[go: up one dir, main page]

CN111706878A - Double oil circuit hedging direct injection nozzle - Google Patents

Double oil circuit hedging direct injection nozzle Download PDF

Info

Publication number
CN111706878A
CN111706878A CN202010483474.1A CN202010483474A CN111706878A CN 111706878 A CN111706878 A CN 111706878A CN 202010483474 A CN202010483474 A CN 202010483474A CN 111706878 A CN111706878 A CN 111706878A
Authority
CN
China
Prior art keywords
wall
central
oil way
injection nozzle
direct injection
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN202010483474.1A
Other languages
Chinese (zh)
Inventor
杨正超
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chuzhou Dibang Technology Co ltd
Original Assignee
Chuzhou Dibang Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chuzhou Dibang Technology Co ltd filed Critical Chuzhou Dibang Technology Co ltd
Priority to CN202010483474.1A priority Critical patent/CN111706878A/en
Publication of CN111706878A publication Critical patent/CN111706878A/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)

Abstract

本发明提供双油路对冲直射式喷嘴,涉及燃气轮机燃烧室领域,包括中心油路和外油路,外油路外壁的末端设置有扩张喷嘴,中心油路的开口位置设置有支撑架,支撑架上设置有第一转动轴承,第一转动轴承上设置有转动轴,转动轴上设置有多个搅拌杆,转动轴位于搅拌杆的一侧设置有隔绝网,扩张喷嘴的末端固定设置有出口支架,出口支架的外侧安装有驱动马达。本发明中的喷嘴具有双油路,使得燃油发生碰撞破碎,通过搅拌杆的设置,能够对燃油进行二次破碎,通过隔绝网的设置,在转动轴的带动下快速转动,对燃油进行第三次破碎,整个发明结构简单,思路情思,能够使得燃油与空气完全混合,且燃油空间分布均匀,雾化效果好,实用性高。

Figure 202010483474

The invention provides a dual-oil-path counter-injection nozzle, which relates to the field of gas turbine combustion chambers. A first rotating bearing is arranged on the first rotating bearing, a rotating shaft is arranged on the first rotating bearing, and a plurality of stirring rods are arranged on the rotating shaft. , A drive motor is installed on the outside of the outlet bracket. The nozzle in the present invention has dual oil paths, so that the fuel is collided and broken, and the fuel can be crushed twice by the setting of the stirring rod. Secondary crushing, the whole invention is simple in structure and thoughtful in thinking, which can make the fuel and air completely mix, and the fuel space is evenly distributed, the atomization effect is good, and the practicability is high.

Figure 202010483474

Description

双油路对冲直射式喷嘴Double oil circuit hedging direct injection nozzle

技术领域technical field

本发明涉及燃气轮机燃烧室领域,尤其涉及双油路对冲直射式喷嘴。The invention relates to the field of gas turbine combustion chambers, in particular to a dual-oil path counteracting direct injection nozzle.

背景技术Background technique

现代航空发动机燃烧室的基本性能和结构分布已经达到相当高的水平,但对于现代航空发动机燃烧室来说,其中仍然存在大量的难题和挑战,因此在结构设计和性能上仍然具有一定的上升空间,例如新材料、新工艺、新结构、新概念的发展应用,这些都是保证其技术持续进步的源泉。The basic performance and structural distribution of modern aero-engine combustion chambers have reached a fairly high level, but for modern aero-engine combustion chambers, there are still a lot of problems and challenges, so there is still room for improvement in structural design and performance , such as the development and application of new materials, new processes, new structures, and new concepts, which are the source of ensuring the continuous progress of its technology.

为了提高航空发动机燃烧室的性能,其内部燃油雾化效果是重要的一环,燃油雾化效果的好坏决定着燃烧室工作特性的好坏,要使燃油与空气完全混合,且燃油空间分布均匀,因此,对于燃油雾化的研究是航空发动机燃烧室研究中一个很重要的部分。In order to improve the performance of the aero-engine combustion chamber, the internal fuel atomization effect is an important part. The quality of the fuel atomization effect determines the working characteristics of the combustion chamber. It is necessary to make the fuel and air completely mix, and the fuel space distribution Therefore, the study of fuel atomization is a very important part in the study of aero-engine combustion chamber.

