CN103291494A - Exercise-decoupling axial-symmetry thrust vectoring nozzle adjusting mechanism with sliding pairs - Google Patents
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Abstract
一种航空发动机技术领域的运动解耦含有移动副的轴对称矢量喷管调节机构,包括:静平台、动平台、通过三个主动支路和三个被动支路组成的轴对称矢量喷管调节机构连接静平台与动平台,从而形成六支路的三自由度并联机构;第一、二被动支路包括:依次串联的万向副以及下、上转动副;第三被动支路包括:依次串联的移动副、转动副和万向副;第四、五、六主动支路包括:依次串联的上球铰副、移动副以及下球铰副。本发明能实现调节环的纯转动输出,即在调节环绕某轴转动的同时不会产生伴随的移动,故其具有运动解耦性好而易于控制等优点;该机构中含有更少的球铰副,从而降低了制造成本和安装难度。
A movement decoupling mechanism in the technical field of aero-engines includes an axisymmetric vector nozzle adjustment mechanism with moving pairs, including: a static platform, a dynamic platform, and an axisymmetric vector nozzle adjustment composed of three active branches and three passive branches. The mechanism connects the static platform and the dynamic platform to form a three-degree-of-freedom parallel mechanism with six branches; the first and second passive branches include: the universal joints connected in series and the lower and upper rotating pairs; the third passive branch includes: The moving pair, the rotating pair and the universal pair connected in series; the fourth, fifth and sixth active branches include: the upper spherical joint pair, the moving pair and the lower spherical joint pair connected in series in sequence. The invention can realize the pure rotation output of the adjustment ring, that is, when the adjustment rotates around a certain axis, there will be no accompanying movement, so it has the advantages of good motion decoupling and easy control; the mechanism contains fewer ball joints Vice, thereby reducing the manufacturing cost and installation difficulty.
Description
技术领域technical field
本发明涉及的是一种航空发动机技术领域的装置,具体是一种运动解耦含有移动副的轴对称矢量喷管调节机构。The invention relates to a device in the field of aero-engine technology, in particular to an axisymmetric vector nozzle adjustment mechanism with motion decoupling and a moving pair.
背景技术Background technique
轴对称推力矢量技术是现代先进战斗机的关键技术之一,其特点是通过改变发动机尾喷管的气流方向而产生的力矩来操纵飞机,在实现了水平推进同时提供偏航俯仰附加力矩,它的引入使战斗机的隐身性、机动性、敏捷性、短距起落能力和超音速巡航等性能得到了充分的发挥和提高。实现推力矢量化需要相应的推力矢量装置,其中可作360度转动的轴对称矢量喷管(Axial-Symmetric Vectoring Exhaust Nozzle,AVEN)代表了发动机排气系统设计与研究的发展方向。在该矢量喷装置中,具有一移动两转动运动特征的调节环结构是实现喷管作360度偏转的关键部件。Axisymmetric thrust vectoring technology is one of the key technologies of modern advanced fighter jets. It is characterized by manipulating the aircraft by changing the direction of the airflow of the engine tail nozzle to provide additional moments for yaw and pitch while achieving horizontal propulsion. The introduction has fully brought into play and improved the stealth, maneuverability, agility, short take-off and landing capability and supersonic cruise of fighter jets. Achieving thrust vectoring requires a corresponding thrust vectoring device, among which the Axial-Symmetric Vectoring Exhaust Nozzle (AVEN), which can rotate 360 degrees, represents the development direction of engine exhaust system design and research. In the vector spraying device, the adjusting ring structure with the characteristics of one movement and two rotations is the key component to realize the 360-degree deflection of the nozzle.
