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Nuclear power engine device

An engine and nuclear power technology, applied in the field of nuclear power engine devices, can solve the problems of large weight and volume, limited cruising range, and radioactive pollution of the indirect cycle scheme, and achieve compact structure, high energy conversion efficiency, and reduced volume of the indirect cycle Effect

Active Publication Date: 2021-10-12
HARBIN ENG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to solve the above technical problems, to provide an efficient indirect cycle, safe, reliable, efficient and compact integrated nuclear power engine device, which can overcome the limited mileage of conventional power devices, radioactive pollution caused by direct cycle nuclear power engines, The problem of large weight and volume and insufficient compactness of the indirect circulation scheme

Method used

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Embodiment Construction

[0028] The present invention will be described in further detail below in combination with examples of embodiments and accompanying drawings.

[0029] The invention provides a compact high-efficiency indirect cycle nuclear power engine device, the specific embodiment is as follows figure 1 As shown, it includes a fixed base, a reactor system installed on the fixed base, an integrated engine, and connecting pipelines; the reactor system includes a pressure vessel 7, a reactor core, a core shroud 10, a control rod drive mechanism 6, and a reflection layer , instrumentation in the reactor, instrumentation support structure, etc., the two ends of the pressure vessel 7 are respectively provided with a reactor coolant inlet 8 and a reactor coolant outlet 12, and the reactor core includes fuel rods 9, fuel limiting devices 11, control rods 6, support structures Wait. Wherein, the reflective layer is located in an area outside the pressure vessel 7 and is used to reflect neutrons esc...

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Abstract

The invention provides a nuclear power engine device. The nuclear power engine device comprises a base, a reactor system, an integrated engine and a connecting pipeline, wherein the reactor system comprises a pressure vessel, a reactor coolant inlet, a reactor coolant outlet, a reactor core, a control rod driving mechanism and the like, and the integrated engine comprises an air inlet port, a compressor, a heat exchanger, a turbine and an exhaust port; the heat exchanger comprises a primary-side heat exchange chamber and a secondary-side heat exchange chamber which are isolated from each other; the compressor comprises a front-end coolant compression section and a rear-end air compression section; and the primary-side heat exchange chamber is connected with the reactor coolant outlet and a front-end coolant compression section inlet through connecting pipes separately, a front-end coolant compression section outlet is connected with the reactor coolant inlet through a connecting pipe, and the secondary-side heat exchange chamber is connected with a rear-end air compression section outlet and the turbine through connecting pipes. By optimally designing a front compression section structure, a rear compression section structure, a primary-side heat exchange loop and a secondary-side heat exchange loop, integrated compression and efficient heat exchange of a primary-side working medium and a secondary-side working medium are realized, and the nuclear power engine device is compact, small, safe and efficient.

Description

technical field [0001] The invention relates to the fields of nuclear reactor engineering technology and power device design, and in particular relates to a nuclear power engine device. Background technique [0002] The peaceful use of nuclear energy can be realized by artificially controlling the speed of the chain fission reaction. The fission reaction will release a large amount of heat. The reactor converts the atomic energy during fission into heat energy. The coolant carries this part of the heat and transfers it to the power plant through the energy conversion device, and finally converts it into mechanical energy, which generates thrust to drive the aircraft to fly. [0003] Traditional aircraft engines use aviation kerosene as fuel, and the aircraft is limited by the amount of fuel carried, and the flight range is generally only hundreds to thousands of kilometers. The energy density of nuclear power engines is extremely high, and a reactor with a power of hundreds...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C1/05G21D5/02
CPCF02C1/05G21D5/02Y02E30/00
Inventor 赵富龙宁可为何宇豪谭思超黄笛卢瑞博赵佳音
Owner HARBIN ENG UNIV
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