专利号为CN201910153702.6 双油路对冲直射式喷嘴,该喷气喷嘴整体形式为直射式喷气喷嘴,通过上游加压,将燃油输运进入喷气喷嘴,喷气喷嘴具有中心油路与外环油路两个输运油路,在喷气喷嘴直段末端与扩张段,外环油路的燃油将逆向进入中心油路,两股燃油发生碰撞破碎。该发明只是简单的通过中心油路和外环油路之间的燃油的碰撞,而使得燃油破碎,这种方式过于简单,且燃油的雾化效果不好。The patent number is CN201910153702.6 dual oil circuit hedging direct injection nozzle, the overall form of the injection nozzle is a direct injection nozzle, through upstream pressure, the fuel is transported into the injection nozzle, the injection nozzle has a central oil circuit and an outer ring oil circuit. At the end of the straight section of the jet nozzle and the expansion section, the fuel in the outer ring oil circuit will enter the central oil circuit in the reverse direction, and the two fuels will collide and be broken. The invention simply breaks the fuel through the collision of the fuel between the central oil circuit and the outer ring oil circuit. This method is too simple and the fuel atomization effect is not good.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于提供双油路对冲直射式喷嘴,以解决上述技术问题。The purpose of the present invention is to provide a dual-oil hedging direct injection nozzle to solve the above-mentioned technical problems.

本发明为解决上述技术问题,采用以下技术方案来实现:双油路对冲直射式喷嘴,包括中心油路和外油路,所述中心油路的外侧设置有中心油路外壁,所述外油路的外侧设置有外油路外壁,所述所述外油路的末端为封闭结构,且中心油路外壁靠近外油路末端位置设置有倾斜射入孔和矩形入口,所述外油路外壁的末端设置有扩张喷气喷嘴,且扩张喷气喷嘴的内侧壁与中心油路外壁紧密焊接,所述中心油路的开口位置设置有支撑架,支撑架的中心位置设置有第一转动轴承,第一转动轴承上沿着中轴线位置设置有转动轴,转动轴上沿着中轴线在同一平面内设置有多个搅拌杆,且所有搅拌杆的外侧通过固定环连接固定,所述转动轴位于搅拌杆的一侧设置有隔绝网,所述扩张喷气喷嘴的末端固定设置有出口支架,所述出口支架的内侧中心位置设置有第二转动轴承,且转动轴右端安装在第二转动轴承,所述出口支架的外侧安装有驱动马达,且驱动马达的输出端与转动轴的输入端传动连接,所述第二转动轴承和驱动马达的外侧均设置有密封罩。In order to solve the above-mentioned technical problems, the present invention adopts the following technical scheme to realize: a double-oil hedging direct injection nozzle, including a central oil passage and an outer oil passage, the outer wall of the central oil passage is arranged on the outer side of the central oil passage, and the outer oil passage is provided with an outer wall of the central oil passage. The outer wall of the outer oil circuit is provided on the outside of the road. The end of the outer oil circuit is a closed structure, and the outer wall of the central oil circuit is provided with an inclined injection hole and a rectangular inlet near the end of the outer oil circuit. The outer wall of the outer oil circuit An expansion jet nozzle is arranged at the end of the expansion jet, and the inner side wall of the expansion jet nozzle is tightly welded with the outer wall of the central oil passage. The opening position of the central oil passage is provided with a support frame, and the center position of the support frame is provided with a first rotating bearing. The rotating bearing is provided with a rotating shaft along the central axis, and a plurality of stirring rods are arranged in the same plane along the central axis on the rotating shaft, and the outer sides of all stirring rods are connected and fixed by a fixing ring, and the rotating shaft is located in the stirring rod. An isolation net is provided on one side of the nozzle, the end of the expanding jet nozzle is fixedly provided with an outlet bracket, the inner center of the outlet bracket is provided with a second rotating bearing, and the right end of the rotating shaft is installed on the second rotating bearing. A drive motor is installed on the outer side of the bracket, and the output end of the drive motor is drivingly connected with the input end of the rotating shaft, and a sealing cover is provided on the outer side of the second rotating bearing and the drive motor.

优选的,所述中心油路外壁为一个圆柱形筒体结构。Preferably, the outer wall of the central oil passage is a cylindrical cylinder structure.

