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CN204988692U - Experimental clamping device of using of nozzle air mass flow - Google Patents

Experimental clamping device of using of nozzle air mass flow Download PDF

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Publication number
CN204988692U
CN204988692U CN201520361805.9U CN201520361805U CN204988692U CN 204988692 U CN204988692 U CN 204988692U CN 201520361805 U CN201520361805 U CN 201520361805U CN 204988692 U CN204988692 U CN 204988692U
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China
Prior art keywords
nozzle
cavity
clamping body
flow
air
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吴建华
伍文锋
刘尚明
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CHENGDU HANGLI AVIATION TECHNOLOGY Co Ltd
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CHENGDU HANGLI AVIATION TECHNOLOGY Co Ltd
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Abstract

The utility model discloses an experimental clamping device of using of nozzle air mass flow, including the clamping body, there be a plurality of the setting side by side and its axis honeycomb ducts parallel with the clamping body at the mid -mounting of cavity, it has a plurality of minutes discharge orifices to open at the upper wall of clamping body, and gas box upper end is through air inlet and outside intercommunication, and gas box lower extreme is through dividing discharge orifice and cavity intercommunication, and the nozzle runs through the local of the clamping body other end and nozzle and the cavity feeds through. A plurality of honeycomb ducts that compressed air passes through the cavity middle part form the air current that the stranded is relatively stable and the velocity of flow is not of uniform size, and stranded air current direct impact to the intercommunication part of nozzle with the cavity, make the nozzle be in the air current environment in emulation stage, convenient fluid flow to the nozzle, the atomizing tapering, detection record is carried out in state distribution etc, shorten nozzle recycle adjust the time in the experimental -> design of design -> product manufacture -> finished product testing, reduce the difference between emulation and the actual production manufacturing.

Description

一种喷嘴空气流量试验用装夹装置A clamping device for nozzle air flow test

技术领域 technical field

本实用新型涉及一种航空、航天等特殊行业中燃油喷嘴的夹持装置,具体是指一种喷嘴空气流量试验用装夹装置。 The utility model relates to a clamping device for fuel nozzles in special industries such as aviation and aerospace, in particular to a clamping device for nozzle air flow tests.

背景技术 Background technique

我国对航空、航天用的发动机空气雾化燃油喷嘴各项性能参数(油液流量、雾化锥角、状态分布、SMD等)都有检测,但在测雾化特性及空气流量检测方面多数仅仅停留在仿制设计及仿真阶段,输入的各项测试参数都是理想状态下的理论值。在实际的产品研制阶段,需花费巨大成本在图纸设计→产品制造→成品检测试验→图纸设计中反复循环去调整、缩减理论设计、仿真和实际生产制造之间的差异,严重的差异会降低喷嘴产品的使用要求,甚至影响到飞行安全。 my country has tested various performance parameters (oil flow, atomization cone angle, state distribution, SMD, etc.) Staying at the stage of imitation design and simulation, the input test parameters are all theoretical values under ideal conditions. In the actual product development stage, it takes a huge cost to adjust and reduce the difference between theoretical design, simulation and actual production and manufacturing repeatedly in the drawing design→product manufacturing→finished product inspection test→drawing design. Serious differences will reduce the nozzle The use requirements of the product even affect flight safety.

实用新型内容 Utility model content

本实用新型的目的在于提供一种喷嘴空气流量试验用装夹装置,缩减设计仿真和成品检测之间的差异,从而缩短产品设计和定型之间的时间,进而达到降低研制成本的目的。 The purpose of this utility model is to provide a clamping device for nozzle air flow test, which can reduce the difference between design simulation and finished product inspection, thereby shortening the time between product design and finalization, and further reducing the development cost.