目前,国外所公开的该类调节机构(如专利文献号US5174502、US5779152、US5820024、US6142416、US6199772、US6415599、EP0886061B1)采用的是3-PRS/3-SPS或3-PRS/3-SPS等六支路并联机构,其中3条SPS支路做主动支链,3条PRS或RRS作被动支链用于对调节环定心。然而对该类机构而言,其不能实现调节环纯转动输出,即当绕某轴转动的同时必然产生伴随的移动,故其耦合性较强,运动求解较复杂,控制也较复杂;含有较多的难以加工的S副,使得制造成本增加。At present, such adjustment mechanisms disclosed abroad (such as patent literature numbers US5174502, US5779152, US5820024, US6142416, US6199772, US6415599, EP0886061B1) use six such as 3-PRS/3-SPS or 3-PRS/3-SPS In parallel mechanism, three SPS branches are used as active branch chains, and three PRS or RRS branches are used as passive branch chains for centering the adjustment ring. However, for this type of mechanism, it cannot realize the pure rotation output of the adjustment ring, that is, when it rotates around a certain axis, it must produce accompanying movement, so its coupling is strong, the motion solution is more complicated, and the control is also more complicated; Many S pairs that are difficult to process make the manufacturing cost increase.
因此,设计含有更少的球铰S副,能实现调节环的纯转动输出、运动解耦性好而易于控制的一移动两转动矢量喷管装置实际工程应用的迫切需要。Therefore, there is an urgent need for the actual engineering application of a one-moving two-rotation vectoring nozzle device with less spherical hinge S pairs, which can realize the pure rotation output of the adjustment ring, good motion decoupling and easy control.
发明内容Contents of the invention
本发明针对现有技术存在的上述不足,提出一种运动解耦含有移动副的轴对称矢量喷管调节机构,能实现动平台的纯转动输出,即在动平台绕某轴转动的同时不会产生伴随的移动,故其具有运动解耦性好而易于控制等优点;该机构中含有更少的球铰副S,从而降低了制造成本和安装难度。Aiming at the above-mentioned deficiencies in the prior art, the present invention proposes an axisymmetric vector nozzle adjustment mechanism with motion decoupling and a moving pair, which can realize the pure rotation output of the moving platform, that is, the moving platform will not rotate around a certain axis at the same time. Accompanied movement is generated, so it has the advantages of good motion decoupling and easy control; the mechanism contains fewer spherical joint pairs S, thereby reducing manufacturing cost and installation difficulty.
本发明是通过以下技术方案实现的,本发明包括:以机匣作为静平台,以调节环作为动平台,通过三个主动支路和三个被动支路组成的轴对称矢量喷管调节机构连接静平台与动平台,从而形成六支路的三自由度并联机构。The present invention is achieved through the following technical proposals. The present invention includes: the casing is used as a static platform, and the adjusting ring is used as a dynamic platform, which is connected by an axisymmetric vector nozzle adjustment mechanism composed of three active branches and three passive branches. The static platform and the dynamic platform form a three-degree-of-freedom parallel mechanism with six branches.
所述的第一、二被动支路包括:依次串联的万向副以及下、上转动副,其中:万向副的第二根转动轴线、下、上转动副的轴线相互平行;The first and second passive branches include: the universal joint and the lower and upper rotating joints connected in series in sequence, wherein: the second rotation axis of the universal joint and the axes of the lower and upper rotating joints are parallel to each other;
所述的第三被动支路包括:依次串联的移动副、转动副和万向副,其中:转动副轴线与万向副的第二根转动轴线相互平行,移动副的轴线与转动副的轴线垂直;The third passive branch includes: a moving pair, a rotating pair and a universal pair connected in series in sequence, wherein: the axis of the rotating pair is parallel to the second rotation axis of the universal pair, and the axis of the moving pair is parallel to the axis of the rotating pair. vertical;
所述的万向副拥有两个相互垂直的转动轴线,其中第一根轴线为固定在机匣或调节环上的转动轴线,第二根转动轴线为与第一根轴线相垂直的转动轴线。The universal joint has two mutually perpendicular rotation axes, wherein the first axis is the rotation axis fixed on the casing or the adjusting ring, and the second rotation axis is the rotation axis perpendicular to the first axis.