优选的,所述搅拌杆共设置有八根,且沿着转动轴的轴线环形阵列分布。Preferably, there are eight stirring rods in total, and they are distributed in an annular array along the axis of the rotating shaft.

优选的,所述搅拌杆的内部设置有通气管道,所述搅拌杆的外侧壁上均匀设置有多个喷气喷嘴,喷气喷嘴上安装有单向阀,所述转动轴的内部设置有输气管,所述通气管道与输气管活动连接,且输气管上连接有气泵。Preferably, a ventilation pipe is arranged inside the stirring rod, a plurality of jet nozzles are evenly arranged on the outer side wall of the stirring rod, a one-way valve is installed on the jet nozzle, and an air delivery pipe is provided inside the rotating shaft, The ventilation pipeline is movably connected with the gas delivery pipe, and the gas delivery pipe is connected with an air pump.

优选的,所述扩张喷气喷嘴的扩张角度为8-10°。Preferably, the expanding angle of the expanding jet nozzle is 8-10°.

优选的,所述输气管与转动轴活动连接。Preferably, the gas delivery pipe is movably connected with the rotating shaft.

优选的,所述中心油路内半径为2~5mm,外油路与中心油路同心,且外油路的内壁与中心油路外壁的距离为0.5~1mm。Preferably, the inner radius of the central oil passage is 2-5 mm, the outer oil passage is concentric with the central oil passage, and the distance between the inner wall of the outer oil passage and the outer wall of the central oil passage is 0.5-1 mm.

优选的,所述扩张喷气喷嘴的内壁上朝向出口支架方向设置有倾斜挡板。Preferably, an inclined baffle is provided on the inner wall of the expanding jet nozzle toward the outlet bracket.

本发明的有益效果是:The beneficial effects of the present invention are:

本发明中的喷气喷嘴具有双油路,包括中心油路和外油路,在扩张段外环燃油逆向进入中心油路,燃油发生碰撞破碎,它能够有效改善燃油雾化效果,通过倾斜射入孔和矩形入口的设置,使得从外油路进入到中心油路的燃油与中心油路的燃油发生碰撞,通过搅拌杆的设置,能够对燃油进行二次破碎,通过隔绝网的设置,在转动轴的带动下快速转动,对燃油进行第三次破碎,使得燃油可以最大程度的雾化,明显的提高了发动机燃烧室的性能,整个发明结构简单,思路情思,能够使得燃油与空气完全混合,且燃油空间分布均匀,雾化效果好,实用性高。The jet nozzle in the present invention has dual oil circuits, including a central oil circuit and an outer oil circuit. In the expansion section, the outer ring fuel enters the central oil circuit in reverse, and the fuel is collided and broken, which can effectively improve the fuel atomization effect. The arrangement of the hole and the rectangular inlet makes the fuel entering the central oil circuit from the outer oil circuit collide with the fuel in the central oil circuit. Driven by the shaft, it rotates rapidly, and the fuel is crushed for the third time, so that the fuel can be atomized to the greatest extent, and the performance of the combustion chamber of the engine is obviously improved. And the fuel space is evenly distributed, the atomization effect is good, and the practicability is high.

附图说明Description of drawings

图1为本发明双油路对冲直射式喷嘴的立体结构示意图;Fig. 1 is the three-dimensional structure schematic diagram of the dual-oil hedging direct injection nozzle of the present invention;

图2为本发明本发明的双油路对冲直射式喷嘴中轴截面示意图;FIG. 2 is a schematic cross-sectional view of the central axis of the dual-oil hedging direct injection nozzle of the present invention;

图3为本发明隔绝网立体结构示意图;3 is a schematic diagram of the three-dimensional structure of the isolation net of the present invention;

图4为本发明搅拌杆主视示意图;4 is a schematic front view of a stirring rod of the present invention;

图5为本发明图4中A部放大示意图;Fig. 5 is the enlarged schematic diagram of part A in Fig. 4 of the present invention;

附图标记:1、中心油路;2、外油路;3、中心油路外壁;4、外油路外壁;5、倾斜射入孔;6、矩形入口;7、扩张喷气喷嘴;8、支撑架;9、第一转动轴承;10、转动轴;11、搅拌杆;12、固定环;13、隔绝网;14、出口支架;15、第二转动轴承;16、驱动马达;17、密封罩;18、通气管道;19、喷气喷嘴;20、单向阀;21、输气管;22、倾斜挡板。Reference numerals: 1. Central oil circuit; 2. Outer oil circuit; 3. Outer wall of central oil circuit; 4. Outer wall of outer oil circuit; 5. Inclined injection hole; 6. Rectangular inlet; Support frame; 9. The first rotating bearing; 10. The rotating shaft; 11. The stirring rod; 12. The fixing ring; 13. The isolation net; 14. The outlet bracket; 15. The second rotating bearing; hood; 18, ventilation pipe; 19, jet nozzle; 20, one-way valve; 21, gas pipe; 22, inclined baffle.

