Three-cavity scramjet combustor has second elements that are attached with first element at position parallel to horizontal plane and third elements attached with second element at slanted position with specific angle with respect to second element
	MALHI G S; CHAND D S; BRANESH A; KOLEY G; VINOTH K G; BANERJEE S
	2023-07-20
专利权人	UNIV CHANDIGARH (UNCD-C)
申请日期	2023-07-20
专利号	IN202311048961-A
成果简介	NOVELTY - Three-cavity scramjet combustor comprises a hollow body (1) to be fixed within a scramjet installed with a fuel inlet to inject fuel within the body that is passed through three cavities (3a, 3b, 3c) consecutively carved within body for appropriate mixing of fuel by reorienting flow stream and increasing combustion efficiency by passing unburnt fuel in subsequent cavities, where each of cavities has a primary and secondary sets (4,5) of a first (4a,5a), second (4b,5b) and third element (4c,5c) arranged in a manner that first elements are attached with body at 45 degrees inclination with respect to horizontal plane of body. The second elements are attached with first element at a position parallel to horizontal plane and third elements are attached with second element at a slanted position with an angle of 45 degrees with respect to second element. USE - Three-cavity scramjet combustor. ADVANTAGE - The combustor is capable of increasing the combustion efficiency of scramjet engine by ensuring proper utilization of the unburnt leftover fuel that aids in producing an ample amount of thrust to aid in propulsion of the engine at a supersonic speed. DESCRIPTION OF DRAWING(S) - The drawing illustrates an isometric view of a three-cavity scramjet combustor. 1Hollow body 3a-3cCavities 4a,5aFirst element 4b,5bSecond element 4c,5cThird element
IPC 分类号	B01D-019/00 ; F02C-007/22 ; F02K-007/10 ; F02K-007/14 ; F23C-007/00
国家	印度
专业领域	化学化工
语种	英语
成果类型	专利
文献类型	科技成果
条目标识符	http://119.78.100.226:8889/handle/3KE4DYBR/21223
专题	中国科学院新疆生态与地理研究所
作者单位	UNIV CHANDIGARH (UNCD-C)
推荐引用方式 GB/T 7714	MALHI G S,CHAND D S,BRANESH A,et al. Three-cavity scramjet combustor has second elements that are attached with first element at position parallel to horizontal plane and third elements attached with second element at slanted position with specific angle with respect to second element. IN202311048961-A[P]. 2023.

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