CN104648674A - Low-resistance fan-aided ejecting air feeding device - Google Patents
Low-resistance fan-aided ejecting air feeding device Download PDFInfo
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- CN104648674A CN104648674A CN201310607305.4A CN201310607305A CN104648674A CN 104648674 A CN104648674 A CN 104648674A CN 201310607305 A CN201310607305 A CN 201310607305A CN 104648674 A CN104648674 A CN 104648674A
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Abstract
本发明属于航空领域,涉及一种低阻风扇辅助引射进气装置。一种低阻风扇辅助引射进气装置,还包括引射管(3)、辅助进气管(7)以及风扇(8);辅助进气管(7)通过引射管(3)与主进气管(2)和冷却管(4)相连,风扇(8)位于辅助进气管(7)通道上。本发明在辅助进气管通道上设置风扇进行辅助进气,较小或无冲压动能时,给设备提供冷却空气。同时,利用风扇气流,通过引射管实现对主进气管内气体的引射作用,提高设备冷却效率。在无需风扇工作或风扇故障时,风扇不占用主进气管路通道,不会增加主进气管路流阻。
The invention belongs to the field of aviation and relates to a low-resistance fan auxiliary ejection air intake device. A low-resistance fan auxiliary ejection air intake device, further comprising an ejection pipe (3), an auxiliary air intake pipe (7) and a fan (8); the auxiliary air intake pipe (7) passes through the ejection pipe (3) and the main air intake pipe (2) is connected to the cooling pipe (4), and the fan (8) is located on the channel of the auxiliary air intake pipe (7). In the present invention, a fan is arranged on the passage of the auxiliary air intake pipe for auxiliary air intake, and when the kinetic energy of stamping is small or there is no stamping energy, cooling air is provided to the equipment. At the same time, the fan airflow is used to realize the ejection effect on the gas in the main air intake pipe through the ejector pipe, so as to improve the cooling efficiency of the equipment. When the fan is not required to work or the fan is faulty, the fan does not occupy the channel of the main air intake pipeline and does not increase the flow resistance of the main air intake pipeline.
Description
技术领域technical field
本发明属于航空领域,涉及一种低阻风扇辅助引射进气装置。The invention belongs to the field of aviation and relates to a low-resistance fan auxiliary ejection air intake device.
背景技术Background technique
在飞机设备冷却设计中,普遍通过导入外界空气,通过管路连接至设备,对设备进行通风冷却。冷却空气的驱动力主要依靠飞机飞行时的冲压动能。当飞机静止时或低速时,由于没有了冲压动能或冲压动能很小,冷却气流量很小,无法满足设备长时间工作的散热冷却要求。在管道上加装风扇能够在无冲压动能时提供冷却气流,但是当有冲压动能时或风扇故障时,风扇又会增加了管道阻力。In the cooling design of aircraft equipment, the equipment is generally ventilated and cooled by introducing outside air and connecting it to the equipment through pipelines. The driving force of the cooling air mainly depends on the ram kinetic energy of the aircraft during flight. When the aircraft is at rest or at low speed, because there is no stamping kinetic energy or the stamping kinetic energy is very small, the cooling air flow is very small, which cannot meet the heat dissipation and cooling requirements of the long-term work of the equipment. Adding a fan to the duct can provide cooling airflow when there is no ram energy, but the fan will increase the duct resistance when there is ram energy or the fan fails.
发明内容Contents of the invention
本发明的目的是:提供一种能够利用风扇辅助引射进气,同时在风扇不工作时,又不会增加管道流阻的进气装置。The purpose of the present invention is to provide an air intake device that can use a fan to assist in introducing intake air, and at the same time, does not increase the flow resistance of the pipeline when the fan is not working.
本发明的技术方案是:一种低阻风扇辅助引射进气装置,包括冲压进气口(1)、主进气管(2)、冷却管(4)、设备(5)以及排气管(6);其中,所述冲压进气口(1)安装在外蒙皮上,并通过主进气管(2)将冷却空气导入,经过冷却管(4),为设备(5)提供冷却空气,并经排气管(6)排出,还包括引射管(3)、辅助进气管(7)以及风扇(8);辅助进气管(7)通过引射管(3)与主进气管(2)和冷却管(4)相连,风扇(8)位于辅助进气管(7)通道上。The technical solution of the present invention is: a low-resistance fan-assisted injection air intake device, including a ram air intake (1), a main air intake pipe (2), a cooling pipe (4), a device (5) and an exhaust pipe ( 6); wherein, the ram air intake (1) is installed on the outer skin, and the cooling air is introduced through the main air intake pipe (2), passes through the cooling pipe (4), provides cooling air for the equipment (5), and Exhausted through the exhaust pipe (6), it also includes the ejector pipe (3), the auxiliary air inlet pipe (7) and the fan (8); the auxiliary air inlet pipe (7) passes through the ejector pipe (3) and the main air inlet pipe (2) It is connected with the cooling pipe (4), and the fan (8) is located on the channel of the auxiliary air intake pipe (7).