具体实施方式Detailed ways

为了使本发明实现的技术手段、创作特征、达成目的与功效易于明白了解,下面结合具体实施例和附图,进一步阐述本发明,但下述实施例仅仅为本发明的优选实施例,并非全部。基于实施方式中的实施例,本领域技术人员在没有做出创造性劳动的前提下所获得其它实施例,都属于本发明的保护范围。In order to make the technical means, creative features, goals and effects realized by the present invention easy to understand, the present invention will be further described below with reference to specific embodiments and accompanying drawings, but the following embodiments are only preferred embodiments of the present invention, not all of them. . Based on the examples in the implementation manner, other examples obtained by those skilled in the art without creative work shall fall within the protection scope of the present invention.

下面结合附图描述本发明的具体实施例。Specific embodiments of the present invention will be described below with reference to the accompanying drawings.

实施例1Example 1

如图1-3所示,双油路对冲直射式喷嘴,包括中心油路1和外油路2,中心油路1的外侧设置有中心油路外壁3,外油路2的外侧设置有外油路外壁4,外油路2的末端为封闭结构,且中心油路外壁3靠近外油路2末端位置设置有倾斜射入孔5和矩形入口6,外油路外壁4的末端设置有扩张喷气喷嘴7,且扩张喷气喷嘴7的内侧壁与中心油路外壁3紧密焊接,中心油路1的开口位置设置有支撑架8,支撑架8的中心位置设置有第一转动轴承9,第一转动轴承9上沿着中轴线位置设置有转动轴10,转动轴10上沿着中轴线在同一平面内设置有多个搅拌杆11,且所有搅拌杆11的外侧通过固定环12连接固定,转动轴10位于搅拌杆11的一侧设置有隔绝网13,扩张喷气喷嘴7的末端固定设置有出口支架14,出口支架14的内侧中心位置设置有第二转动轴承15,且转动轴10右端安装在第二转动轴承15,出口支架14的外侧安装有驱动马达16,且驱动马达16的输出端与转动轴10的输入端传动连接,第二转动轴承15和驱动马达16的外侧均设置有密封罩17。As shown in Figure 1-3, the dual-oil hedging direct injection nozzle includes a central oil passage 1 and an outer oil passage 2. An outer wall 3 of the central oil passage is arranged on the outer side of the central oil passage 1, and an outer wall 3 is arranged on the outer side of the outer oil passage 2. The outer wall 4 of the oil passage, the end of the outer oil passage 2 is a closed structure, and the outer wall 3 of the central oil passage is provided with an inclined injection hole 5 and a rectangular inlet 6 near the end of the outer oil passage 2, and the end of the outer wall 4 of the outer oil passage is provided with expansion. Air jet nozzle 7, and the inner side wall of expanding jet nozzle 7 is tightly welded with the outer wall 3 of the central oil passage, the opening position of the central oil passage 1 is provided with a support frame 8, and the central position of the support frame 8 is provided with a first rotating bearing 9, the first The rotating bearing 9 is provided with a rotating shaft 10 along the central axis. The rotating shaft 10 is provided with a plurality of stirring rods 11 in the same plane along the central axis, and the outer sides of all stirring rods 11 are connected and fixed by the fixing ring 12, and the rotation The shaft 10 is provided with an isolation net 13 on one side of the stirring rod 11, the end of the expansion jet nozzle 7 is fixedly provided with an outlet bracket 14, the inner center position of the outlet bracket 14 is provided with a second rotating bearing 15, and the right end of the rotating shaft 10 is installed on the The second rotating bearing 15 has a drive motor 16 installed on the outside of the outlet bracket 14, and the output end of the drive motor 16 is drivingly connected to the input end of the rotating shaft 10. The outside of the second rotating bearing 15 and the drive motor 16 is provided with a sealing cover 17.

