CN109187019B - Swing cylinder loaded main rotor ball hinge bearing comprehensive testing machine - Google Patents
Swing cylinder loaded main rotor ball hinge bearing comprehensive testing machine Download PDFInfo
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- CN109187019B CN109187019B CN201811282484.8A CN201811282484A CN109187019B CN 109187019 B CN109187019 B CN 109187019B CN 201811282484 A CN201811282484 A CN 201811282484A CN 109187019 B CN109187019 B CN 109187019B
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Abstract
本发明公开一种摆动油缸加载式主旋翼球铰轴承综合试验机,涉及直升机主旋翼系统轴承试验技术领域,包括支承框架、传动主轴、大圆锥齿轮、小圆锥齿轮、驱动轴、主减速器、驱动电机、液压旋转接头外壳、叶片式摆动油缸、液压阀站、旋翼平台、自动倾斜器旋转环、不旋转环、大球铰轴承、双列薄壁轴承、变距拉杆、扭力臂、防扭臂、助力油缸、油缸摆杆、中立柱、连接座、铰链等构件。本发明加载过程与直升机主旋翼系统的载荷同相位、同频率,能真实模拟直升机主旋翼系统的载荷状态,能实现交变载荷、脉动载荷和恒定载荷的加载,保证主旋翼系统各类轴承服役寿命的确定更精确、更客观。
The invention discloses a comprehensive testing machine for a main rotor ball hinge bearing loaded by a swing oil cylinder, which relates to the technical field of bearing testing of a helicopter main rotor system. Drive motor, hydraulic rotary joint housing, vane swing cylinder, hydraulic valve station, rotor platform, automatic tilter rotating ring, non-rotating ring, large spherical hinge bearing, double row thin-wall bearing, variable pitch rod, torsion arm, anti-twist Arm, booster cylinder, cylinder swing rod, neutral column, connecting seat, hinge and other components. The loading process of the invention is in the same phase and frequency as the load of the main rotor system of the helicopter, which can truly simulate the load state of the main rotor system of the helicopter, realize the loading of alternating loads, pulsating loads and constant loads, and ensure the service of various types of bearings of the main rotor system. The determination of lifespan is more precise and objective.
Description
技术领域technical field
本发明涉及直升机主旋翼系统轴承试验技术领域,特别是涉及一种摆动油缸加载式主旋翼球铰轴承综合试验机。The invention relates to the technical field of bearing testing of a helicopter main rotor system, in particular to a comprehensive testing machine for a swing oil cylinder-loaded main rotor ball hinge bearing.
背景技术Background technique
直升机在飞行过程中,任何组成构件的失效都会造成灾难性后果。因此对直升机组成构件服役寿命的确定是一项非常严肃而重要的工作。为了准确的确定直升机组成构件的服役寿命,通常做法是对直升机组成构件进行模拟真实工况条件下的疲劳试验,再把通过试验求得的疲劳寿命除以一个安全系数即为航空飞行器组成构件的服役寿命。During the flight of the helicopter, the failure of any component can have catastrophic consequences. Therefore, it is a very serious and important work to determine the service life of helicopter components. In order to accurately determine the service life of the components of the helicopter, the usual practice is to carry out the fatigue test of the components of the helicopter under simulated real working conditions, and then divide the fatigue life obtained by the test by a safety factor, which is the component of the aircraft. service life.
直升机主旋翼系统是直升机的核心部件之一,主旋翼系统各活动构件之间的连接是通过各类轴承(球铰轴承、硬质合金套筒轴承和滚动轴承等)实现的。以往主旋翼系统各轴承服役寿命实验均采用单个轴承在疲劳试验机上进行。其缺点是:①难以准确地模拟直升机主旋翼系统各种轴承真实的工况条件;②难以准确判断主旋翼系统中哪类或哪个轴承为最薄弱环节,导致直升机主旋翼系统轴承的定寿存在较大误差。出于安全考虑,一般将主旋翼系统轴承的服役寿命定的偏低,造成轴承使用上的浪费,同时增加了维修成本。The main rotor system of the helicopter is one of the core components of the helicopter. The connection between the moving components of the main rotor system is realized through various types of bearings (ball hinge bearings, carbide sleeve bearings and rolling bearings, etc.). In the past, the service life experiments of each bearing of the main rotor system were carried out on a fatigue testing machine with a single bearing. The disadvantages are: ① It is difficult to accurately simulate the real working conditions of various bearings of the helicopter main rotor system; ② It is difficult to accurately determine which type or which bearing in the main rotor system is the weakest link, resulting in the existence of fixed life of the helicopter main rotor system bearings. large error. For safety reasons, the service life of the bearing of the main rotor system is generally set low, which results in waste in the use of the bearing and increases the maintenance cost.