本实用新型的目的通过下述技术方案实现: The purpose of this utility model is achieved through the following technical solutions:

一种喷嘴空气流量试验用装夹装置,包括内部开设空腔的装夹本体,在所述空腔的中部安装有多个并排设置且其轴线与装夹本体平行的导流管,在所述装夹本体一端上安装有气盒,在装夹本体的上壁开有多个分流孔,所述气盒上端通过进气口与外部连通,气盒下端通过分流孔与空腔连通,喷嘴贯穿所述装夹本体另一端且喷嘴的局部与空腔连通,喷嘴通过密封件、密封环实现在装夹本体上的密封。本实用新型使用时,通过密封件以及密封环将喷嘴固定密封在空腔的端部,向进气口内注入压缩空气,使得压缩空气在气盒内汇聚后通过多个分流孔进行初步的分流直至进入到空腔内,此时压缩空气通过空腔中部的多个导流管形成多股相对稳定且流速大小不一的气流,且多股气流直接冲击至喷嘴与空腔的连通部分,使得喷嘴处于仿真阶段的气流环境,方便对喷嘴的油液流量、雾化锥度、状态分布等进行检测记录,缩短喷嘴在图纸设计→产品制造→成品检测试验→图纸设计中反复循环调整时间,降低仿真与实际生产制造之间的差异;并且压缩空气的流量以及流速可根据实际检测的需要进行及时调节,通过分流孔以及导流管的逐级稳定分流,使得仿真阶段的气流状态更加接近与实际值,提高喷嘴空气流量检测数据的精确度。 A clamping device for a nozzle air flow test, comprising a clamping body with a cavity inside, and a plurality of flow guide tubes arranged side by side and whose axis is parallel to the clamping body are installed in the middle of the cavity. An air box is installed on one end of the clamping body, and a plurality of diversion holes are opened on the upper wall of the clamping body. The upper end of the air box communicates with the outside through the air inlet, and the lower end of the air box communicates with the cavity through the diversion holes, and the nozzle runs through The other end of the clamping body and part of the nozzle communicate with the cavity, and the nozzle is sealed on the clamping body through a seal and a sealing ring. When the utility model is in use, the nozzle is fixed and sealed at the end of the cavity through the sealing member and the sealing ring, and compressed air is injected into the air inlet, so that the compressed air is initially diverted through a plurality of diverter holes in the air box until the Entering the cavity, at this time, the compressed air passes through multiple guide tubes in the middle of the cavity to form multiple relatively stable airflows with different flow velocities, and the multiple airflows directly impact the connecting part between the nozzle and the cavity, so that the nozzle The airflow environment in the simulation stage facilitates the detection and recording of the nozzle’s oil flow, atomization taper, and state distribution, shortens the nozzle’s repeated cycle adjustment time in the drawing design→product manufacturing→finished product inspection test→drawing design, and reduces the simulation and The difference between actual production and manufacturing; and the flow rate and flow rate of compressed air can be adjusted in time according to the needs of actual detection, and the flow state is closer to the actual value in the simulation stage through the step-by-step stable flow distribution of the distribution hole and the draft tube. Improve the accuracy of nozzle air flow detection data.

还包括固定在所述装夹本体上壁且与空腔连通的测压件,所述测压件与喷嘴的中心距为5~15㎜。测压件与喷嘴和导流管之间的空腔区域连通,即实时检测最终的稳定的仿真气流压力值,方便工作人员根据实际情况及时调整压缩空气的流量以及流速,提高喷嘴检测性能参数的多样性,使得产品仿真设计更加接近于合格成品的参数数值,大幅度降低喷嘴的研制成本。 It also includes a pressure measuring piece fixed on the upper wall of the clamping body and communicated with the cavity. The center distance between the pressure measuring piece and the nozzle is 5-15mm. The pressure measuring part is connected with the cavity area between the nozzle and the nozzle, that is, real-time detection of the final and stable simulated airflow pressure value, which is convenient for the staff to adjust the flow rate and flow rate of the compressed air in time according to the actual situation, and improve the accuracy of the nozzle detection performance parameters. Diversity makes the product simulation design closer to the parameter values of qualified finished products, greatly reducing the development cost of nozzles.