工作原理:将燃油经过加压后在喷气喷嘴入口分为两部分进入喷气喷嘴内部,包括中心油路1和外油路2,外油路2中的燃油在由于油路封闭,会沿着倾斜射入孔5和矩形入口6斜喷入中心油路1,在燃油射入到中心油路1时,两股燃油碰撞将造成燃油的初步破碎,随后燃油进入扩张喷气喷嘴7段,驱动马达16工作,带动转动轴10快速转动,搅拌杆11对进入到扩张喷气喷嘴7中的燃油进行第二步破碎,然后燃油会经过隔绝网13,隔绝网13在转动轴10的带动下转动,对燃油进行第三步的破碎,使燃油表面波动更加剧烈,在经过出口支架14的作用,喷气喷嘴射出的燃油将很难出现液柱,而是直接破碎成小液滴,从而缩短喷射距离,使得燃油雾化,蒸发效果明显改善。Working principle: After the fuel is pressurized, it is divided into two parts at the inlet of the jet nozzle and enters the jet nozzle, including the central oil circuit 1 and the outer oil circuit 2. The fuel in the outer oil circuit 2 will be inclined along the slope due to the closed oil circuit. The injection hole 5 and the rectangular inlet 6 are injected obliquely into the central oil circuit 1. When the fuel is injected into the central oil circuit 1, the collision of the two fuels will cause the initial fragmentation of the fuel, and then the fuel enters the expansion jet nozzle 7 section, which drives the motor 16. Work, drive the rotating shaft 10 to rotate rapidly, the stirring rod 11 will crush the fuel entering the expanding jet nozzle 7 in the second step, and then the fuel will pass through the isolation net 13, and the isolation net 13 will be driven by the rotating shaft 10. The third step of crushing will make the fuel surface fluctuate more violently. After the action of the outlet bracket 14, the fuel injected by the jet nozzle will hardly appear liquid column, but will be directly broken into small droplets, thereby shortening the injection distance and making the fuel Atomization, evaporation effect is significantly improved.

实施例2Example 2

如图1-5所示,双油路对冲直射式喷嘴,包括中心油路1和外油路2,中心油路1的外侧设置有中心油路外壁3,外油路2的外侧设置有外油路外壁4,外油路2的末端为封闭结构,且中心油路外壁3靠近外油路2末端位置设置有倾斜射入孔5和矩形入口6,外油路外壁4的末端设置有扩张喷气喷嘴7,且扩张喷气喷嘴7的内侧壁与中心油路外壁3紧密焊接,中心油路1的开口位置设置有支撑架8,支撑架8的中心位置设置有第一转动轴承9,第一转动轴承9上沿着中轴线位置设置有转动轴10,转动轴10上沿着中轴线在同一平面内设置有多个搅拌杆11,且所有搅拌杆11的外侧通过固定环12连接固定,转动轴10位于搅拌杆11的一侧设置有隔绝网13,扩张喷气喷嘴7的末端固定设置有出口支架14,出口支架14的内侧中心位置设置有第二转动轴承15,且转动轴10右端安装在第二转动轴承15,出口支架14的外侧安装有驱动马达16,且驱动马达16的输出端与转动轴10的输入端传动连接,第二转动轴承15和驱动马达16的外侧均设置有密封罩17。As shown in Figure 1-5, the dual-oil hedging direct injection nozzle includes a central oil passage 1 and an outer oil passage 2. The outer wall of the central oil passage 3 is arranged on the outside of the central oil passage 1, and the outer wall of the outer oil passage 2 is arranged on the outer side. The outer wall 4 of the oil passage, the end of the outer oil passage 2 is a closed structure, and the outer wall 3 of the central oil passage is provided with an inclined injection hole 5 and a rectangular inlet 6 near the end of the outer oil passage 2, and the end of the outer wall 4 of the outer oil passage is provided with expansion. Air jet nozzle 7, and the inner side wall of expanding jet nozzle 7 is tightly welded with the outer wall 3 of the central oil passage, the opening position of the central oil passage 1 is provided with a support frame 8, and the central position of the support frame 8 is provided with a first rotating bearing 9, the first The rotating bearing 9 is provided with a rotating shaft 10 along the central axis. The rotating shaft 10 is provided with a plurality of stirring rods 11 in the same plane along the central axis, and the outer sides of all stirring rods 11 are connected and fixed by the fixing ring 12, and the rotation The shaft 10 is provided with an isolation net 13 on one side of the stirring rod 11, the end of the expansion jet nozzle 7 is fixedly provided with an outlet bracket 14, the inner center position of the outlet bracket 14 is provided with a second rotating bearing 15, and the right end of the rotating shaft 10 is installed on the The second rotating bearing 15 has a drive motor 16 installed on the outside of the outlet bracket 14, and the output end of the drive motor 16 is drivingly connected to the input end of the rotating shaft 10. The outside of the second rotating bearing 15 and the drive motor 16 is provided with a sealing cover 17.