因此,研制直升机主旋翼系统配套组合轴承综合实验机是非常必要的。Therefore, it is very necessary to develop a comprehensive experimental machine with combined bearing for the main rotor system of the helicopter.
发明内容SUMMARY OF THE INVENTION
本发明的目的是提供一种摆动油缸加载式主旋翼球铰轴承综合试验机,以解决上述现有技术存在的问题,能准确模拟直升机主旋翼系统各类轴承的真实工况条件,能保证主旋翼系统各类轴承服役寿命的确定更精确、更客观。The purpose of the present invention is to provide a comprehensive testing machine for the main rotor ball hinge bearing loaded by a swing oil cylinder, so as to solve the problems existing in the above-mentioned prior art, to accurately simulate the real working conditions of various types of bearings of the main rotor system of a helicopter, and to ensure the main The determination of the service life of various bearings of the rotor system is more accurate and objective.
为实现上述目的,本发明提供了如下方案:本发明提供一种摆动油缸加载式主旋翼球铰轴承综合试验机,包括支承框架、传动主轴、驱动电机、液压旋转接头外壳、叶片式摆动油缸、液压阀站、旋翼平台和自动倾斜器;所述支承框架固定在地面上,所述支承框架上平台中部的中央孔内支承有所述传动主轴,所述驱动电机用于带动所述传动主轴旋转;所述传动主轴的下端固联所述旋翼平台,所述叶片式摆动油缸连接在所述旋翼平台的一侧,所述叶片式摆动油缸的旋转轴与旋翼平台的旋转轴成垂直状态;In order to achieve the above purpose, the present invention provides the following solutions: the present invention provides a comprehensive testing machine for swinging oil cylinder loaded main rotor ball hinge bearings, including a supporting frame, a transmission main shaft, a driving motor, a hydraulic rotary joint casing, a blade-type swinging oil cylinder, Hydraulic valve station, rotor platform and automatic tilter; the supporting frame is fixed on the ground, the transmission main shaft is supported in the central hole in the middle of the upper platform of the supporting frame, and the driving motor is used to drive the transmission main shaft to rotate The lower end of the transmission main shaft is fixedly connected to the rotor platform, the blade-type swinging oil cylinder is connected to one side of the rotor-wing platform, and the rotation axis of the blade-type swing oil cylinder is in a vertical state with the rotation axis of the rotor platform;
所述叶片式摆动油缸的输出轴与一个油缸摆杆的一端连接,所述油缸摆杆的另一端通过第七铰链与一变距拉杆的一端连接,所述变距拉杆的另一端通过第六铰链与所述自动倾斜器相连;所述旋翼平台的下部通过第八铰链连接有扭力臂摆杆I,所述扭力臂摆杆I还通过第九铰链连接有扭力臂摆杆II,所述扭力臂摆杆II通过第十铰链与所述自动倾斜器相连;所述支承框架上固定有中立柱,所述中立柱与所述自动倾斜器间隙配合;The output shaft of the vane-type swinging oil cylinder is connected to one end of a swing rod of an oil cylinder, the other end of the swing rod of the oil cylinder is connected to one end of a pitch-changing rod through a seventh hinge, and the other end of the pitch-changing rod passes through a sixth hinge. The hinge is connected with the automatic tilter; the lower part of the rotor platform is connected with a torsion arm swing rod I through the eighth hinge, and the torsion arm swing rod I is also connected with a torsion arm swing rod II through the ninth hinge. The arm swing rod II is connected with the automatic tilter through a tenth hinge; a neutral column is fixed on the support frame, and the neutral column is in clearance fit with the automatic tilter;
所述自动倾斜器的下方还通过第一铰链连接有防扭臂摆杆I,所述防扭臂摆杆I通过第二铰链连接防扭臂摆杆II,所述防扭臂摆杆II通过第三铰链与所述支承框架相连;所述自动倾斜器下方还固联有连接座,所述连接座通过第五铰链与一个助力油缸的活塞杆相连,所述助力油缸的缸体通过第四铰链与所述支承框架相连;The lower part of the automatic tilter is also connected with an anti-twist arm swing rod I through a first hinge, the anti-twist arm swing rod I is connected with an anti-torsion arm swing rod II through a second hinge, and the anti-torsion arm swing rod II is connected by a second hinge. The third hinge is connected with the support frame; a connecting seat is also fixedly connected below the automatic tilter, and the connecting seat is connected with the piston rod of a booster cylinder through the fifth hinge, and the cylinder body of the booster cylinder is connected by the fourth hinge. a hinge is connected to the support frame;