所述的第四、五、六主动支路包括:依次串联的下球铰副、移动副以及上球铰副;该移动副为主动副;主动移动副的驱动是电机带动的丝杆机构或液压缸系统驱动。The fourth, fifth, and sixth active branches include: the lower ball joint pair, the moving pair and the upper ball joint pair connected in series; the moving pair is the active pair; the driving of the active moving pair is a screw mechanism or Driven by hydraulic cylinder system.
第一被动支路中的第一万向副与第二被动支路中的第二万向副,以及第三被动支路中的第三下移动副为基准对称布置;The first universal pair in the first passive branch, the second universal pair in the second passive branch, and the third lower moving pair in the third passive branch are based on a symmetrical arrangement;
第一被动支路中第一万向副的第一根转动轴线与第三被动支路中第三上转动副的轴线相互平行;The first rotation axis of the first universal joint in the first passive branch is parallel to the axis of the third upper rotation joint in the third passive branch;
第一被动支路中第一上转动副的轴线与第三被动支路中第三万向副的第一根转动轴线相互平行;The axis of the first upper rotating pair in the first passive branch is parallel to the first rotation axis of the third universal joint in the third passive branch;
第一被动支路中第一万向副的第一根转动轴线与第二被动支路中第二万向副的第一根转动轴线共线;The first rotation axis of the first universal joint in the first passive branch is collinear with the first rotation axis of the second universal joint in the second passive branch;
第一被动支路中第一上转动副轴线与第二被动支路中第二上转动副轴线平行。The axis of the first upper rotary pair in the first passive branch is parallel to the axis of the second upper rotary pair in the second passive branch.
第一被动支路中第一万向副的第一根转动轴线、第二被动支路中第二万向副的第一根转动轴线以及第三被动支路中第三上转动副的轴线均平行于静平台所在的平面。The first rotation axis of the first universal joint in the first passive branch, the first rotation axis of the second universal joint in the second passive branch, and the axis of the third upper rotating joint in the third passive branch are all Parallel to the plane where the static platform is located.
此外,保持各被动分支的型位关系,将动平台与静平台位置互换一下,也可以得到类似的一种运动解耦的轴对称矢量喷管调节机构。In addition, maintaining the type-position relationship of each passive branch and exchanging the positions of the dynamic platform and the static platform, a similar motion-decoupled axisymmetric vector nozzle adjustment mechanism can also be obtained.
该调节机构以球铰副-移动副-球铰副(SPS)为主动支链,万向副-转动副-转动副(URR)与移动副-转动副-万向副(PRU)为被动支链;调节环动平台可实现空间内的两个转动自由度和一个移动自由度;其中一个转动自由度是动平台可绕第一被动支路的第一万向副的第一根转动轴线转动,另一个转动自由度是动平台可绕第三被动支路第三万向副的第一转动轴线转动;移动自由度是动平台可沿第一上转动副的轴线与第三被动支路第三上转动副的轴线的公垂线方向移动。The adjustment mechanism uses the spherical joint-moving joint-spherical joint (SPS) as the active branch chain, the universal joint-rotating joint-rotating joint (URR) and the mobile joint-rotating joint-universal joint (PRU) as the passive supporting chain. chain; adjusting the ring motion platform can realize two degrees of freedom of rotation and one degree of freedom of movement in space; one of the degrees of freedom of rotation is that the motion platform can rotate around the first axis of rotation of the first universal joint of the first passive branch , the other degree of freedom of rotation is that the moving platform can rotate around the first rotation axis of the third universal joint of the third passive branch; the degree of freedom of movement is that the moving platform can rotate along the axis of the first upper rotating joint The common vertical direction of the axes of the three upper revolving pairs moves.
技术效果technical effect
与现有技术相比,本发明动平台能实现绕上述转动轴线的纯转动,而不产生伴随的移动;动平台能实现沿上述移动方向的纯移动,而不产生伴随的转动。由此可知该机构运动完全解耦,故其具有运动求解较、控制较易的优点。Compared with the prior art, the moving platform of the present invention can realize pure rotation around the above-mentioned rotation axis without accompanying movement; the moving platform can realize pure movement along the above-mentioned moving direction without producing accompanying rotation. It can be seen that the motion of the mechanism is completely decoupled, so it has the advantages of relatively easy motion solution and easy control.