搅拌杆11的内部设置有通气管道18,搅拌杆11的外侧壁上均匀设置有多个喷气喷嘴19,喷气喷嘴19上安装有单向阀20,转动轴10的内部设置有输气管21,通气管道18与输气管21活动连接,且输气管21上连接有气泵。The inside of the stirring rod 11 is provided with a ventilation pipe 18, the outer side wall of the stirring rod 11 is evenly provided with a plurality of jet nozzles 19, the jet nozzle 19 is provided with a one-way valve 20, and the interior of the rotating shaft 10 is provided with an air delivery pipe 21, ventilation. The pipeline 18 is movably connected with the gas delivery pipe 21 , and an air pump is connected to the gas delivery pipe 21 .

工作原理:在燃油经过第二步粉碎时,转动轴10带动搅拌杆11快速转动,从而对燃油进行破碎,同时打开气泵,气泵中的气体将会沿着输气管21到达转动轴10的内部腔体中,然后到达通气管道18的内部,最终沿着喷气喷嘴19喷出,且喷出的气流快速,对燃油直接进行冲击,使得燃油的破碎效果更佳,配合上单向阀20的设置,使得只能气流从喷气喷嘴19喷出,而燃油不可以进入到通气管道18。Working principle: When the fuel is crushed in the second step, the rotating shaft 10 drives the stirring rod 11 to rotate rapidly, thereby crushing the fuel, and at the same time, the air pump is turned on, and the gas in the air pump will reach the inner cavity of the rotating shaft 10 along the gas pipeline 21. into the body, then reach the interior of the ventilation duct 18, and finally spray along the jet nozzle 19, and the jetted air flow is fast, directly impacting the fuel, making the fuel crushing effect better, with the setting of the one-way valve 20, So that only the air flow can be ejected from the jet nozzle 19 , and the fuel cannot enter the ventilation duct 18 .

在本发明中,除非另有明确的规定和限定,第一特征在第二特征之 “上”或之“下”可以包括第一和第二特征直接接触,也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且,第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方,或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”包括第一特征在第二特征正下方和斜下方,或仅仅表示第一特征水平高度小于第二特征。In the present invention, unless otherwise expressly specified and limited, a first feature "on" or "under" a second feature may include the first and second features in direct contact, or may include the first and second features Not directly but through additional features between them. Also, the first feature being "above", "over" and "above" the second feature includes the first feature being directly above and obliquely above the second feature, or simply means that the first feature is level higher than the second feature. The first feature is "below", "below" and "below" the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature has a lower level than the second feature.

以上显示和描述了本发明的基本原理、主要特征和本发明的优点。本行业的技术人员应该了解,本发明不受上述实施例的限制,上述实施例和说明书中描述的仅为本发明的优选例,并不用来限制本发明,在不脱离本发明精神和范围的前提下,本发明还会有各种变化和改进,这些变化和改进都落入要求保护的本发明范围内。本发明要求保护范围由所附的权利要求书及其等效物界定。The foregoing has shown and described the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above-mentioned embodiments, and the above-mentioned embodiments and descriptions are only preferred examples of the present invention, and are not intended to limit the present invention, without departing from the spirit and scope of the present invention. Under the premise, the present invention will also have various changes and improvements, and these changes and improvements all fall within the scope of the claimed invention. The claimed scope of the present invention is defined by the appended claims and their equivalents.