所述传动主轴的上部密封连接有一液压旋转接头外壳,所述传动主轴与所述液压旋转接头外壳转动配合,所述液压旋转接头外壳通过液压旋转接头固定架与支承框架固连;所述液压阀站通过第三高压软管、第四高压软管与所述传动主轴的内部液压油通道联通,所述叶片式摆动油缸通过第一高压软管、第二高压软管与所述传动主轴的内部液压油通道联通。The upper part of the transmission main shaft is sealed and connected with a hydraulic rotary joint casing, the transmission main shaft is rotatably matched with the hydraulic rotary joint casing, and the hydraulic rotary joint casing is fixedly connected with the support frame through the hydraulic rotary joint fixing frame; the hydraulic valve The station communicates with the internal hydraulic oil channel of the transmission main shaft through the third high-pressure hose and the fourth high-pressure hose, and the vane-type swing oil cylinder is connected to the inner part of the transmission main shaft through the first high-pressure hose and the second high-pressure hose. The hydraulic oil channel is connected.
优选的,所述支承框架上平台中部的中央孔内通过第一双列轴承和第二双列轴承支承所述传动主轴。Preferably, the transmission main shaft is supported by the first double row bearing and the second double row bearing in the central hole in the middle of the upper platform of the support frame.
优选的,所述传动主轴上固联一个大圆锥齿轮,所述驱动电机与一主减速器固联,所述主减速器的输出轴上固联有一驱动轴,所述驱动轴通过第三双列轴承与所述支承框架连接,所述驱动轴的端部固定有与所述大圆锥齿轮啮合的小圆锥齿轮。Preferably, a large bevel gear is fixedly connected to the transmission main shaft, the drive motor is fixedly connected to a main reducer, and a drive shaft is fixedly connected to the output shaft of the main reducer, and the drive shaft passes through the third double gear. The row bearing is connected with the support frame, and the end of the drive shaft is fixed with a small bevel gear that meshes with the large bevel gear.
优选的,所述变距拉杆由两段构成,两段所述变距拉杆由一个拉压力传感器固连在一起。Preferably, the variable pitch rod is composed of two sections, and the two sections of the variable pitch rod are connected together by a tension pressure sensor.
优选的,所述自动倾斜器包括由外向内依次设置的旋转环、不旋转环、大球铰轴承外环和大球铰轴承内环,所述大球铰轴承内环与所述中立柱间隙配合,所述大球铰轴承外环位于所述大球铰轴承内环的外侧,所述不旋转环与所述大球铰轴承外环固联,所述旋转环通过双列薄壁轴承与所述不旋转环连接。Preferably, the automatic tilter includes a rotating ring, a non-rotating ring, a large ball hinge bearing outer ring, and a large ball hinge bearing inner ring, which are sequentially arranged from the outside to the inside, and the large ball hinge bearing inner ring has a gap between the center column. Matching, the outer ring of the large ball hinge bearing is located on the outside of the inner ring of the large ball hinge bearing, the non-rotating ring is fixedly connected with the outer ring of the large ball hinge bearing, and the rotating ring is connected with the double-row thin-walled bearing. The non-rotating ring connection.
优选的,所述变距拉杆通过所述第六铰链与所述旋转环相连,所述扭力臂摆杆II通过所述第十铰链与所述旋转环相连;所述防扭臂摆杆I通过所述第一铰链与所述不旋转环相连,所述连接座与所述不旋转环固联。Preferably, the variable pitch rod is connected with the rotating ring through the sixth hinge, the torsion arm swing rod II is connected with the rotating ring through the tenth hinge; the anti-torsion arm swing rod I is connected with the rotating ring through the tenth hinge The first hinge is connected with the non-rotating ring, and the connecting seat is fixedly connected with the non-rotating ring.
