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CN101408237A - Hollow shafting core rod type damping vibration absorber - Google Patents

Hollow shafting core rod type damping vibration absorber Download PDF

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Publication number
CN101408237A
CN101408237A CNA2008101558414A CN200810155841A CN101408237A CN 101408237 A CN101408237 A CN 101408237A CN A2008101558414 A CNA2008101558414 A CN A2008101558414A CN 200810155841 A CN200810155841 A CN 200810155841A CN 101408237 A CN101408237 A CN 101408237A
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China
Prior art keywords
layer
damping
mandrel
vibration
hollow shaft
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Pending
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CNA2008101558414A
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Chinese (zh)
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陈前
段勇
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Nanjing University of Aeronautics and Astronautics
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Nanjing University of Aeronautics and Astronautics
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Priority to CNA2008101558414A priority Critical patent/CN101408237A/en
Publication of CN101408237A publication Critical patent/CN101408237A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a hollow shafting mandril type damping shock absorber which belongs to the damping vibration reduction field. The absorber comprises a binder course (2), a viscoelasticity damping layer (3) and a damping mandril (4). The viscoelasticity damping layer is used for simultaneously controlling the torsional vibration and the longitudinal vibration of the hollow shafting. The damping mandril has the restriction function. The viscoelasticity damping layer can be expanded into multi-layer structure and is replaced by the composite structure consisting of a viscoelasticiy layer and an elastic restraint layer. The absorber integrates torsional vibration and longitudinal control devices, meanwhile, the absorber is arranged in the internal cavity of the shafting, which does not occupy outer space, and saves cost and space.

Description

空心轴系芯棒式阻尼减振器 Hollow Shaft Mandrel Type Damping Shock Absorber

技术领域 technical field

本发明涉及一种空心轴系芯棒式阻尼减振器,属于阻尼减振技术领域,尤其涉及空心轴系扭转振动、纵向振动阻尼减振器。The invention relates to a hollow shaft mandrel type damping shock absorber, which belongs to the technical field of damping and vibration reduction, in particular to a hollow shafting torsional vibration and longitudinal vibration damping shock absorber.

背景技术 Background technique

船舶等大型机构的传动系统的轴系由于受到动力设备及螺旋桨的激励容易产生振动,而且其振动形式是多向的,即同时存在扭转振动、纵向振动和横向振动。而由于由扭转振动所产生的事故占有较大的比例,所以人们在研究中往往关注扭转振动较多,研究了多种扭转振动减振器,包括各种摆式扭振阻尼器,粘性液式阻尼器以及磁流变液阻尼器,同时也有控制其横向振动的减振装置,像专利CN 1620563A所述的轴阻尼器,而由于纵向振动的减振装置的复杂性,一般很少涉及,而且目前轴系各种的振动控制装置均是置于轴系的外部,需要占用额外的空间,同时由于控制不同方向振动的装置是分开来研究的,加大了研究和制造的成本。The shafting of the transmission system of ships and other large-scale institutions is prone to vibration due to the excitation of power equipment and propellers, and its vibration form is multi-directional, that is, torsional vibration, longitudinal vibration and lateral vibration exist at the same time. Since the accidents caused by torsional vibration account for a relatively large proportion, people often pay more attention to torsional vibration in research, and have studied a variety of torsional vibration dampers, including various pendulum torsional vibration dampers, viscous liquid type Dampers and magnetorheological fluid dampers also have damping devices to control their lateral vibrations, such as the shaft dampers described in patent CN 1620563A, but due to the complexity of the damping devices for longitudinal vibrations, they are generally rarely involved, and At present, various vibration control devices of the shafting system are placed outside the shafting system, which requires additional space. At the same time, since the devices for controlling vibration in different directions are studied separately, the cost of research and manufacturing is increased.

发明内容 Contents of the invention

本发明目的在于弥补现有轴系振动减振器的不足,提供了一种新型的轴系振动综合控制减振器,该减振器可以同时减小轴系的两向振动,即减振器既可减小其扭转振动又可减小其纵向振动。同时根据船舶等大型机构的传动轴系为空心结构的特点,将减振器设置于轴的空腔内,不占用额外的空间。The purpose of the present invention is to make up for the deficiencies of existing shafting vibration dampers, and provides a new type of shafting vibration comprehensive control damper, which can simultaneously reduce the two-way vibration of the shafting, that is, the shock absorber It can reduce its torsional vibration and reduce its longitudinal vibration. At the same time, according to the characteristics of the hollow structure of the transmission shaft system of large-scale institutions such as ships, the shock absorber is arranged in the cavity of the shaft without occupying additional space.

