CN218955816U - Engine inlet gas uniform distribution acquisition device - Google Patents
Engine inlet gas uniform distribution acquisition device Download PDFInfo
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- CN218955816U CN218955816U CN202223476587.2U CN202223476587U CN218955816U CN 218955816 U CN218955816 U CN 218955816U CN 202223476587 U CN202223476587 U CN 202223476587U CN 218955816 U CN218955816 U CN 218955816U
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- collecting box
- engine inlet
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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Abstract
The utility model relates to an engine inlet gas uniform distribution acquisition device, and belongs to the field of aviation machinery control. The device comprises a gas sensor, a gas collecting box, a temperature sensor, a pressure sensor and an ECU; the gas sensor is arranged on the casing on the inner wall of the engine inlet, the gas sensor is connected with the gas collecting box guide pipe, and 2 paths of gas are led out of the gas collecting box and respectively supplied to the temperature sensor and the pressure sensor; the temperature sensor and the pressure sensor are connected with the ECU. The utility model ensures that the aeroengine collects the atmospheric temperature and pressure data more accurately and improves the engine control.
Description
Technical Field
The utility model relates to an engine inlet gas uniform distribution acquisition device, and belongs to the field of aviation machinery control.
Background
Because the flight envelope of the aircraft is wide, the working environment of the aircraft engine is greatly changed, and the engine needs to stably work under different air pressure and air temperature conditions. In recent years, with the development of aero-engine technology, aero-engines adopting electronic control and monitoring technology gradually replace traditional mechanically controlled aero-engines. It is often necessary to collect pressure and temperature data of the engine inlet gas for the ECU to control the engine.
At present, the method for collecting the temperature and the pressure of the inlet gas of the engine at home is to arrange probes on the inner wall of the inlet of the engine, and the probes are connected with a sensor conduit. The method can only collect one point on the circumference of the engine inlet during collection, the collected parameters are not representative, and the error is large.
Disclosure of Invention
The utility model aims to provide an engine inlet gas uniform distribution acquisition device which aims to meet the acquisition accuracy of an aeroengine on inlet atmospheric temperature and pressure. The principle is that 3 gas sensors are uniformly arranged on the inner wall of an inlet of an engine, the sensors are connected with a gas collecting box through a conduit, and temperature and pressure sensors are arranged on the gas collecting box. This makes the acquired data more accurate.
In order to achieve the above purpose, the utility model adopts the following technical scheme: the device comprises a gas sensor, a gas collecting box, a temperature sensor, a pressure sensor and an ECU;
the gas sensor is arranged on the casing on the inner wall of the engine inlet, the gas sensor is connected with the gas collecting box guide pipe, and 2 paths of gas are led out of the gas collecting box and respectively supplied to the temperature sensor and the pressure sensor;
the temperature sensor and the pressure sensor are connected with the ECU.
Further, the number of the gas sensors is 3 and the gas sensors are uniformly arranged on the inner wall casing of the engine inlet.
Further, 3 gas sensors are installed at intervals of 120 ° in pairs.
Further, the temperature sensor and the pressure sensor are electrically connected with the ECU through cables.
Further, in the engine operation, the inlet gas is introduced into the gas collecting box through 3 gas sensors respectively, and three inlet gases are uniformly mixed in the gas collecting box.
The inlet casing of the engine is uniformly provided with 3 gas sensors, and the sensors are respectively connected with one gas collecting box through a conduit, so that the inlet gas of the 3 paths of engines can be uniformly distributed in the gas collecting boxes. The gas collecting box is provided with a temperature and pressure sensor, and the measured atmospheric temperature and pressure data are transmitted to the ECU through electricity for controlling the engine.