所述分流孔的孔径为导流管孔径的1/4。压缩空气通过进气口注入到气盒中,通过分流孔的泄压,使得气流以一个更快的流速喷射入空腔内,最终通过空腔端部空间的缓冲并且在导流管的导向作用下,形成多股的稳定气流向喷嘴移动,而分流孔的孔径为导流孔孔径的1/4,使得压缩空气通过气盒、分流孔、靠近空腔端部的区域以及导流管实现多次换向和变速,与直射喷流相比,本实用新型中气流状态变化更加复杂,更加贴近于喷嘴所处的实际环境条件,并且通过多次换向和变速,由导流管中喷出气流所产生的絮流与通过Fluent软件模拟确认紊流相比消减78%以上,保证了喷嘴良好的测试环境。 The diameter of the distribution hole is 1/4 of the diameter of the draft tube. Compressed air is injected into the air box through the air inlet, and through the pressure relief of the split hole, the air flow is injected into the cavity at a faster flow rate, and finally passes through the buffer of the end space of the cavity and guides the guide tube Under this condition, multiple streams of stable air flow are formed to move towards the nozzle, and the aperture of the diversion hole is 1/4 of the diameter of the diversion hole, so that the compressed air passes through the air box, the diversion hole, the area near the end of the cavity and the diversion tube to achieve multiple Compared with the direct jet flow, the change of the airflow state in the utility model is more complicated, and it is closer to the actual environmental conditions where the nozzle is located, and through multiple changes of direction and speed, it is sprayed from the guide tube The flocculation generated by the airflow is reduced by more than 78% compared with the turbulence confirmed by the Fluent software simulation, ensuring a good test environment for the nozzle.

多个所述分流孔均匀分布在所述气盒的底部,且多个所述分流孔的总分布面积为所述气盒的底部面积的1/10~1/5。作为优选,多个分流孔的均匀分布以及其总分布面积的特殊设置,进一步减小在导流管内的气流产生的絮流量,提高仿真环境下喷嘴检测参数的准确性和全面性。 The multiple distribution holes are evenly distributed on the bottom of the air box, and the total distribution area of the multiple distribution holes is 1/10-1/5 of the bottom area of the air box. Preferably, the uniform distribution of the plurality of distribution holes and the special setting of the total distribution area further reduce the floc flow generated by the air flow in the draft tube, and improve the accuracy and comprehensiveness of the nozzle detection parameters in the simulation environment.

本实用新型与现有技术相比,具有如下的优点和有益效果: Compared with the prior art, the utility model has the following advantages and beneficial effects:

1、本实用新型中压缩空气通过空腔中部的多个导流管形成多股相对稳定且流速大小不一的气流,且多股气流直接冲击至喷嘴与空腔的连通部分,使得喷嘴处于仿真阶段的气流环境,方便对喷嘴的油液流量、雾化锥度、状态分布等进行检测记录,缩短喷嘴在图纸设计→产品制造→成品检测试验→图纸设计中反复循环调整时间,降低仿真与实际生产制造之间的差异;并且压缩空气的流量以及流速可根据实际检测的需要进行及时调节,通过分流孔以及导流管的逐级稳定分流,使得仿真阶段的气流状态更加接近与实际值,提高喷嘴空气流量检测数据的精确度; 1. In the utility model, the compressed air passes through multiple guide tubes in the middle of the cavity to form a plurality of relatively stable airflows with different flow velocities, and the multiple airflows directly impact the connecting part between the nozzle and the cavity, so that the nozzle is in a simulated state. The airflow environment in each stage facilitates the detection and recording of the oil flow rate, atomization taper, and state distribution of the nozzle, shortens the time for repeated cycle adjustment of the nozzle in drawing design→product manufacturing→finished product inspection test→drawing design, and reduces simulation and actual production. The difference between manufacturing; and the flow rate and flow rate of compressed air can be adjusted in time according to the actual detection needs, through the step-by-step stable diversion of the diversion hole and the guide tube, the airflow state in the simulation stage is closer to the actual value, and the nozzle can be improved. The accuracy of air flow detection data;

2、本实用新型的测压件与喷嘴和导流管之间的空腔区域连通,即实时检测最终的稳定的仿真气流压力值,方便工作人员根据实际情况及时调整压缩空气的流量以及流速,提高喷嘴检测性能参数的多样性,使得产品仿真设计更加接近于合格成品的参数数值,大幅度降低喷嘴的研制成本; 2. The pressure measuring part of the utility model communicates with the cavity area between the nozzle and the guide tube, that is, real-time detection of the final stable simulated airflow pressure value, which is convenient for the staff to adjust the flow rate and flow rate of the compressed air in time according to the actual situation. Improve the diversity of nozzle detection performance parameters, make product simulation design closer to the parameter values of qualified finished products, and greatly reduce the development cost of nozzles;