一种空心轴系芯棒式阻尼减振器,用来同时控制轴系的扭转振动和纵向振动,其特征在于:它包括安装于空心轴内部空腔的联结层,粘贴在联结层上的粘弹性阻尼层,以及置于空心轴轴心的约束芯棒。A hollow shaft mandrel type damping shock absorber, which is used to simultaneously control the torsional vibration and longitudinal vibration of the shaft, is characterized in that it includes a connecting layer installed in the inner cavity of the hollow shaft, and an adhesive An elastic damping layer, and a constrained mandrel placed at the center of the hollow shaft.

粘弹性阻尼层可考虑拓展为多层结构,由粘弹性层和弹性约束层组成的复合结构代替。The viscoelastic damping layer can be considered to be extended to a multi-layer structure, which is replaced by a composite structure composed of a viscoelastic layer and an elastic constrained layer.

联结层和约束芯棒之间的粘弹性阻尼层在轴系扭转振动和纵向振动时均处于有效剪切状态,能够耗散系统能量。本发明的阻尼芯棒式减振器将扭转振动控制装置和纵向振动控制装置合二为一,既可控制轴系的扭转振动又可控制其纵向振动,同时将减振器置于空心轴系的空腔内,即节省了成本又节约了空间。The viscoelastic damping layer between the connecting layer and the constraining mandrel is in an effective shear state during torsional vibration and longitudinal vibration of the shaft system, which can dissipate the energy of the system. The damping mandrel type shock absorber of the present invention combines the torsional vibration control device and the longitudinal vibration control device into one, which can control both the torsional vibration of the shaft system and its longitudinal vibration, and at the same time place the shock absorber in the hollow shaft system In the cavity, it saves cost and saves space.

附图说明 Description of drawings

图1为空心轴系芯棒式阻尼减振器的轴向视图。Fig. 1 is an axial view of a hollow shafting mandrel type damping shock absorber.

图2为空心轴系芯棒式阻尼减振器的轴线剖面图。Fig. 2 is an axial sectional view of the hollow shaft mandrel type damping shock absorber.

图中各部件名称为:1.空心轴  2.联结层  3.粘弹性阻尼层  4.约束芯棒。The names of the components in the figure are: 1. Hollow shaft 2. Coupling layer 3. Viscoelastic damping layer 4. Constraint mandrel.

具体实施方式 Detailed ways

如图1、2所示,本发明的空心轴系芯棒式阻尼减振器,它包括安装于轴内部空腔的圆筒形的联结层2,还包括圆柱状的约束芯棒4,圆筒形的粘弹性阻尼层3黏附于联结层和芯棒之间,其中根据图所示,联结层的长度比粘弹性层和芯棒的稍长,目的是为了在伸出来的部分上加工联接零件,使减振器更方便的固定在轴内部。As shown in Figures 1 and 2, the hollow shafting mandrel type damping shock absorber of the present invention includes a cylindrical coupling layer 2 installed in the inner cavity of the shaft, and also includes a cylindrical restraining mandrel 4, round A cylindrical viscoelastic damping layer 3 is adhered between the connecting layer and the mandrel, wherein according to the figure, the length of the connecting layer is slightly longer than that of the viscoelastic layer and the mandrel, in order to process the connection on the protruding part Parts, so that the shock absorber is more conveniently fixed inside the shaft.

当轴系发生扭转振动时,粘弹性阻尼层在联结层和约束芯棒的约束下发生周向剪切变形,耗散能量,起到减小扭转振动的作用;当轴系发生纵向振动时粘弹性阻尼层在联结层和约束芯棒的约束下发生轴向剪切变形,耗散能量,起到减小纵向振动的作用。When the torsional vibration of the shaft system occurs, the viscoelastic damping layer undergoes circumferential shear deformation under the constraints of the coupling layer and the restraint mandrel, dissipates energy, and plays a role in reducing torsional vibration; when the shaft system undergoes longitudinal vibration, the viscoelastic damping layer The elastic damping layer undergoes axial shear deformation under the constraint of the connecting layer and the constraining mandrel, dissipates energy, and plays a role in reducing longitudinal vibration.

粘弹性阻尼层3可考虑拓展为多层结构,由粘弹性层和弹性约束层组成的复合结构代替;可以根据需要改变其层数,设计成多层结构。The viscoelastic damping layer 3 can be expanded to a multi-layer structure, replaced by a composite structure composed of a viscoelastic layer and an elastic constrained layer; the number of layers can be changed according to needs, and a multi-layer structure can be designed.