引射管(3)为环形出口构型,并与主进气管(2)同轴。The ejector pipe (3) has an annular outlet configuration and is coaxial with the main inlet pipe (2).
当飞机速度较高时,依靠冲压动能进入冲压进气口(1)的气流量能够满足设备(5)冷却要求时,风扇(8)不工作。当冲压空气不能满足流量要求时,风扇(8)工作,通过辅助进气管(7)给设备提供冷却空气,同时,辅助进气管(7)气流经过引射管(3)起到引射作用,驱动主进气管(2)气流进入冷却管(4),为设备(5)提供冷却气流。When the speed of the aircraft is high, the fan (8) does not work when the airflow entering the ram air inlet (1) by means of ram kinetic energy can meet the cooling requirements of the equipment (5). When the ram air cannot meet the flow requirements, the fan (8) works to provide cooling air to the equipment through the auxiliary air intake pipe (7), and at the same time, the airflow of the auxiliary air intake pipe (7) passes through the ejector pipe (3) to play the role of ejection, Drive the airflow from the main air intake pipe (2) into the cooling pipe (4) to provide cooling airflow to the equipment (5).
本发明具有的优点和有益效果:本发明在辅助进气管通道上设置风扇进行辅助进气,较小或无冲压动能时,给设备提供冷却空气。同时,利用风扇气流,通过引射管实现对主进气管内气体的引射作用,提高设备冷却效率。在无需风扇工作或风扇故障时,风扇不占用主进气管路通道,不会增加主进气管路流阻。The present invention has the advantages and beneficial effects: the present invention sets a fan on the passage of the auxiliary air intake pipe for auxiliary air intake, and provides cooling air to the equipment when there is little or no punching kinetic energy. At the same time, the fan airflow is used to realize the ejection effect on the gas in the main air intake pipe through the ejector pipe, so as to improve the cooling efficiency of the equipment. When the fan is not required to work or the fan is faulty, the fan does not occupy the channel of the main air intake pipeline and does not increase the flow resistance of the main air intake pipeline.
附图说明Description of drawings
图1是本发明低阻风扇辅助引射进气装置的结构示意图,Fig. 1 is a schematic structural view of a low-resistance fan-assisted injection air intake device of the present invention,
其中,1-冲压进气口、2-主进气管、3-引射管、4-冷却管、5-设备、6-排气管、7-辅助进气管、8-风扇。Among them, 1-ram air intake, 2-main air intake pipe, 3-extraction pipe, 4-cooling pipe, 5-equipment, 6-exhaust pipe, 7-auxiliary air intake pipe, 8-fan.
具体实施方式Detailed ways
下面结合附图和实施例对本发明作进一步说明:Below in conjunction with accompanying drawing and embodiment the present invention will be further described:
请参阅图1,其是本发明低阻风扇辅助引射进气装置的结构示意图。Please refer to FIG. 1 , which is a schematic diagram of the structure of the low-resistance fan-assisted introduction air intake device of the present invention.
所述低阻风扇辅助引射进气装置,其包括冲压进气口(1)、主进气管(2)、引射管(3)、冷却管(4)、设备(5)、排气管(6)、辅助进气管(7)、风扇(8)。其中,所述冲压进气口(1)位于外蒙皮上,从外界摄取空气进入主进气管(2),经冷却管(4),提供给设备(5)冷却用。所述辅助进气管(7)通过引射管(3)与主进气管(2)、冷却管(4)连接。风扇(8)位于辅助进气管(7)通道上。The low-resistance fan auxiliary injection air intake device includes a ram air inlet (1), a main air intake pipe (2), an injection pipe (3), a cooling pipe (4), equipment (5), and an exhaust pipe (6), auxiliary air intake pipe (7), fan (8). Wherein, the ram air intake (1) is located on the outer skin, and the air taken from the outside enters the main air intake pipe (2), and is supplied to the equipment (5) for cooling through the cooling pipe (4). The auxiliary air intake pipe (7) is connected with the main air intake pipe (2) and the cooling pipe (4) through the ejector pipe (3). The fan (8) is located on the passage of the auxiliary air intake pipe (7).