优选的,所述第一铰链、第二铰链、第三铰链、第八铰链、第九铰链和第十铰链均为柱铰。Preferably, the first hinge, the second hinge, the third hinge, the eighth hinge, the ninth hinge and the tenth hinge are all column hinges.
优选的,所述第四铰链、第五铰链、第六铰链和第七铰链均为球铰。Preferably, the fourth hinge, the fifth hinge, the sixth hinge and the seventh hinge are all spherical hinges.
优选的,所述液压阀站包括油箱,所述油箱通过第一油管与所述第三高压软管连通,所述油箱通过第二油管与所述第四高压软管连通。Preferably, the hydraulic valve station includes an oil tank, the oil tank communicates with the third high pressure hose through a first oil pipe, and the oil tank communicates with the fourth high pressure hose through a second oil pipe.
优选的,所述第一油管与所述第三高压软管的连接处并联设置有第一伺服阀和第一单向阀,所述第二油管与所述第四高压软管的连接处并联设置有第二伺服阀和第二单向阀。Preferably, a first servo valve and a first check valve are arranged in parallel at the connection between the first oil pipe and the third high-pressure hose, and the second oil pipe is connected in parallel with the fourth high-pressure hose. A second servo valve and a second one-way valve are provided.
本发明相对于现有技术取得了以下技术效果:The present invention has achieved the following technical effects with respect to the prior art:
1)该发明的加载过程与直升机主旋翼系统的载荷同相位、同频率,能真实模拟直升机主旋翼系统的载荷状态;1) The loading process of the invention is in the same phase and frequency as the load of the helicopter main rotor system, which can truly simulate the load state of the helicopter main rotor system;
2)能实现交变载荷、脉动载荷和恒定载荷的加载。2) It can realize the loading of alternating load, pulsating load and constant load.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the accompanying drawings required in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some of the present invention. In the embodiments, for those of ordinary skill in the art, other drawings can also be obtained according to these drawings without any creative effort.
图1为本发明摆动油缸加载式主旋翼球铰轴承综合试验机示意图;Fig. 1 is the schematic diagram of the comprehensive testing machine of the swing cylinder loaded main rotor ball hinge bearing of the present invention;
图2为本发明液压阀站原理示意图;Fig. 2 is the principle schematic diagram of the hydraulic valve station of the present invention;
图3为本发明叶片式摆动油缸工作原理示意图;Fig. 3 is the schematic diagram of the working principle of the vane type swing oil cylinder of the present invention;
其中,1.第一铰链,2.第二铰链,3.防扭臂摆杆II,4.第三铰链,5.防扭臂摆杆I,6.中立柱,7.支承框架,8.大球铰轴承内环,9.大球铰轴承外环,10.第四铰链,11.助力油缸,12.第五铰链,13.连接座,14.第六铰链,15.变距拉杆,16.油缸摆杆,17.第七铰链,18.叶片式摆动油缸,19.定子,20.叶片,21.第一高压软管,22.小圆锥齿轮,23.驱动轴,24.驱动电机,25.主减速器,26.第一双列轴承,27.液压阀站,28.第三高压软管,29.第四高压软管,30.液压旋转接头外壳,31.液压旋转接头固定架,32.第二双列轴承,33.大圆锥齿轮,34.第三双列轴承,35.第二高压软管,36.传动主轴,37.旋翼平台,38.第八铰链,39.扭力臂摆杆I,40.第九铰链,41.扭力臂摆杆II,42.第十铰链,43.旋转环,44.双列薄壁轴承,45.不旋转环,46.挡块,47.拉压力传感器,48.油口,49.第一单向阀,50.第一伺服阀,51.第一油管,52.油箱,53.第二油管,54.第二伺服阀,55.第二单向阀,52.油箱。Among them, 1. the first hinge, 2. the second hinge, 3. the anti-torsion arm swing rod II, 4. the third hinge, 5. the anti-torsion arm swing rod I, 6. the center column, 7. the supporting frame, 8. Large ball hinge bearing inner ring, 9. Large ball hinge bearing outer ring, 10. Fourth hinge, 11. Power cylinder, 12. Fifth hinge, 13. Connecting seat, 14. Sixth hinge, 15. Variable pitch rod, 16. Cylinder swing rod, 17. Seventh hinge, 18. Vane swing cylinder, 19. Stator, 20. Vane, 21. First high pressure hose, 22. Small bevel gear, 