A Closed-Loop Adaptive Adjustable Ejector and Rocket Nozzle
A self-adaptive adjustment and ejector technology, applied in the field of ejectors, can solve the problems of inability to change the flow rate and flow rate of working fluid and ejection fluid, small application range, waste of resources, etc., so as to improve the mixed output effect and improve the work efficiency. Scope, the effect of strengthening the blending ability
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Embodiment 1
[0038] as attached Figure 1-3Shown is a closed-loop self-adaptive adjustable ejector. In this embodiment, the ejector has an axisymmetric nozzle configuration as a whole, and each component pipeline is cylindrical, including a fixed connection with an upstream device and a The working fluid upstream pipeline 15 whose overall shape is tapered, the upstream device can be rockets, aircraft and other spacecraft components, and can also be industrial equipment components; the tail of the working fluid upstream pipeline 15 extends into the injection fluid channel 3 Inside, and leave a certain gap to form a channel for the injection fluid, the injection fluid channel 3 is sequentially sealed and connected with the equivalent section 11 and the expansion section 13 along the length direction of the injector, the injection fluid channel 3 The expansion section 13 is in the shape of a trumpet with openings at both ends, and the equivalent section 11 is in the shape of a hollow cylinder...
Embodiment 2
[0049] as attached Figure 4-5 Shown is a closed-loop self-adaptive adjustable ejector. In this embodiment, the ejector as a whole has a two-dimensional nozzle configuration, and each component pipeline is in the shape of a hollow column, including a working unit fixedly connected to an upstream device. The fluid upstream pipeline 15, the tail of the working fluid upstream pipeline 15 extends into the injection fluid channel 3, and the injection fluid channel 3 is sequentially sealed and connected to the equivalent section 11 and the expansion section along the length direction of the injector 13. The working fluid upstream pipeline 15 is sequentially provided with a coaxial and interconnected working fluid nozzle straight section 16, a working fluid nozzle converging section 1, a working fluid nozzle throat 5 and a working fluid nozzle along the central axis. Expansion segment 9;
[0050] The middle part of the expansion section 9 of the working fluid nozzle is provided with...
Embodiment 3
[0054] On the basis of Embodiment 1 or Embodiment 2, the present invention also provides a rocket-based combined cycle engine adaptive rocket nozzle, including a closed-loop adaptive adjustment as described in any one of Embodiment 1 or Embodiment 2 ejector.
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