3、本实用新型中分流孔的孔径为导流孔孔径的1/4,使得压缩空气通过气盒、分流孔、靠近空腔端部的区域以及导流管实现多次换向和变速,与直射喷流相比,本实用新型中气流状态变化更加复杂,更加贴近于喷嘴所处的实际环境条件,并且通过多次换向和变速,由导流管中喷出气流所产生的絮流与通过Fluent软件模拟确认紊流相比消减78%以上,保证了喷嘴良好的测试环境。 3. The diameter of the diversion hole in the utility model is 1/4 of the diameter of the diversion hole, so that the compressed air can pass through the air box, the diversion hole, the area near the end of the cavity and the diversion tube to realize multiple reversing and speed changes, which is consistent with Compared with the direct jet flow, the change of the air flow state in the utility model is more complicated, and it is closer to the actual environmental conditions where the nozzle is located, and through multiple reversing and speed changes, the flocculate flow produced by the jet flow in the guide tube and the Through Fluent software simulation, it is confirmed that the turbulent flow is reduced by more than 78%, which ensures a good test environment for the nozzle.

附图说明 Description of drawings

此处所说明的附图用来提供对本实用新型实施例的进一步理解,构成本申请的一部分,并不构成对本实用新型实施例的限定。在附图中: The drawings described here are used to provide a further understanding of the embodiments of the utility model, constitute a part of the application, and do not constitute a limitation to the embodiments of the utility model. In the attached picture:

图1为本实用新型的结构示意图; Fig. 1 is the structural representation of the utility model;

图2本实用新型的俯视图; Fig. 2 is the top view of the utility model;

附图中标记及相应的零部件名称: Marks and corresponding component names in the attached drawings:

1-导流管、2-气盒、3-分流孔、4-密封环、5-进气口、6-装夹本体、7-测压件、8-喷嘴、9-密封件。 1-Drain pipe, 2-Air box, 3-Split hole, 4-Sealing ring, 5-Inlet, 6-Clamping body, 7-Pressure measuring part, 8-Nozzle, 9-Seal.

具体实施方式 detailed description

为使本实用新型的目的、技术方案和优点更加清楚明白,下面结合实施例和附图,对本实用新型作进一步的详细说明,本实用新型的示意性实施方式及其说明仅用于解释本实用新型,并不作为对本实用新型的限定。 In order to make the purpose, technical solutions and advantages of the utility model clearer, the utility model will be further described in detail below in conjunction with the examples and accompanying drawings. The schematic implementation of the utility model and its description are only used to explain the utility model Novelty, not as a limitation to the utility model.