23. Drive shaft, 24. Drive motor , 25. Main reducer, 26. First double row bearing, 27. Hydraulic valve station, 28. Third high pressure hose, 29. Fourth high pressure hose, 30. Hydraulic rotary joint housing, 31. Hydraulic rotary joint fixed Frame, 32. Second double row bearing, 33. Large bevel gear, 34. Third double row bearing, 35. Second high pressure hose, 36. Transmission main shaft, 37. Rotor platform, 38. Eighth hinge, 39. Torsion arm swing rod I, 40. Ninth hinge, 41. Torsion arm swing rod II, 42. Tenth hinge, 43. Rotating ring, 44. Double row thin-wall bearing, 45. Non-rotating ring, 46. Stopper, 47. Pull pressure sensor, 48. Oil port, 49. First check valve, 50. First servo valve, 51. First oil pipe, 52. Oil tank, 53. Second oil pipe, 54. Second servo valve, 55 . Second check valve, 52. Fuel tank.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
本发明的目的是提供一种摆动油缸加载式主旋翼球铰轴承综合试验机,以解决上述现有技术存在的问题,能准确模拟直升机主旋翼系统各类轴承的真实工况条件,能保证主旋翼系统各类轴承服役寿命的确定更精确、更客观。The purpose of the present invention is to provide a comprehensive testing machine for the main rotor ball hinge bearing loaded by a swing oil cylinder, so as to solve the problems existing in the above-mentioned prior art, to accurately simulate the real working conditions of various types of bearings of the main rotor system of a helicopter, and to ensure the main The determination of the service life of various bearings of the rotor system is more accurate and objective.
为使本发明的上述目的、特征和优点能够更加明显易懂,下面结合附图和具体实施方式对本发明作进一步详细的说明。In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments.
实施例Example
如图1所示,本实施例提供一种摆动油缸加载式主旋翼球铰轴承综合试验机,包括支承框架、传动主轴、驱动电机、液压旋转接头外壳、叶片式摆动油缸、液压阀站、旋翼平台和自动倾斜器;支承框架7固定在地面上,在支承框架7上的平台中部设置有中央空孔,中央孔内通过上下设置的一对第一双列轴承32和一对第二双列轴承34支承传动主轴36。驱动电机用于带动传动主轴旋转,具体的,传动主轴36上固联一个大圆锥齿轮33,与大圆锥齿轮33垂直啮合的小圆锥齿轮22固定在驱动轴23上,驱动轴23与主减速器25的输出轴固联,驱动电机24与主减速器25固联,驱动电机24通过主减速器25、驱动轴23、小圆锥齿轮22、大圆锥齿轮33带动传动主轴36旋转,传动主轴36下端固联旋翼平台37。As shown in FIG. 1, this embodiment provides a comprehensive testing machine for swinging cylinder-loaded main rotor ball hinge bearings, including a support frame, a drive spindle, a drive motor, a hydraulic rotary joint shell, a blade-type swinging cylinder, a hydraulic valve station, and a rotor. Platform and automatic tilting device; the supporting frame 7 is fixed on the ground, and a central hollow hole is arranged in the middle of the platform on the supporting frame 7, and a pair of first double row bearings 32 and a pair of second double row bearings arranged up and down pass through the central hole. Bearings 34 support drive shaft 36 . The drive motor is used to drive the transmission main shaft to rotate. Specifically, a large bevel gear 33 is fixedly connected to the transmission main shaft 36, and a small bevel gear 22 vertically meshed with the large bevel gear 33 is fixed on the drive shaft 23. The drive shaft 23 is connected to the main reducer. The output shaft of 25 is fixedly connected, and the driving motor 24 is fixedly connected with the main reducer 25. The driving motor 24 drives the transmission main shaft 36 to rotate through the main reducer 25, the driving shaft 23, the small bevel gear 22 and the large bevel gear 33, and the lower end of the transmission main shaft 36 rotates. Fixed-wing rotor platform 37.
