1. Either stall or surge may result in combustor blowout.

2. It is shown that the combustor has a high intensity of combustion and slagging ratio, and the temperatures basically come up to standards of foreign similar systems.

3. By optimizing ejector combustor geometry, ejector rocket in SMC combustion mode can obtain comparable thrust augmentation.

4. System structure is introduced for control of combustor temperature in enamelling machine with single-board computer.

5. 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.

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

7. The combustor is of the vaporiser type, and hence is equipped with three preheat burners.

8. Self-sustained oscillation will appear in gas turbine combustor when unstable combustion couples with acoustic.

9. The combustor resonance properties are portrayed by instability zones,(/combustor.html) one z one for each acoustic mode.

10. This engine consists of an inlet, a combustor, and a nozzle.

11. The flame tube of combustor consists of fuel nozzle, double inverse swirlers, venturi flare and primary holes and so on.

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

13. A gas turbine combustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side.

14. The methodology for scramjet combustor performance analysis and evaluation is build up.

15. 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.

16. A mathematical model describing combustion in a high pressure liquid hypergolic bipropellant(UDMH/H2O4) rocket engine combustor has been developed.

17. The axis of a flame tube being parallel to that of an engine, the flame crossover tube of a turbine combustor is usually orthogonal with respect to the flame tube.

18. Predicted gas flow field in the free board of a vortexing fluidized-bed combustor gives plausible results which reveals the non-isotropic featu...

19. On the contrary, if temperature gradient is relatively low, combustor only undergo low compressive stress at high temperature. The combustor of engine has a longer life length.

20. In this paper, both the cold condition flow characteristic experiment and the hot condition experiment have been done in a novel lower ash coal pulverized combustor.

21. It is not only of strong flame stability and combustion intensity but also in the position to prevent coking in the flat jet combustor.

22. The result showed that the advantages offered by the catalytic combustor is that catalytic combustion can be carried out over a wide air: fuel ratio and at low temperature with high heat efficiency.

23. The following conclusion are obtained: the method of pulse-inject fuel is a very useful technology for mixing enhancement, and the combustor with dual cavity and pre-heated flow is a practical design.

24. The fragmentation char combustion behavior in a fluidized bed combustor.

25. The results have showed that local port flanges and welded joints are dangerous areas on the combustor case.

26. The semicoke is poured by turning tray of the sealing chamber of semicoke screw conveyer to the speed-up zone of the aerofountain combustor (hereinafter referred to as AFC).

27. In this paper, the method and some results of cold experimental investigations of liquid slagging coal-fired combustor are described.

28. The cooler consists of an absorber, a solution pump, a solution heat exchanger, a desorber , a evaporator, a condenser and a combustor.

29. The annular multi - hole radial jets have important effect on combustor liner.

30. The experimental results of the axial velocity and the tangential velocity in combustor have been given.

31. The present invention relates to an ultra low injection angle fuel holes in a combustor fuel nozzle.

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

33. Aircrafts have continued to fly on aviation fuels, kerosene fuel or a wide-cut fuel blended from heavy naphtha and kerosene, burned in the gas turbine combustor for many years.

34. The fore-end of the chamber wall is thus cooled more effectively. Additionally, a larger injection angle reduces the peak temperature of the fore-end wall of the combustor.

35. Micro combustor is one of the most important components in a micro - thermo - photovoltaic MTP system.

36. 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.

37. The Ground start ignition,[Sentencedict] altitude restart ignition and combustion stability are important performance indexes to the combustor.

38. Its equipment is formed from fan, flammable gas source, combustor, feeder, spouted bed, cyclone separator, static dust-remover, condensator, flowmeter, thermometer and control device.

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

40. A new style boiler used in power plant adopts a design of double channel axial swirling combustor, transverse impact arrangement, double breeching tail, single reheating and balanced ventilation.

41. Predicted gas flow field in the free board of a vortexing fluidized-bed combustor gives plausible results which reveals the non-isotropic...