초록 ▼

A pilot for a scramjet provides a flame front whose arrival at the wall of the scramjet combustor is delayed thereby reducing combustor heat load. By combining in-stream injection of fuel with an interior pilot and a lean (fuel-poor) outer annulus, the bulk of combustion is confined to the scramjet

A pilot for a scramjet provides a flame front whose arrival at the wall of the scramjet combustor is delayed thereby reducing combustor heat load. By combining in-stream injection of fuel with an interior pilot and a lean (fuel-poor) outer annulus, the bulk of combustion is confined to the scramjet combustor center. This concept, referred to as “core-burning,” further reduces combustor heat load. One such pilot is for a two dimensional scramjet effective to propel a vehicle. This pilot includes a plurality of spaced apart struts separated by ducts and a strut pilot contained within each strut. A second such pilot is for an axisymmetric scramjet engine has, in sequence and in fluid communication, an air intake, an open bore scramjet isolator and a scramjet combustor. This centerbody pilot pod includes a pilot isolator disposed between the air intake and a pilot diffuser, the pilot diffuser disposed between the pilot isolator and a pilot with the pilot disposed between the pilot diffuser and a pilot combustor. The pilot pod is in axis symmetry around a central axis of the scramjet isolator and supported by a plurality of struts extending from an inner wall of the open bore to an outer surface of the centerbody pilot pod.

대표청구항 ▼

What is claimed is: 1. A centerbody pilot pod for a scramjet engine, where said scramjet engine has, in sequence and in fluid communication an air intake that is effective to divide a supersonic stream of air into a pilot air portion and a main air portion, a main isolator and a main combustor, sai

What is claimed is: 1. A centerbody pilot pod for a scramjet engine, where said scramjet engine has, in sequence and in fluid communication an air intake that is effective to divide a supersonic stream of air into a pilot air portion and a main air portion, a main isolator and a main combustor, said centerbody pilot pod comprising: a pilot isolator effective to receive said pilot air portion, which is from 3% to 10%, by volume, of said supersonic stream and to reduce said pilot air portion to subsonic, said pilot isolator disposed between said air intake and a pilot diffuser; said pilot diffuser disposed between said pilot isolator and a pilot flameholder; said pilot flameholder disposed between said pilot diffuser and a pilot combustor; wherein said centerbody pilot pod is disposed in axis symmetry along a central axis of said main isolator and supported by a plurality of struts extending from an inner wall of said main isolator to an outer surface of said centerbody pilot pod such that the exhaust from said pilot combustor is confined to said main combustor center and said main air portion travels around said centerbody pilot pod. 2. The centerbody pilot pod of claim 1 wherein said plurality of struts include pilot fuel injectors effective to deliver fuel to said pilot isolator and to said pilot flameholder. 3. The centerbody pilot pod of claim 2 wherein main fuel injectors are located on said inner wall of said main isolator and on an outer surface of said pilot pod. 4. The centerbody pilot pod of claim 2 wherein a combination of said plurality of struts and said pilot pod occupy less than 20% of a cross sectional area of said main isolator. 5. The centerbody pilot pod of claim 2 wherein a nozzle affixed to said pilot combustor is effective to deliver exhaust from said pilot combustor to said main combustor. 6. The centerbody pilot pod of claim 5 wherein main fuel injectors located on said inner wall of said main isolator are in a no-flow position while a remainder of said main fuel injectors are in a provide flow position. 7. The centerbody pilot pod further including main fuel injectors along bases of said struts.