叶片式摆动油缸18连接在旋翼平台37的一侧,叶片式摆动油缸18的旋转轴与旋翼平台37的旋转轴在空间成垂直状态,油缸摆杆16的一端固连在叶片式摆动油缸18的输出轴上,油缸摆杆16的另一端通过第七铰链17与变距拉杆15的一端相连,变距拉杆15的另一端通过第六铰链14与自动倾斜器的旋转环43相连;其中变距拉杆15由两段构成,两段变距拉杆由一个拉压力传感器47固连在一起。在旋翼平台37的下部通过第八铰链38与扭力臂摆杆I39相连,扭力臂摆杆I39与扭力臂摆杆II41之间通过第九铰链40连接,扭力臂摆杆II41通过第十铰链42与自动倾斜器的旋转环43相连。The vane type swing cylinder 18 is connected to one side of the rotor platform 37 , the rotation axis of the blade type swing cylinder 18 and the rotation axis of the rotor platform 37 are in a vertical state in space, and one end of the cylinder swing rod 16 is fixedly connected to the blade type swing cylinder 18 . On the output shaft, the other end of the oil cylinder swing rod 16 is connected to one end of the pitch-changing pull rod 15 through the seventh hinge 17, and the other end of the pitch-changing pull rod 15 is connected to the rotating ring 43 of the automatic tilter through the sixth hinge 14; The pull rod 15 is composed of two sections, and the two sections of the pull rod with variable pitch are connected together by a tension pressure sensor 47 . The lower part of the rotor platform 37 is connected with the torsion arm swing rod I39 through the eighth hinge 38 , the torsion arm swing rod I39 and the torsion arm swing rod II41 are connected through the ninth hinge 40 , and the torsion arm swing rod II41 is connected with the tenth hinge 42 through the ninth hinge 40 . The rotating ring 43 of the automatic tilter is connected.
自动倾斜器的旋转环43与不旋转环45之间通过双列薄壁轴承44连接在一起,不旋转环45与大球铰轴承外环9固联,大球铰轴承内环8与中立柱6为间隙配合,中立柱6固定在支承框架7上。The rotating ring 43 and the non-rotating ring 45 of the automatic tilter are connected together by a double-row thin-walled bearing 44, the non-rotating ring 45 is fixedly connected with the outer ring 9 of the large ball hinge bearing, and the inner ring 8 of the large ball hinge bearing is connected with the center column 6 is a clearance fit, and the center column 6 is fixed on the supporting frame 7 .
防扭臂摆杆I5通过第一铰链1与自动倾斜器的不旋转环45相连,防扭臂摆杆I5与防扭臂摆杆II3通过第二铰链2连接,防扭臂摆杆II3通过第三铰链4与支承框架7相连。连接座13与自动倾斜器不旋转环45的下方固联,连接座13通过第五铰链12与助力油缸11的活塞杆相连,助力油缸11的缸体通过第四铰链10与支承框架7相连,传动主轴36的上部与一个液压旋转接头外壳30构成带密封的转动配合,液压旋转接头外壳30通过液压旋转接头固定架31与支承框架7固连。The anti-twist arm swing rod I5 is connected with the non-rotating ring 45 of the automatic tilter through the first hinge 1, the anti-torsion arm swing rod I5 is connected with the anti-torsion arm swing rod II3 through the second hinge 2, and the anti-torsion arm swing rod II3 passes through the first hinge. The three hinges 4 are connected to the support frame 7 . The connecting seat 13 is fixedly connected with the lower part of the non-rotating ring 45 of the automatic tilter, the connecting seat 13 is connected with the piston rod of the booster cylinder 11 through the fifth hinge 12, and the cylinder block of the booster cylinder 11 is connected with the support frame 7 through the fourth hinge 10, The upper part of the transmission main shaft 36 forms a sealed rotation fit with a hydraulic rotary joint housing 30 , and the hydraulic rotary joint housing 30 is fixedly connected with the support frame 7 through the hydraulic rotary joint fixing frame 31 .
液压阀站27通过第三高压软管28、第四高压软管29、液压旋转接头外壳30与传动主轴36的内部液压油通道联通,叶片式摆动油缸18通过第一高压软管21、第二高压软管35与传动主轴36的内部液压油通道联通。The hydraulic valve station 27 communicates with the internal hydraulic oil channel of the transmission main shaft 36 through the third high pressure hose 28, the fourth high pressure hose 29 and the hydraulic rotary joint housing 30, and the vane type swing cylinder 18 passes through the first high pressure hose 21, the second The high pressure hose 35 communicates with the internal hydraulic oil passage of the transmission spindle 36 .