由于含有比原有机构3-PRS/3-SPS或3-PRS/3-SPS更少的球铰副S,故其结构简单,制造精度要求可以降低,制造成本也可以降低。Because it contains fewer spherical hinge pairs S than the original mechanism 3-PRS/3-SPS or 3-PRS/3-SPS, the structure is simple, the manufacturing precision requirement can be reduced, and the manufacturing cost can also be reduced.
附图说明Description of drawings
图1为本发明结构示意图。Fig. 1 is a schematic diagram of the structure of the present invention.
图2为实施例尾喷管整体结构图。Fig. 2 is the overall structure diagram of the tail nozzle of the embodiment.
具体实施方式Detailed ways
下面对本发明的实施例作详细说明,本实施例在以本发明技术方案为前提下进行实施,给出了详细的实施方式和具体的操作过程,但本发明的保护范围不限于下述的实施例。The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.
实施例1Example 1
如图1所示,动平台M通过六个分支与机匣F并联连接:As shown in Figure 1, the moving platform M is connected in parallel with the casing F through six branches:
第一被动支路I中,第一万向副U1连接机匣F与第一下连杆11,第一下转动副R1a连接第一下连杆11与第一上连杆12,第二上转动副R1b连接第一上连杆12与动平台M;In the first passive branch I, the first universal pair U1 is connected to the case F and the first
第二被动支路II中,第二万向副U2连接机匣F与第二下连杆21,第二下转动副R2a连接第二下连杆21与第二上连杆22,第二上转动副R2b连接第二上连杆22与动平台M;In the second passive branch II, the second universal pair U 2 is connected to the casing F and the second
第三被动支路III中,第三下移动副P3a连接机匣F与第三下连杆31,第三上转动副R3b连接第三下连杆31与第三上连杆32,第三万向副U3连接第三上连杆32与动平台M;In the third passive branch III, the third lower moving pair P 3a is connected to the casing F and the third
第四主动支路IV中,第一下球铰副S1a连接机匣F与第四下连杆41,第一移动副P1连接第四下连杆41与第四上连杆42,第一下上球铰副S1b连接第四上连杆42与动平台M;In the fourth active branch IV, the first lower ball joint pair S 1a connects the casing F and the fourth
第五主动支路V中,第二下球铰副S2a连接机匣F与第五下连杆51,第二移动副P2连接第五下连杆51与第五上连杆52,第二上球铰副S2b连接第五上连杆52与动平台M;In the fifth active branch V, the second lower ball joint pair S 2a is connected to the casing F and the fifth
第六主动支路VI中,第三下球铰副S3a连接机匣F与第六下连杆61,第三移动副P3连接第六下连杆61与第六上连杆62,第三上球铰副S3b连接第六上连杆62与动平台M;In the sixth active branch VI, the third lower ball joint pair S 3a is connected to the casing F and the sixth
其中,各分支的运动副满足如下关系:Among them, the motion pair of each branch satisfies the following relationship:
第一支路I中U1的第二根转动轴线、第一下转动副R1a、第一上转动副R1b转动副轴线相互平行;The second rotation axis of U 1 in the first branch I, the first lower rotation pair R 1a , and the first upper rotation pair R 1b rotation pair axes are parallel to each other;
第二支路II中U2的第二根转动轴线、第二下转动副R2a、第二上转动副R2b转动副轴线相互平行;The second rotation axis of U 2 in the second branch II, the second lower rotation pair R 2a , and the second upper rotation pair R 2b are parallel to each other;
第三被动支路III中第三上转动副R3b的轴线与第三万向副U3的第二根转动轴线相互平行,第三下移动副P3a与第三上转动副R3b的轴线垂直;The axis of the third upper rotating pair R 3b in the third passive branch III is parallel to the second rotating axis of the third universal joint U 3 , and the axes of the third lower moving pair P 3a and the third upper rotating pair R 3b vertical;
第一被动支路I中的第一万向副U1与第二被动支路II中的第二万向副U2,以第三被动支路中的第三下移动副P3a为基准对称布置;The first universal pair U 1 in the first passive branch I and the second universal pair U 2 in the second passive branch II are symmetrical with respect to the third lower moving pair P 3a in the third passive branch arrangement;