Claims (3)

1、一种空心轴系芯棒式阻尼减振器,用来同时控制空心轴系扭转振动和纵向振动,其特征在于:它包括安装于空心轴内部空腔的圆筒形的联结层(2),圆柱状的约束芯棒(4),以及黏附于联结层和约束芯棒之间的粘弹性阻尼层(3)。1. A hollow shaft mandrel type damping shock absorber, which is used to simultaneously control the torsional vibration and longitudinal vibration of the hollow shaft, is characterized in that: it includes a cylindrical coupling layer (2 ), a cylindrical constraining mandrel (4), and a viscoelastic damping layer (3) adhered between the tie layer and the constraining mandrel. 2、一种空心轴系芯棒式阻尼减振器,用来同时控制空心轴系扭转振动和纵向振动。其特征在于:它包括安装于空心轴内部空腔的圆筒形的联结层(2),圆柱状的约束芯棒(4),以及黏附于联结层和约束芯棒之间的弹性--粘弹性复合结构,该复合结构由粘弹性层(5)和弹性约束层(6)组成。2. A hollow shaft mandrel type damping shock absorber, which is used to simultaneously control the torsional vibration and longitudinal vibration of the hollow shaft. It is characterized in that it includes a cylindrical coupling layer (2) installed in the inner cavity of the hollow shaft, a cylindrical constraining mandrel (4), and an elastic-viscosity bonded between the coupling layer and the constraining mandrel. An elastic composite structure, the composite structure is composed of a viscoelastic layer (5) and an elastic constrained layer (6). 3、根据权利要求2中所述的空心轴系芯棒式阻尼减振器,其特征在于:所述的弹性-粘弹性复合结构的粘弹性层和弹性约束层的层数可以根据需要任意设计。3. The hollow shaft mandrel type damping shock absorber according to claim 2, characterized in that: the number of viscoelastic layers and elastic constrained layers of the elastic-viscoelastic composite structure can be arbitrarily designed according to needs .
CNA2008101558414A 2008-10-10 2008-10-10 Hollow shafting core rod type damping vibration absorber Pending CN101408237A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA2008101558414A CN101408237A (en) 2008-10-10 2008-10-10 Hollow shafting core rod type damping vibration absorber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA2008101558414A CN101408237A (en) 2008-10-10 2008-10-10 Hollow shafting core rod type damping vibration absorber

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CN101408237A true CN101408237A (en) 2009-04-15

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102052387A (en) * 2011-01-07 2011-05-11 富奥汽车零部件股份有限公司 Vibration reduction structure of transmission shaft assembly
CN103671699A (en) * 2013-12-23 2014-03-26 江苏科技大学 Inbuilt damping device for hollow shaft
CN103727168A (en) * 2013-11-18 2014-04-16 安徽淮化股份有限公司 Shaft body energy absorber
CN104279264A (en) * 2014-09-18 2015-01-14 亚新科噪声与振动技术(安徽)有限公司 Transmission shaft vibration absorber
CN104696432A (en) * 2015-02-13 2015-06-10 柳州金鸿橡塑有限公司 Built-in broadband torsion damper
CN105422732A (en) * 2015-12-09 2016-03-23 北京工业大学 Composite damping vibration attenuation expansion rod structure for thin and long rotary shaft
CN109933916A (en) * 2019-03-18 2019-06-25 山东大学 Method and system for inversion of longitudinal excitation of propeller based on longitudinal vibration response measurement of shafting

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102052387A (en) * 2011-01-07 2011-05-11 富奥汽车零部件股份有限公司 Vibration reduction structure of transmission shaft assembly
CN103727168A (en) * 2013-11-18 2014-04-16 安徽淮化股份有限公司 Shaft body energy absorber
CN103671699A (en) * 2013-12-23 2014-03-26 江苏科技大学 Inbuilt damping device for hollow shaft
CN103671699B (en) * 2013-12-23 2015-09-02 江苏科技大学 The built-in vibration damping equipment of a kind of hollow shaft
CN104279264A (en) * 2014-09-18 2015-01-14 亚新科噪声与振动技术(安徽)有限公司 Transmission shaft vibration absorber
CN104696432A (en) * 2015-02-13 2015-06-10 柳州金鸿橡塑有限公司 Built-in broadband torsion damper
CN105422732A (en) * 2015-12-09 2016-03-23 北京工业大学 Composite damping vibration attenuation expansion rod structure for thin and long rotary shaft
CN105422732B (en) * 2015-12-09 2018-12-07 北京工业大学 Stick structure that a kind of composite damping vibration damping for elongated rotating shaft is swollen
CN109933916A (en) * 2019-03-18 2019-06-25 山东大学 Method and system for inversion of longitudinal excitation of propeller based on longitudinal vibration response measurement of shafting
CN109933916B (en) * 2019-03-18 2020-07-31 山东大学 Method and system for inverting propeller longitudinal excitation based on shafting longitudinal vibration response measurement

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Open date: 20090415