实施例1 Example 1

如图1和图2所示,本实施例包括内部开设空腔的装夹本体6,在所述空腔的中部安装有多个并排设置且其轴线与装夹本体6平行的导流管1,在所述装夹本体6一端上安装有气盒2,在装夹本体6的上壁开有多个分流孔3,所述气盒2上端通过进气口5与外部连通,气盒2下端通过分流孔3与空腔连通,喷嘴8贯穿所述装夹本体6另一端且喷嘴8的局部与空腔连通,喷嘴8通过密封件9、密封环4实现在装夹本体6上的密封。本实用新型使用时,通过密封件9以及密封环4将喷嘴8固定密封在空腔的端部,向进气口5内注入压缩空气,使得压缩空气在气盒2内汇聚后通过多个分流孔3进行初步的分流直至进入到空腔内,此时压缩空气通过空腔中部的多个导流管1形成多股相对稳定且流速大小不一的气流,且多股气流直接冲击至喷嘴8与空腔的连通部分,使得喷嘴8处于仿真阶段的气流环境,方便对喷嘴8的油液流量、雾化锥度、状态分布等进行检测记录,缩短喷嘴8在图纸设计→产品制造→成品检测试验→图纸设计中反复循环调整时间,降低仿真与实际生产制造之间的差异;并且压缩空气的流量以及流速可根据实际检测的需要进行及时调节,通过分流孔3以及导流管1的逐级稳定分流,使得仿真阶段的气流状态更加接近与实际值,提高喷嘴8空气流量检测数据的精确度。 As shown in Figures 1 and 2, this embodiment includes a clamping body 6 with a cavity inside, and a plurality of flow guide tubes 1 arranged side by side and whose axes are parallel to the clamping body 6 are installed in the middle of the cavity. , an air box 2 is installed on one end of the clamping body 6, and a plurality of flow holes 3 are opened on the upper wall of the clamping body 6, and the upper end of the air box 2 communicates with the outside through the air inlet 5, and the air box 2 The lower end communicates with the cavity through the split hole 3, the nozzle 8 runs through the other end of the clamping body 6 and part of the nozzle 8 communicates with the cavity, the nozzle 8 is sealed on the clamping body 6 through the seal 9 and the sealing ring 4 . When the utility model is in use, the nozzle 8 is fixed and sealed at the end of the cavity through the sealing member 9 and the sealing ring 4, and compressed air is injected into the air inlet 5, so that the compressed air passes through multiple shunts after gathering in the air box 2 The hole 3 performs a preliminary diversion until it enters the cavity. At this time, the compressed air passes through multiple guide tubes 1 in the middle of the cavity to form multiple relatively stable airflows with different flow velocities, and the multiple airflows directly hit the nozzle 8. The connection part with the cavity makes the nozzle 8 in the airflow environment of the simulation stage, which is convenient for testing and recording the oil flow, atomization taper, state distribution, etc. of the nozzle 8, and shortens the process of the nozzle 8 in drawing design → product manufacturing → finished product inspection test →Repeated cycle adjustment time in drawing design to reduce the difference between simulation and actual manufacturing; and the flow rate and flow rate of compressed air can be adjusted in time according to the actual detection needs, through the step-by-step stability of the diversion hole 3 and the guide tube 1 The split flow makes the air flow state in the simulation stage closer to the actual value, and improves the accuracy of the air flow detection data of the nozzle 8.

其中,还包括固定在所述装夹本体6上壁且与空腔连通的测压件7,所述测压件7与喷嘴8的中心距为5~15㎜。测压件7与喷嘴8和导流管1之间的空腔区域连通,即实时检测最终的稳定的仿真气流压力值,方便工作人员根据实际情况及时调整压缩空气的流量以及流速,提高喷嘴8检测性能参数的多样性,使得产品仿真设计更加接近于合格成品的参数数值,大幅度降低喷嘴8的研制成本;压缩空气通过进气口5注入到气盒2中,通过分流孔3的泄压,使得气流以一个更快的流速喷射入空腔内,最终通过空腔端部空间的缓冲并且在导流管1的导向作用下,形成多股的稳定气流向喷嘴8移动,而分流孔3的孔径为导流孔孔径的1/4,使得压缩空气通过气盒2、分流孔3、靠近空腔端部的区域以及导流管1实现多次换向和变速,与直射喷流相比,本实用新型中气流状态变化更加复杂,更加贴近于喷嘴8所处的实际环境条件,并且通过多次换向和变速,由导流管1中喷出气流所产生的絮流与通过Fluent软件模拟确认紊流相比消减78%以上,保证了喷嘴8良好的测试环境。 Wherein, it also includes a pressure measuring part 7 fixed on the upper wall of the clamping body 6 and communicated with the cavity, and the center distance between the pressure measuring part 7 and the nozzle 8 is 5-15 mm. The pressure measuring part 7 communicates with the cavity area between the nozzle 8 and the guide tube 1, that is, real-time detection of the final and stable simulated airflow pressure value, which is convenient for the staff to adjust the flow rate and flow rate of the compressed air in time according to the actual situation, and improve the pressure of the nozzle 8. The diversity of detection performance parameters makes the product simulation design closer to the parameter values of qualified finished products, greatly reducing the development cost of nozzle 8; , so that the air flow is injected into the cavity at a faster flow rate, and finally passes through the buffer of the end space of the cavity and under the guidance of the guide tube 1, forms a plurality of stable air flows to the nozzle 8, while the split hole 3 The aperture is 1/4 of the aperture of the diversion hole, so that the compressed air passes through the air box 2, the diversion hole 3, the area near the end of the cavity, and the diversion tube 1 to achieve multiple reversing and speed changes. Compared with the direct jet , the change of the air flow state in the utility model is more complicated, and it is closer to the actual environmental conditions where the nozzle 8 is located, and through multiple reversing and speed changes, the flocculation generated by the jetting air flow in the draft tube 1 is compared with the flow through the Fluent software The simulation confirms that the turbulent flow is reduced by more than 78% compared to that, which ensures a good test environment for the nozzle 8 .