The utility model has the beneficial effects that:
the utility model ensures that the aeroengine collects the atmospheric temperature and pressure data more accurately and improves the engine control.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
in the figure: 1-gas sensor, 2-gas collection box, 3-temperature sensor, 4-pressure sensor, 5-ECU.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
The engine inlet gas uniform distribution acquisition device comprises a gas sensor 1, a gas collection box 2, a temperature sensor 3, a pressure sensor 4 and an ECU5;
the gas sensor 1 is arranged on a casing on the inner wall of an engine inlet, the gas sensor 1 is connected with a guide pipe of the gas collecting box 2, and 2 paths of gas are led out of the gas collecting box 2 to the temperature sensor 3 and the pressure sensor 4 respectively;
the temperature sensor 3 and the pressure sensor 4 are connected to the ECU 5.
Further, the number of the gas sensors 1 is 3 and uniformly mounted on the inner wall casing of the engine inlet.
Further, 3 gas sensors 1 are installed at intervals of 120 ° in pairs.
Further, the connection between the temperature sensor 3 and the pressure sensor 4 and the ECU5 is made electrically by cables.
The specific working process is as follows: in the engine work, inlet gas is respectively introduced into the gas collecting box through 3 gas sensors, three inlet gases are uniformly mixed in the gas collecting box, the temperature sensor and the pressure sensor measure the atmospheric temperature and pressure parameters in the gas collecting box and send the parameters to the ECU, and the ECU is used for controlling the engine in real time after obtaining the temperature and pressure parameters.
In all the above mentioned solutions, in which the connection between two components can be chosen according to the actual situation, a welded, bolt-and-nut-fitted connection, a bolt-or-screw connection or other known connection means, which are not described in detail herein, where reference is made to a written fixed connection, the preferred consideration is welding, although embodiments of the utility model have been shown and described, it will be understood by those skilled in the art that numerous variations, modifications, substitutions and alterations can be made to these embodiments without departing from the principle and spirit of the utility model, the scope of which is defined by the appended claims and their equivalents.
Claims (5)
1. An engine inlet gas equipartition collection system, its characterized in that: the device comprises a gas sensor (1), a gas collecting box (2), a temperature sensor (3), a pressure sensor (4) and an ECU (5);
the gas sensor (1) is arranged on the engine inlet inner wall casing, the gas sensor (1) is connected with a gas collecting box (2) guide pipe, and 2 paths of gas are led out of the gas collecting box (2) to a temperature sensor (3) and a pressure sensor (4) respectively;
the temperature sensor (3) and the pressure sensor (4) are connected to an ECU (5).
2. The engine inlet gas uniform distribution collection device according to claim 1, wherein: the number of the gas sensors (1) is 3 and the gas sensors are uniformly arranged on the inner wall casing of the engine inlet.
3. The engine inlet gas uniform distribution collection device according to claim 2, wherein: the 3 gas sensors (1) are installed at intervals of 120 degrees.
4. The engine inlet gas uniform distribution collection device according to claim 1, wherein: the connection mode between the temperature sensor (3) and the pressure sensor (4) and the ECU (5) is electric through cables.
5. The engine inlet gas uniform distribution collection device according to claim 2, wherein: in the operation of the engine, inlet gases are respectively introduced into the gas collecting box (2) through 3 gas sensors (1), and three inlet gases are uniformly mixed in the gas collecting box (2).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202223476587.2U CN218955816U (en) | 2022-12-26 | 2022-12-26 | Engine inlet gas uniform distribution acquisition device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202223476587.2U CN218955816U (en) | 2022-12-26 | 2022-12-26 | Engine inlet gas uniform distribution acquisition device |
Publications (1)
Publication Number | Publication Date |
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CN218955816U true CN218955816U (en) | 2023-05-02 |
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Family Applications (1)
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CN202223476587.2U Active CN218955816U (en) | 2022-12-26 | 2022-12-26 | Engine inlet gas uniform distribution acquisition device |
Country Status (1)
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CN (1) | CN218955816U (en) |
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2022
- 2022-12-26 CN CN202223476587.2U patent/CN218955816U/en active Active
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