CN112229635A - Test system for testing plateau and high-altitude performance of fuel cell engine - Google Patents
Test system for testing plateau and high-altitude performance of fuel cell engine Download PDFInfo
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- CN112229635A CN112229635A CN202011178698.8A CN202011178698A CN112229635A CN 112229635 A CN112229635 A CN 112229635A CN 202011178698 A CN202011178698 A CN 202011178698A CN 112229635 A CN112229635 A CN 112229635A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/02—Details or accessories of testing apparatus
Abstract
The invention discloses a test system for testing the plateau and high altitude performance of a fuel cell engine. The plateau environment simulation test cabin is respectively connected with a low-pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system and an air supply system; the low-pressure simulation and control system reduces the atmospheric pressure in the whole plateau environment cabin in a vacuum pumping mode, the low-temperature simulation in the temperature simulation and control system is realized in a refrigerating mode, the high-temperature simulation is realized in an electric heating mode, the humidity simulation and control system simulates plateau and high-altitude humidity environments in a humidifying and dehumidifying mode, a fuel cell engine dynamometer bench is installed in a plateau environment simulation test cabin, and a fuel cell engine, a DC/DC converter, a motor and a dynamometer are sequentially installed on the fuel cell engine dynamometer bench. The invention can evaluate the adaptability of the fuel cell engine to altitude plateaus and high altitudes with the performance of 0-6000 m, and provides support for the research of key technologies of the fuel cell engine and the establishment of relevant standards.
Description
Technical Field
The invention relates to the field of fuel cell engines, in particular to a test system for testing the plateau and high altitude performance of a fuel cell engine.
Background
The fuel cell engine has the characteristics of zero noise, zero emission, low noise, weak infrared radiation and the like, and can be applied to special equipment such as unmanned aerial vehicles, vehicles and the like. At present, the commercial utilization of domestic fuel cell technology has already been provided with a certain scale, and the application research of fuel cells on military equipment has also been started. With the complication of military equipment, the multidimensional operation space and the diversification of battlefield environment, the method has to put forward higher requirements on the battlefield environment adaptability of the new fuel cell, so that the research on the battlefield environment adaptability of the fuel cell is very necessary. Since the test is an important means for verifying whether the fuel cell reaches a predetermined target at each stage of demonstration, development, sizing, production, and equipment armies.
Although commercial utilization of domestic fuel cell technology has been on a certain scale, few domestic researchers have conducted research on changes in performance and durability and countermeasures of vehicular hydrogen fuel cells in high-altitude environments (low oxygen concentration, low temperature, etc.). Therefore, the invention establishes a plateau and high altitude simulation test system of the fuel cell engine and establishes a corresponding test method, which has important significance for improving the plateau adaptability of the fuel cell engine.
Disclosure of Invention
The invention aims to solve the technical problem of providing a test system for testing the plateau and high-altitude performance of a fuel cell engine aiming at the plateau battlefield environment.
The invention relates to a test system for testing the plateau and high altitude performance of a fuel cell engine, which consists of a plateau environment simulation test cabin, a low air pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system, an air supply system and a fuel cell engine dynamometer rack; the plateau environment simulation test cabin is respectively connected with a low-pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system and an air supply system; the plateau and high altitude environment simulation cabin is a closed space capable of bearing plateau low air pressure, high and low temperature and humidity environments, the low air pressure simulation and control system reduces the atmospheric pressure in the whole plateau environment cabin in a vacuum pumping mode, the low temperature simulation in the temperature simulation and control system is realized in a refrigerating mode, the high temperature simulation is realized in an electric heating mode, the humidity simulation and control system mainly simulates the plateau and high altitude humidity environments in a humidifying and dehumidifying mode, a fuel cell engine dynamometer bench is installed in the plateau environment simulation test cabin, and a fuel cell engine, a DC/DC converter, a motor and a dynamometer are sequentially installed on the fuel cell engine dynamometer bench.
The plateau and high altitude environment simulation cabin bears atmospheric pressure: 101-47 kPa; temperature: -45 ℃ to +70 ℃; humidity: 15% -95% of closed space
Compared with the prior art, the invention has the beneficial effects that:
at present, fuel cell engine performance test research is mostly concentrated in plain areas, for example, GB/T2454-2009 "fuel cell engine performance test method" only stipulates test methods such as fuel cell engine starting characteristics, steady-state characteristics, dynamic response characteristics, airtightness detection, insulation resistance detection and the like under plain normal temperature conditions. And the influence of the extreme low-temperature and low-pressure environment on the performance of the fuel cell engine is less researched.