第一被动支路I中第一万向副U1的第一根转动轴线与第三被动支路III中第三上转动副R3b的轴线相互平行;The first rotation axis of the first universal joint U 1 in the first passive branch I is parallel to the axis of the third upper rotating pair R 3b in the third passive branch III;
第一被动支路I中第一上转动副R1b的轴线与第三被动支路III中第三万向副U2的第一根转动轴线相互平行;The axis of the first upper rotating pair R 1b in the first passive branch I is parallel to the first rotation axis of the third universal joint U2 in the third passive branch III;
第一被动支路I中第一万向副U1的第一根转动轴线与第二被动支路II中第二万向副U2的第一根转动轴线共线;The first rotation axis of the first universal joint U1 in the first passive branch I is collinear with the first rotation axis of the second universal joint U2 in the second passive branch II;
第一被动支路I中第一上转动副R1b的轴线与第二被动支路II中第二上转动副R2b的轴线相互平行。The axis of the first upper rotating pair R 1b in the first passive branch I and the axis of the second upper rotating pair R 2b in the second passive branch II are parallel to each other.
所述的第四、五、六支路中第一至第三移动副P1、P2、P3为主动副;主动移动副的驱动是电机带动的丝杆机构或液压缸系统驱动。The first to third moving pairs P 1 , P 2 , and P 3 in the fourth, fifth, and sixth branches are active pairs; the driving of the active moving pairs is driven by a screw mechanism driven by a motor or a hydraulic cylinder system.
所述第一被动支路I中的第一万向副U1的第一根转动轴线、第二被动支路II中第二万向副U2的第一根转动轴线以及第三被动支路III中第三上转动副R3b的轴线均平行于静平台F所在的平面。The first rotation axis of the first universal joint U1 in the first passive branch I, the first rotation axis of the second universal joint U2 in the second passive branch II, and the third passive branch The axes of the third upper rotary pair R 3b in III are all parallel to the plane where the static platform F is located.
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CN111779549A (en) * | 2020-07-08 | 2020-10-16 | 孙涛 | Aircraft engine tail nozzle |
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Cited By (8)
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CN105643606A (en) * | 2016-04-01 | 2016-06-08 | 江苏大学 | Novel three-degree-of-freedom parallel robot |
CN106428486A (en) * | 2016-10-08 | 2017-02-22 | 西北工业大学 | Vector propelling device for small underwater vehicle |
CN106428486B (en) * | 2016-10-08 | 2018-11-27 | 西北工业大学 | A kind of vector propulsion device for small-scale underwater vehicle device |
CN107630766A (en) * | 2017-10-11 | 2018-01-26 | 高小秒 | A kind of small-sized fixed-wing unmanned vehicle engine vector spout |
CN108519169A (en) * | 2018-04-25 | 2018-09-11 | 浙江大唐国际绍兴江滨热电有限责任公司 | The temperature sensor assembly of the Natural Gas Power Plant of anti-dropout |
CN111779549A (en) * | 2020-07-08 | 2020-10-16 | 孙涛 | Aircraft engine tail nozzle |
CN115816423A (en) * | 2022-09-20 | 2023-03-21 | 北京萌友智能科技有限公司 | Parallel mechanism holder device for robot, pose control method and controller |
CN115816423B (en) * | 2022-09-20 | 2024-07-05 | 北京萌友智能科技有限公司 | Parallel mechanism holder device for robot, pose control method and controller |
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