本实施例中第一铰链1、第二铰链2、第三铰链4、第八铰链38、第九铰链40和第十铰链42均为柱铰,即被连接的两构件只能绕铰链轴线相对转动,而不能有其他形式的相对运动;这些柱铰均为被试轴承。第四铰链10、第五铰链12、第六铰链14和第七铰链17均为球铰,即被连接的两构件间能绕三个坐标轴方向相对转动,但不能相对移动,这些球铰均为被试轴承。In this embodiment, the first hinge 1 , the second hinge 2 , the third hinge 4 , the eighth hinge 38 , the ninth hinge 40 and the tenth hinge 42 are all column hinges, that is, the two connected members can only face each other around the hinge axis Rotation, but no other form of relative motion; these column hinges are tested bearings. The fourth hinge 10, the fifth hinge 12, the sixth hinge 14 and the seventh hinge 17 are all spherical hinges, that is, the two connected components can rotate relative to each other around the three coordinate axes, but cannot move relative to each other. for the tested bearing.
如图2所示,本实施例中液压阀站27包括油箱52,油箱通过第一油管51与第三高压软管28连通,油箱通过第二油管53与第四高压软管29连通。第一油管51与第三高压软管28的连接处并联设置有第一伺服阀50和第一单向阀49,第二油管53与第四高压软管29的连接处并联设置有第二伺服阀54和第二单向阀55。As shown in FIG. 2 , in this embodiment, the hydraulic valve station 27 includes an oil tank 52 , which is communicated with the third high pressure hose 28 through a first oil pipe 51 , and communicated with the fourth high pressure hose 29 through a second oil pipe 53 . A first servo valve 50 and a first check valve 49 are arranged in parallel at the connection between the first oil pipe 51 and the third high pressure hose 28 , and a second servo valve is arranged in parallel at the connection between the second oil pipe 53 and the fourth high pressure hose 29 . valve 54 and second one-way valve 55 .
本发明的工作过程如下:驱动电机24通过主减速器25、驱动轴23、小圆锥齿轮22、大圆锥齿轮33、传动主轴36带动旋翼平台37和与之相连的叶片式摆动油缸18、第一高压软管21、第二高压软管35同步旋转,旋翼平台37通过第八铰链38、扭力臂摆杆I39、第九铰链40、扭力臂摆杆II41、第十铰链42带动自动倾斜器的旋转环43旋转,旋翼平台37与自动倾斜器旋转环43的旋转通过第六铰链14带动变距拉杆15、拉压力传感器47、第七铰链17同步旋转。The working process of the present invention is as follows: the drive motor 24 drives the rotor platform 37 and the blade-type swing cylinder 18 connected to it through the main reducer 25, the drive shaft 23, the small bevel gear 22, the large bevel gear 33, and the transmission main shaft 36. The high-pressure hose 21 and the second high-pressure hose 35 rotate synchronously, and the rotor platform 37 drives the rotation of the automatic tilter through the eighth hinge 38, the torsion arm swing rod I39, the ninth hinge 40, the torsion arm swing rod II41, and the tenth hinge 42 The ring 43 rotates, and the rotation of the rotor platform 37 and the rotation ring 43 of the automatic tilter drives the pitch change rod 15 , the pull pressure sensor 47 and the seventh hinge 17 to rotate synchronously through the sixth hinge 14 .
在试验机旋转运动的同时,助力油缸11活塞杆作上下往复运动,通过第五铰链12、连接座13带动自动倾斜器不旋转环45、双列薄壁轴承44、旋转环43、大球铰轴承外环9往复摆动。自动倾斜器旋转环43的往复摆动通过第六铰链14、变距拉杆15、拉压力传感器47、第七铰链17、油缸摆杆16带动叶片式摆动油缸18的叶片20往复摆动。While the testing machine rotates, the piston rod of the booster cylinder 11 reciprocates up and down, and drives the automatic tilter through the fifth hinge 12 and the connecting seat 13 to drive the non-rotating ring 45, the double-row thin-wall bearing 44, the rotating ring 43, and the large ball hinge. The bearing outer ring 9 swings back and forth. The reciprocating swing of the automatic tilter rotating ring 43 drives the vane 20 of the vane swing cylinder 18 to swing back and forth through the sixth hinge 14 , the pitch rod 15 , the tension pressure sensor 47 , the seventh hinge 17 , and the cylinder swing rod 16 .
