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发明公开
CN101413439A 旋转式热力发动机 失效 - 权利终止 转让

旋转式热力发动机
摘要：
一种喷气推动的旋转式发动机包括定子和转子，转子可操作地接合于定子，用于使转子相对于定子绕定子轴线旋转。转子包括至少第一和第二推力物质喷射部件，第一推力物质喷射部件限定第一收缩流动区域、位于第一收缩流动区域下游的第一扩张流动区域以及第一排出口，第二推力物质喷射部件限定第二收缩流动区域、位于第二收缩流动区域下游的第二扩张流动区域以及第二排出口。旋转式发动机还包括有上游区域的燃烧区域，并适于使氧-燃料混合物在燃烧区域发生燃烧反应而生成燃烧反应产物，该燃烧反应产物包括将要通过第一和第二推力物质喷射部件的排出口喷出的至少一部分推力物质。旋转式发动机适于使至少一些氧-燃料混合物在燃烧区域的上游部分内燃烧，使得至少一部分燃烧反应发生在燃烧区域的上游部分，旋转式发动机构造成使燃烧区域的上游部分生成的至少一些推力物质引导通过第一和第二推力物质喷射部件的排出口。
摘要（英）：

A jet-propelled rotary engine comprises a stator and a rotor operatively coupled to the stator for rotation of the rotor relative to the stator about a rotor axis. The rotor comprises at least first and second jet assemblies wherein the first jet assembly defines a first converging flow region, a first diverging flow region downstream of the first converging flow region, and a first discharge port and wherein the second jet assembly defines a second converging flow region, a second diverging flow region downstream of the second converging flow region, and a second discharge port. The rotary engine further comprises a combustion region having an upstream portion and is adapted to cause a combustion reaction of an oxygen-fuel mixture in the combustion region in a manner to form combustion reaction products which comprise at least a part of thrust matter to be discharged through the discharge ports of the first and second jet assemblies. The rotary engine is adapted to combust at least some of the oxygen-fuel mixture in the upstream portion of the combustion region such that at least a portion of the combustion reaction occurs in the upstream portion of the combustion region and is adapted and configured to channel at least some of the thrust matter formed in the upstream portion of the combustion region through the discharge ports of the first and second jet assemblies.

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