A fuel cell is a device that directly converts chemical energy of hydrogen and oxygen into electrical energy through an electrochemical reaction. Air is an oxidant of the electrochemical reaction of the fuel cell, and in order to ensure the continuous operation of the electrochemical reaction in the stack, air with certain pressure and flow and good filtration must be continuously supplied to the stack. And the atmospheric pressure and the temperature in the plateau area are low, and the energy conversion efficiency of the fuel cell engine is directly influenced, so that the research significance of developing the influence of the extreme low-temperature and low-pressure environment on the performance of the fuel cell engine is important.
The invention provides a plateau and high altitude performance simulation test system of a fuel cell engine, aiming at checking and evaluating the plateau (high altitude) environment adaptability of a fuel cell. The method can be used for carrying out simulation test on the performance of the fuel cell engine under the atmospheric environmental condition (atmospheric pressure: 101-47 kPa; temperature: minus 45-70 ℃ and humidity: 15-95%) with the altitude of 0-6000 m, evaluating the adaptability of the fuel cell engine to the altitude of 0-6000 m and high altitude, and providing support for key technical research of the fuel cell engine and establishment of related standards.
Drawings
Fig. 1 is a schematic block diagram of the structure of the present invention.
Detailed Description
The invention is described in further detail below with reference to the figures and specific examples. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The fuel cell engine plateau and altitude performance test system of the present invention is shown in fig. 1. The test system for testing the plateau and high altitude performance of the fuel cell engine consists of a plateau environment simulation test cabin, a low air pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system, an air supply system and a fuel cell engine dynamometer rack; the plateau environment simulation test cabin is respectively connected with a low-pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system and an air supply system; the plateau and high altitude environment simulation cabin is a closed space capable of bearing plateau low air pressure, high and low temperature and humidity environments, the low air pressure simulation and control system reduces the atmospheric pressure in the whole plateau environment cabin in a vacuum pumping mode, the low temperature simulation in the temperature simulation and control system is realized in a refrigerating mode, the high temperature simulation is realized in an electric heating mode, the humidity simulation and control system mainly simulates the plateau and high altitude humidity environments in a humidifying and dehumidifying mode, a fuel cell engine dynamometer bench is installed in the plateau environment simulation test cabin, and a fuel cell engine, a DC/DC converter, a motor and a dynamometer are sequentially installed on the fuel cell engine dynamometer bench.
The system can reproduce the atmospheric environmental conditions (atmospheric pressure: 101-47 kPa, temperature: 45-70 ℃ below zero and humidity: 15-95%) of 0-6000 m of altitude in plain areas, and can test, calibrate, evaluate and research the plateau and high altitude performance of the fuel cell under the environmental conditions of 0-6000 m of altitude, and establish related test methods and technical standards.
The plateau and high altitude performance simulation test system for the fuel cell mainly comprises a plateau environment simulation test chamber, a low air pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system, an air supply system and a power measuring rack of a fuel cell engine.
1) Plateau and high altitude environment simulation cabin
The plateau and high altitude environment simulation cabin is a closed space capable of bearing plateau low-pressure, high-low temperature and humidity environments, and can bear low-pressure of 6000m (47kPa) of altitude, and the environmental temperature and humidity changes of the plateau of-45 ℃ to +70 ℃ and 15-95%.
2) Low-pressure simulation and control system
The low-pressure simulation and control system reduces the atmospheric pressure in the whole plateau environment cabin in a vacuum pumping mode, and realizes the simulation and control of the plateau low-pressure environment.
3) Temperature simulation and control system
The temperature simulation and control system simulates the plateau, high altitude and low temperature environment in the plateau and high altitude environment simulation test cabin through the temperature environment simulation technology. The low temperature simulation is realized by a refrigeration mode, and the high temperature simulation is realized by an electric heating mode.
4) Humidity simulation system
The humidity simulation and control system mainly simulates plateau and high altitude humidity environments in a plateau environment simulation test cabin in a humidifying and dehumidifying mode through a humidity environment simulation technology.
5) Air supply system
The air supply system supplies fresh air to the plateau environment simulation cabin in real time, and the air requirement of the fuel cell is guaranteed.