Claims (8)

1. Two oil circuit offset direct injection formula nozzles, including central oil circuit (1) and outer oil circuit (2), its characterized in that:
a central oil way outer wall (3) is arranged on the outer side of the central oil way (1), an outer oil way outer wall (4) is arranged on the outer side of the outer oil way (2), the tail end of the outer oil way (2) is of a closed structure, an inclined injection hole (5) and a rectangular inlet (6) are arranged at the position, close to the tail end of the outer oil way (2), of the central oil way outer wall (3), an expansion nozzle (7) is arranged at the tail end of the outer oil way outer wall (4), the inner side wall of the expansion nozzle (7) is tightly welded with the central oil way outer wall (3), a support frame (8) is arranged at the opening position of the central oil way (1), a first rotating bearing (9) is arranged at the central position of the support frame (8), a rotating shaft (10) is arranged on the first rotating bearing (9) along the central axis, and a plurality of stirring rods (11, and the outside of all puddlers (11) is connected fixedly through solid fixed ring (12), one side that axis of rotation (10) is located puddler (11) is provided with isolated net (13), the fixed exit bracket (14) that is provided with in end of expansion nozzle (7), the inboard central point of exit bracket (14) puts and is provided with second rolling bearing (15), and axis of rotation (10) right-hand member installs at second rolling bearing (15), driving motor (16) are installed in the outside of exit bracket (14), and the output of driving motor (16) is connected with the input transmission of axis of rotation (10), the outside of second rolling bearing (15) and driving motor (16) all is provided with sealed cowling (17).
2. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: the outer wall (3) of the central oil way is of a cylindrical barrel structure.
3. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: eight stirring rods (11) are arranged and distributed in an annular array along the axis of the rotating shaft (10).
4. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: the utility model discloses a stirring shaft, including puddler (11), the inside of puddler (11) is provided with breather pipe (18), evenly be provided with a plurality of air injection nozzle (19) on the lateral wall of puddler (11), install check valve (20) on air injection nozzle (19), the inside of axis of rotation (10) is provided with gas-supply pipe (21), breather pipe (18) and gas-supply pipe (21) swing joint, and be connected with the air pump on gas-supply pipe (21).
5. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: the expansion angle of the expansion nozzle (7) is 8-10 degrees.
6. The dual oil path opposed jet direct injection nozzle of claim 4, wherein: the gas pipe (21) is movably connected with the rotating shaft (10).
7. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: the inner radius of the central oil way (1) is 2-5 mm, the outer oil way (2) is concentric with the central oil way (1), and the distance between the inner wall of the outer oil way (2) and the outer wall of the central oil way (1) is 0.5-1 mm.
8. The dual oil path opposed jet direct injection nozzle of claim 1, wherein: an inclined baffle (22) is arranged on the inner wall of the expansion nozzle (7) towards the outlet support (14).
CN202010483474.1A 2020-06-01 2020-06-01 Double oil circuit hedging direct injection nozzle Withdrawn CN111706878A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010483474.1A CN111706878A (en) 2020-06-01 2020-06-01 Double oil circuit hedging direct injection nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010483474.1A CN111706878A (en) 2020-06-01 2020-06-01 Double oil circuit hedging direct injection nozzle

Publications (1)

Publication Number Publication Date
CN111706878A true CN111706878A (en) 2020-09-25

Family

ID=72538502

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010483474.1A Withdrawn CN111706878A (en) 2020-06-01 2020-06-01 Double oil circuit hedging direct injection nozzle

Country Status (1)

Country Link
CN (1) CN111706878A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113513408A (en) * 2021-07-07 2021-10-19 南京航空航天大学 Combined oil supply device, combustion chamber and oil supply method

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0348500A4 (en) * 1987-12-28 1990-04-10 Sundstrand Corp Annular combustor with tangential cooling air injection.
CN1464958A (en) * 2001-07-10 2003-12-31 三菱重工业株式会社 Premixing nozzle, burner and gas turbine
CN103988023A (en) * 2012-01-05 2014-08-13 三菱日立电力系统株式会社 Burner
CN204227463U (en) * 2014-09-03 2015-03-25 北京华清燃气轮机与煤气化联合循环工程技术有限公司 Gas-turbine combustion chamber axial admission nozzle
CN208579351U (en) * 2018-06-29 2019-03-05 德阳钰鑫机械制造有限公司 A kind of aerospace fuel spray device
US20190101291A1 (en) * 2013-03-04 2019-04-04 Delavan, Inc. Air swirlers
CN109751621A (en) * 2019-01-02 2019-05-14 西北工业大学 A kind of simple nozzle that induction is broken
CN109915855A (en) * 2019-03-01 2019-06-21 西北工业大学 Double oil circuits liquidate simple nozzle
CN109915856A (en) * 2019-03-01 2019-06-21 西北工业大学 A kind of after-burner rectification supporting plate structure
CN111059574A (en) * 2019-12-31 2020-04-24 中国科学院工程热物理研究所 Swirl cup type dual-fuel air atomizing nozzle structure

