in solid rocket ramjet combustor

固体火箭冲压发动机燃烧室热防护层烧蚀计算

40. A Numerical Study on Ignition and Combustion of Boron Particles in the Flowfield of a Ducted Rocket Secondary Combustor

固冲发动机补燃室内硼颗粒点火和燃烧数值研究

41. Fig. 2 Schematic of the combustor model.

图2微燃烧器数值模型内部结构。

42. The effect of combustor pressure on soot concentrati on and flame radiation was investigated in a small model gas turbine combustor with an air-blast atomizer.

在一个小型高压燃烧试验台上研究了燃烧室采用空气雾化喷嘴后,燃烧室压力对燃烧室内烟粒浓度和火焰辐射的影响。

43. A stable positive and reverse rotating airflow was observed in the combustor of a tangentially firing boiler and is similar to the coanda effect.

在冷态模拟试验中，发现切向燃烧的炉膛内存在着稳定的正旋和反旋现象，它与射流附壁效应相似，属于双稳结构。

44. Furthermore, as the total step height is the same, the combustor configuration with one backwind step has higher performance than the combustor configuration with two backwind step.

在台阶高度一定的条件下,单台阶结构的燃烧室具有更好的燃烧性能。

45. The combustor consisted of a vertical tube opened at both ends with a swirling-stream flame stabiliser located near the middle of its lower half.

在实验 中所采用的脉劝燃烧器是基于里克管原理设计的。

46. As the total expanding angle is the same, two-sides expending combustor configuration has higher performance than one-side expending combustor configuration.

在总扩张角一定的条件下,双面扩张结构的燃烧室性能较单面扩张的占优势;

47. Based on the research,simulates the combustor with a ring fin indicate that the ring fin can enhance the turbulence of the mixed gas in the combustor,improve combustion status,increa.

在此基础上,模拟了带有环形翅片燃烧室的情况,表明环形翅片能增强微燃烧室内混合气体的湍流扰动,改善燃烧状况,有效地提高燃烧效率。

48. Then the flow fields of scramjet combustor with fix geometry and isolator are simulated at different inflow Mach number and the influence of direction of injection fuel to flow structure are analyzed.

在此基础上对固定几何、带隔离段的双模态超燃冲压发动机在不同飞行马赫数下的流场进行了模拟，最后分析了不同的燃料喷射方向对燃烧室和隔离段流场的影响。

49. In furnace sorbent injection the limestone or dolomite is injected with or without coal in the high temperature zone of the combustor where calcination and sulfation takes place and as a result removal of SO2 is achieved.

在炉内吸附剂注入法中，石灰石或白云石在燃烧炉的高温区同煤一起注入（或分别注入），煅烧作用和硫酸盐化作用都发生在这个高温区，同时可消除二氧化硫。

50. One of the main combustion characteristics is the burning rate, which is influenced by intrinsic flame instabilities, external turbulence and flame interaction with walls of combustor and sound waves.

在研究中使用一个双环同轴喷流燃烧器，于燃烧器的中心圆管提供气态甲烷充作燃料，而外环圆管则供给空气，以产生双环同轴喷流扩散火焰。

51. In this system combustible premixed gases change their direction periodically, and flow into a combustor from two ends.

在该系统中,可燃预混气周期性换向,分别从两端流入燃烧器。

52. The wall temperature distribution is tested on an annular combustor by using thermocouple and temperature-indicating paint.

壁温分布试验在全环形燃烧室试验台上进行，采用热电偶和示温漆测量。

53. The results show that ejector combustor geometry is the key factor to ejector rocket relative thrust in SMC combustion mode, and primary rocket chamber pressure plays a subordination role.

实验结果表明，引射器后体结构对于提高SMC二级燃烧模式下引射火箭的相对推力非常关键，而一次火箭工作压强的作用相对较小。

54. Combustor dome design with three swirlers was experimentally investigated in order taken to widen the operation stability range.

对有三旋流器的单头部燃烧室进行了燃烧性能的实验研究，进行了慢车工况的贫油熄火过程及大工况的冒烟性能的研究。

55. Elastoplastic finite element analysis and low cycle fatigue life prediction of an engine combustor case were completed.

对某发动机燃烧室外套进行了弹塑性有限元分析和低循环疲劳寿命预测。

56. The characteristic of static pressure profiles in supersonic combustor was analyzed.

对超声速燃烧室内的静压分布特点作出了分析；

57. This paper analyzes the type of snail boiler rotory combustor, describes the calculating process of strength stable, and comes to a comclusion of qualified strength.

对锅壳式锅炉回燃室的结构型式进行了分析，并通过分析详述了强度稳定计算的过程，得出强度合格的结论。

58. oil-minimum ignition combustor

少油点火燃烧器

59. Research on primary jet of a reverse flow combustor model with swirl cup

带旋流杯的模型回流燃烧室主燃孔射流研究

60. The model of combustion fraction for dense phase in circulating fluidized bed combustor has been built up, based on thermal balance, gas analysis and total gas amount.