实施时,风扇的工作可由飞机管理计算机或发动机控制器根据设备温度进行控制,也可以由设备自身进行单独控制。当飞机速度较高时,依靠冲压动能进入冲压进气口的气流量能够满足设备冷却要求时,风扇不工作。当冲压空气不能满足流量要求时,风扇工作,通过辅助进气管给设备提供冷却空气。同时,辅助进气管气流经过引射管起到引射作用,驱动主进气管气流进入冷却管,为设备提供冷却气流。本发明利用风扇辅助进气冷却设备,同时形成引射,驱动主进气管进气,提高冷却效果。当风扇不工作时,风扇不占用主冷却管通道,不增加主进气管道流阻。During implementation, the work of the fan can be controlled by the aircraft management computer or the engine controller according to the temperature of the equipment, and can also be controlled independently by the equipment itself. When the speed of the aircraft is high, the fan does not work when the air flow entering the ram air intake by the ram kinetic energy can meet the cooling requirements of the equipment. When the ram air cannot meet the flow requirements, the fan works to provide cooling air to the equipment through the auxiliary intake pipe. At the same time, the airflow of the auxiliary intake pipe passes through the ejector pipe to play an ejection role, driving the airflow of the main intake pipe into the cooling pipe to provide cooling airflow for the equipment. The invention utilizes the fan to assist the air intake cooling equipment, and at the same time forms ejection to drive the main air intake pipe to intake air, thereby improving the cooling effect. When the fan is not working, the fan does not occupy the channel of the main cooling pipe and does not increase the flow resistance of the main air intake pipe.
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106892120A (en) * | 2015-12-21 | 2017-06-27 | 中国航空工业集团公司西安飞机设计研究所 | A kind of fan exhaust induces the ram-air ring cold integral system of control liquid |
CN107339266A (en) * | 2017-08-19 | 2017-11-10 | 哈尔滨点航科技发展有限公司 | The pressure method of self-pressurized type jet pump |
CN108263622A (en) * | 2017-12-27 | 2018-07-10 | 彩虹无人机科技有限公司 | A kind of dopey active cooling device |
CN108266273A (en) * | 2018-03-07 | 2018-07-10 | 天津曙光天成科技有限公司 | A kind of engine heat dissipating device and unmanned plane |
CN108408036A (en) * | 2018-03-07 | 2018-08-17 | 天津曙光天成科技有限公司 | A kind of multi-rotor unmanned aerial vehicle |
CN111831085A (en) * | 2019-04-23 | 2020-10-27 | 广达电脑股份有限公司 | Bleed air systems and remote air bleed devices |
EP4470922A3 (en) * | 2016-10-18 | 2025-02-19 | Wisk Aero LLC | Ventilated rotor mounting boom for personal aircraft |
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GB1436697A (en) * | 1972-02-07 | 1976-05-19 | Hawker Siddeley Dynamics Ltd | Flow-inducing ejectors in fluid flow ducts |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106892120A (en) * | 2015-12-21 | 2017-06-27 | 中国航空工业集团公司西安飞机设计研究所 | A kind of fan exhaust induces the ram-air ring cold integral system of control liquid |
EP4470922A3 (en) * | 2016-10-18 | 2025-02-19 | Wisk Aero LLC | Ventilated rotor mounting boom for personal aircraft |
CN107339266A (en) * | 2017-08-19 | 2017-11-10 | 哈尔滨点航科技发展有限公司 | The pressure method of self-pressurized type jet pump |
CN107339266B (en) * | 2017-08-19 | 2020-04-07 | 哈尔滨点航科技发展有限公司 | Pressurizing method of self-pressurizing type injection pump |
CN108263622A (en) * | 2017-12-27 | 2018-07-10 | 彩虹无人机科技有限公司 | A kind of dopey active cooling device |
CN108266273A (en) * | 2018-03-07 | 2018-07-10 | 天津曙光天成科技有限公司 | A kind of engine heat dissipating device and unmanned plane |
CN108408036A (en) * | 2018-03-07 | 2018-08-17 | 天津曙光天成科技有限公司 | A kind of multi-rotor unmanned aerial vehicle |
CN108266273B (en) * | 2018-03-07 | 2024-11-26 | 天津凤凰智能科技有限公司 | Engine cooling device and unmanned aerial vehicle |
CN111831085A (en) * | 2019-04-23 | 2020-10-27 | 广达电脑股份有限公司 | Bleed air systems and remote air bleed devices |
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