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0348500A4 (en) * 1987-12-28 1990-04-10 Sundstrand Corp Annular combustor with tangential cooling air injection.
CN1464958A (en) * 2001-07-10 2003-12-31 三菱重工业株式会社 Premixing nozzle, burner and gas turbine
CN103988023A (en) * 2012-01-05 2014-08-13 三菱日立电力系统株式会社 Burner
US20190101291A1 (en) * 2013-03-04 2019-04-04 Delavan, Inc. Air swirlers
CN204227463U (en) * 2014-09-03 2015-03-25 北京华清燃气轮机与煤气化联合循环工程技术有限公司 Gas-turbine combustion chamber axial admission nozzle
CN208579351U (en) * 2018-06-29 2019-03-05 德阳钰鑫机械制造有限公司 A kind of aerospace fuel spray device
CN109751621A (en) * 2019-01-02 2019-05-14 西北工业大学 A kind of simple nozzle that induction is broken
CN109915855A (en) * 2019-03-01 2019-06-21 西北工业大学 Double oil circuits liquidate simple nozzle
CN109915856A (en) * 2019-03-01 2019-06-21 西北工业大学 A kind of after-burner rectification supporting plate structure
CN111059574A (en) * 2019-12-31 2020-04-24 中国科学院工程热物理研究所 Swirl cup type dual-fuel air atomizing nozzle structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113513408A (en) * 2021-07-07 2021-10-19 南京航空航天大学 Combined oil supply device, combustion chamber and oil supply method
CN113513408B (en) * 2021-07-07 2022-10-21 南京航空航天大学 Combined oil supply device, combustion chamber and oil supply method

Similar Documents

Publication Publication Date Title
US11548028B2 (en) Air-assisted electrostatic ultrasonic atomization nozzle and method
CN106441915B (en) A kind of exhaust apparatus of supersonic speed nozzle exhaust simulation test
CN106441916B (en) A kind of exhaust apparatus of supersonic speed nozzle exhaust simulation test
CN106150612A (en) Gas jet type adds blue combined jet device and application thereof
CN111706878A (en) Double oil circuit hedging direct injection nozzle
CN103953461B (en) A kind of mechanical valve that reduces air inlet of air-breathing pulse detonation engine back-pressure
CN102619644A (en) Structure for reducing back pressure of air-breathing type pulse detonation air inlet passage
TWM341764U (en) Air pressurization and spoiler structure for internal combustion engine
CN111997760A (en) Aircraft engine
CN116557908B (en) Variable flame stabilizer with pneumatic atomization function
CN108318252A (en) A kind of modular water injector for compressor inlet humidification experiment
CN202578944U (en) Back pressure reducing device for aspirating pulse knock air inlet channel
CN116080881B (en) Two-phase ramjet underwater propulsion system with non-condensable gas
US7464691B2 (en) Mixing element for creating a vortex motion in an inlet manifold of an internal combustion engine
CN206002320U (en) A kind of exhaust apparatus of supersonic speed nozzle aerofluxuss simulation test
CN216714841U (en) Novel fluid ejector
CN112879112A (en) Fluid reinforcing device
CN114838387A (en) Oil thrower with impact jet flow disturbing column
CN115371075A (en) Combustion nozzle capable of reducing emission through water injection
CN113058758A (en) An atomizing nozzle combining pulse excitation and bubble atomization
CN207729590U (en) turbocharged combustion engine
CN112901565B (en) A novel fluid ejector
CN223760293U (en) A ternary two-phase fire extinguishing device
CN207661766U (en) Supercharged combustion machine
CN207661765U (en) Jet-flow type burner

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication
WW01 Invention patent application withdrawn after publication

Application publication date: 20200925