6) Power measuring rack of fuel cell engine
The fuel cell engine power testing bench simulates real working conditions by using a power testing machine as a loading device and provides loads for the fuel cell engine according to test standards. In the working process of the engine, the output voltage is reduced along with the increase of the output power, the DC/DC converter keeps the bus voltage within a certain range, the driver controls the alternating current motor to operate at the moment, the output shaft of the alternating current motor transmits the mechanical power to the dynamometer, the power analyzer is used for measuring the output current voltage, and the output power is calculated.
Claims (2)
1. A test system for testing the plateau and high altitude performance of a fuel cell engine is characterized by consisting of a plateau environment simulation test cabin, a low air pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system, an air supply system and a fuel cell engine power measuring rack; the plateau environment simulation test cabin is respectively connected with a low-pressure simulation and control system, a temperature simulation and control system, a humidity simulation and control system and an air supply system; the low-pressure simulation and control system reduces the atmospheric pressure in the whole plateau environment cabin in a vacuum pumping mode, the low-temperature simulation in the temperature simulation and control system is realized in a refrigerating mode, the high-temperature simulation is realized in an electric heating mode, the humidity simulation and control system simulates plateau and high-altitude humidity environments in a humidifying and dehumidifying mode, a fuel cell engine dynamometer bench is installed in a plateau environment simulation test cabin, and a fuel cell engine, a DC/DC converter, a motor and a dynamometer are sequentially installed on the fuel cell engine dynamometer bench.
2. The testing system for testing the plateau and high altitude performance of a fuel cell engine as claimed in claim 1, wherein said plateau and high altitude environmental simulation chamber is subjected to atmospheric pressure: 101-47 kPa; temperature: -45 ℃ to +70 ℃; humidity: 15-95% of the sealed space.
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| CN202011178698.8A CN112229635A (en) | 2020-10-29 | 2020-10-29 | Test system for testing plateau and high-altitude performance of fuel cell engine |
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| CN202011178698.8A CN112229635A (en) | 2020-10-29 | 2020-10-29 | Test system for testing plateau and high-altitude performance of fuel cell engine |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113237665A (en) * | 2021-04-29 | 2021-08-10 | 中国人民解放军陆军军事交通学院 | Plateau low-temperature starting test device and method for cabin type diesel engine |
| CN113299956A (en) * | 2021-04-28 | 2021-08-24 | 一汽解放汽车有限公司 | Fuel cell engine test system |
| CN113359055A (en) * | 2021-04-23 | 2021-09-07 | 中国消防救援学院 | Environmental adaptability testing and operating method for multi-energy emergency power supply system |
| CN114112403A (en) * | 2021-10-12 | 2022-03-01 | 中国北方车辆研究所 | High-altitude simulation test device and method for performance of power pack of unmanned vehicle |
| CN115060521A (en) * | 2022-06-28 | 2022-09-16 | 北京航天试验技术研究所 | High-humidity environment simulation device and method for torch test |
| CN115754744A (en) * | 2022-11-28 | 2023-03-07 | 广州擎天实业有限公司 | Environment simulation system of fuel cell and control method thereof |
-
2020
- 2020-10-29 CN CN202011178698.8A patent/CN112229635A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113359055A (en) * | 2021-04-23 | 2021-09-07 | 中国消防救援学院 | Environmental adaptability testing and operating method for multi-energy emergency power supply system |
| CN113299956A (en) * | 2021-04-28 | 2021-08-24 | 一汽解放汽车有限公司 | Fuel cell engine test system |
| CN113237665A (en) * | 2021-04-29 | 2021-08-10 | 中国人民解放军陆军军事交通学院 | Plateau low-temperature starting test device and method for cabin type diesel engine |
| CN114112403A (en) * | 2021-10-12 | 2022-03-01 | 中国北方车辆研究所 | High-altitude simulation test device and method for performance of power pack of unmanned vehicle |
| CN114112403B (en) * | 2021-10-12 | 2024-04-05 | 中国北方车辆研究所 | Unmanned vehicle power pack performance high-altitude simulation test device and method |
| CN115060521A (en) * | 2022-06-28 | 2022-09-16 | 北京航天试验技术研究所 | High-humidity environment simulation device and method for torch test |
| CN115754744A (en) * | 2022-11-28 | 2023-03-07 | 广州擎天实业有限公司 | Environment simulation system of fuel cell and control method thereof |
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