建立了基于热平衡法、烟气分析法和烟气量法的循环流化床锅炉燃烧室密相区燃烧份额计算数学模型,并分析比较了各种模型的特点。

61. Stowe R A, Champlain A De, Mayer A E H J. Modeling combustor performance of a ducted rocket[R]. AIAA paper 2000-3728.

张炜,方丁酉,夏智勋,等.非壅塞固体火箭冲压发动机工作特性研究[J].固体火箭技术,1999,22(4):10-13.

62. DONBAR J,POWELL O,GRUBER M,JACKSON T.Post-test analysis of flush-wall fuel injection experiments in a scramjet combustor[R].AIAA 2001-3197.

张鹏,俞刚.超燃燃烧室一维流场分析模型研究[J].流体力学实验与测量,2003,17(1):88-92.

63. CH chromatophore cell COL circulating fluidized bed combustor

循环流化床燃烧室

64. Application of Microcomputer in Aeroengine Combustor Test

微机在航空发动机燃烧室试验中的应用

65. Micro combustor is one of the most important components of micro thermophotovoltaic (MTPV) system.

微燃烧室是微热光电(MTPV)系统的重要组成部分。

66. constant temperature combustor

恒温燃烧室

67. annular combustor with slinger

折流燃烧室

68. A novel coal combustor and its experimental system were designed for igniting the cold pulverized coal flow by high temperature air (HTA).

提出了一种新型的高温空气煤粉直接点火燃烧器，并建立了相关试验系统平台。

69. Abstract A numerical study of the cold flowfield of a hydrocarbon fueled model scramjet combustor have been completed with the NUMECA, which is a famous computational fluid dynamic software .

摘 要 超声速燃烧一直以来被视为人类采用吸气式推进器实现高超声速飞行的最关键的技术难题之一。

70. Experiments of pulverization and evaporation performance of two kinds evaporating tubes as fuel spray properties for the e turbine combustor have been presented.

摘要为了研究满足燃烧室雾化要求的雾化方式，设计了采用侧喷和逆喷供油方式的两种蒸发管，并对其分别进行了雾化和蒸发率两方面的实验。

71. To investigated the ignition and lean blow out performance of a trapped vortex combustor (TVC) test rig, abundant experiments have been employed in variety inlet conditions.

摘要为了研究驻涡燃烧室拓宽燃烧边界的能力，设计了一种驻涡燃烧室实验件，并对其点火性能和贫油熄火特性进行了实验研究。

72. An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.

摘要为某微型涡喷发动机设计了一个蒸发管环形燃烧室。

73. The experimental investigation was conducted for the fuel-circumferential-staging combustor with two domes to improve the lean blowout fuel air ratio.

摘要为降低贫油熄火油气比，对双头部燃烧室进行了燃油周向分级贫油熄火模拟实验研究。

74. The numerical simulation was used to study the effusion holes on the longitudinal wavy liner in the combustor.

摘要对燃烧室内开有发散孔的纵向波纹隔热屏进行了数值模拟。

75. Increasing the combustion efficiency of the micro combustor to the greatest extent is very important to the micro thermophotovoltaic systems.

摘要最大化提高微燃烧室的燃烧效率对于微热光电系统是非常关键的。

76. The transient turbulent flows were predicted by large eddy simulation in a model combustor with a V gutter flame holder.

摘要本文采用三种不同亚网格尺度模型对带有V型稳定器的模型燃烧室二维瞬态紊流流动进行了大涡模拟。

77. The fragmentation influences the char combustion behavior in a fluidized bed combustor.

摘要流化床燃烧中破碎特性影响了焦炭的燃烧。

78. An experimental study of cold flow field was conducted under entrance Mach number 2.5 on a supersonic combustor experiment rig with subsonic pilot combustor and stream wise vortices mixer.

摘要结合对应的数值计算，对一种带亚声速预燃室和流向涡掺混器的超声速燃烧模型燃烧室实验台，在其进口马赫数为2.5的来流条件下，进行了冷态流场的实验研究。

79. This paper is dealt with application situation for developed regenerative radiant-tube combustor on use of zincked-plated plank production line continuous anneal furnace in Guangdong Foshan Guangheng Iron and Steel Co. , Ltd.

摘要论述了蓄热式辐射管燃烧器在佛山南方广恒钢铁公司连续热镀锌生产线还原退火炉上的应用情况。

80. Abstract: To counter the abuse existing in air heating app aratus of gas combustor at ammoniumsulfur drying system,the technique refo rmation of heater is made and is successful.

文摘:针对杭钢焦化硫铵生产线硫铵干燥系统的煤气燃烧器空气加热装置存在的弊端，进行了技术改造，并取得了成功。