作为优选,多个分流孔3的均匀分布以及其总分布面积的特殊设置,进一步减小在导流管1内的气流产生的絮流量,提高仿真环境下喷嘴8检测参数的准确性和全面性。 As a preference, the uniform distribution of a plurality of distribution holes 3 and the special setting of its total distribution area further reduce the floc flow generated by the air flow in the draft tube 1, and improve the accuracy and comprehensiveness of the detection parameters of the nozzle 8 in the simulation environment .

以上所述的具体实施方式,对本实用新型的目的、技术方案和有益效果进行了进一步详细说明,所应理解的是,以上所述仅为本实用新型的具体实施方式而已,并不用于限定本实用新型的保护范围,凡在本实用新型的精神和原则之内,所做的任何修改、等同替换、改进等,均应包含在本实用新型的保护范围之内。 The specific embodiments described above have further described the purpose, technical solutions and beneficial effects of the present utility model in detail. Within the protection scope of the utility model, any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the utility model shall be included in the protection scope of the utility model.

Claims (4)

1. a nozzle air flow test clamping device, comprise the clamping body (6) that cavity is offered in inside, it is characterized in that: multiple being arranged side by side and its axis mozzle (1) parallel with clamping body (6) is installed at the middle part of described cavity, described clamping body (6) one end is provided with gas box (2), multiple tap hole (3) is had at the upper wall of clamping body (6), described gas box (2) upper end is by air intake opening (5) and ft connection, gas box (2) lower end is by tap hole (3) and cavity connects, nozzle (8) runs through described clamping body (6) other end and the local of nozzle (8) and cavity connects, nozzle (8) is by seal (9), sealing ring (4) realizes the sealing on clamping body (6).
2. a kind of nozzle air flow test clamping device according to claim 1, it is characterized in that: also comprise be fixed on described clamping body (6) upper wall and with the pressure measuring piece (7) of cavity connects, described pressure measuring piece (7) is 5 ~ 15 ㎜ with the centre distance of nozzle (8).
3. a kind of nozzle air flow test clamping device according to claim 1, is characterized in that: the aperture of described tap hole (3) is 1/4 of mozzle (1) aperture.
4. a kind of nozzle air flow test clamping device according to claim 1 or 3, it is characterized in that: multiple described tap hole (3) is evenly distributed on the bottom of described gas box (2), and the total distributed area of multiple described tap hole (3) is 1/10 ~ 1/5 of the bottom area of described gas box (2).
CN201520361805.9U 2015-05-29 2015-05-29 Experimental clamping device of using of nozzle air mass flow Expired - Lifetime CN204988692U (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106768946A (en) * 2016-12-21 2017-05-31 成都航利航空科技有限责任公司 A kind of fuel nozzle radial distribution comprehensive measurement device
CN108603779A (en) * 2016-02-09 2018-09-28 高准公司 Method and apparatus for modulating flow passage
CN109632324A (en) * 2018-12-13 2019-04-16 西安航天动力研究所 A test device for nozzle liquid flow test
CN110068458A (en) * 2019-04-16 2019-07-30 安徽捷迅光电技术有限公司 A kind of snifting valve flow detection frock

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108603779A (en) * 2016-02-09 2018-09-28 高准公司 Method and apparatus for modulating flow passage
CN106768946A (en) * 2016-12-21 2017-05-31 成都航利航空科技有限责任公司 A kind of fuel nozzle radial distribution comprehensive measurement device
CN109632324A (en) * 2018-12-13 2019-04-16 西安航天动力研究所 A test device for nozzle liquid flow test
CN109632324B (en) * 2018-12-13 2020-07-24 西安航天动力研究所 Test device for nozzle liquid flow test
CN110068458A (en) * 2019-04-16 2019-07-30 安徽捷迅光电技术有限公司 A kind of snifting valve flow detection frock

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