当叶片式摆动油缸18的叶片20逆时针(按图3所示方位)摆动时,油箱52中的油液通过第二油管53、第二单向阀55、第四高压软管29、液压旋转接头外壳30、传动主轴36的内部液压油通道、第二高压软管35、左侧的油口48被吸入叶片式摆动油缸18的左腔,而与叶片式摆动油缸18右腔相联通的第一单向阀49处于关闭状态,叶片式摆动油缸18右腔中的油液只能通过第一高压软管21、传动主轴36的内部液压油通道、液压旋转接头外壳30、第三高压软管28、第一伺服阀50进入油箱52,通过控制第一伺服阀50阀口大小就可控制叶片式摆动油缸18的载荷。When the vane 20 of the vane-type swing cylinder 18 swings counterclockwise (in the orientation shown in FIG. 3 ), the oil in the oil tank 52 passes through the second oil pipe 53 , the second check valve 55 , the fourth high-pressure hose 29 , the hydraulic rotation The joint housing 30 , the internal hydraulic oil passage of the transmission main shaft 36 , the second high pressure hose 35 , and the oil port 48 on the left side are sucked into the left cavity of the vane type swing cylinder 18 A one-way valve 49 is in a closed state, and the oil in the right chamber of the vane swing cylinder 18 can only pass through the first high pressure hose 21, the internal hydraulic oil passage of the transmission spindle 36, the hydraulic rotary joint housing 30, and the third high pressure hose. 28. The first servo valve 50 enters the oil tank 52, and the load of the vane-type swing oil cylinder 18 can be controlled by controlling the size of the valve port of the first servo valve 50.
当叶片式摆动油缸18的叶片顺时针(按图3所示方位)摆动时,油箱52中的油液通过第一油管51、第一单向阀49、第三高压软管28、液压旋转接头外壳30、传动主轴36的内部液压油通道、第一高压软管21被吸入叶片式摆动油缸18的右腔,而与叶片式摆动油缸18左腔相联通的第二单向阀55处于关闭状态,叶片式摆动油缸18左腔中的油液只能通过第二高压软管35、传动主轴36的内部液压油通道、液压旋转接头外壳30、第四高压软管29、第二伺服阀54进入油箱,通过控制第二伺服阀54阀口大小就可控制加载油缸的载荷。When the vane of the vane-type swinging oil cylinder 18 swings clockwise (in the orientation shown in FIG. 3 ), the oil in the oil tank 52 passes through the first oil pipe 51 , the first check valve 49 , the third high-pressure hose 28 , and the hydraulic rotary joint The casing 30 , the internal hydraulic oil passage of the transmission main shaft 36 , and the first high-pressure hose 21 are sucked into the right chamber of the vane swing cylinder 18 , while the second check valve 55 communicating with the left chamber of the vane swing cylinder 18 is in a closed state. , the oil in the left cavity of the vane type swing cylinder 18 can only enter through the second high pressure hose 35 , the internal hydraulic oil passage of the transmission spindle 36 , the hydraulic rotary joint housing 30 , the fourth high pressure hose 29 and the second servo valve 54 For the oil tank, the load of the loading oil cylinder can be controlled by controlling the size of the valve port of the second servo valve 54 .
本发明中应用了具体个例对本发明的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本发明的方法及其核心思想;同时,对于本领域的一般技术人员,依据本发明的思想,在具体实施方式及应用范围上均会有改变之处。综上所述,本说明书内容不应理解为对本发明的限制。In the present invention, specific examples are used to illustrate the principles and implementations of the present invention, and the descriptions of the above embodiments are only used to help understand the method and the core idea of the present invention; There will be changes in the specific implementation manner and application scope of the idea of the invention. In conclusion, the contents of this specification should not be construed as limiting the present invention.
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4089211A (en) * | 1976-11-01 | 1978-05-16 | United Technologies Corporation | Elastomeric bearing test machine |
CN1818598A (en) * | 2006-03-17 | 2006-08-16 | 燕山大学 | Externally swing joint-bearing fatigue experimental apparatus of automatic rotor oblique device for helicopter |
CN2876754Y (en) * | 2006-03-17 | 2007-03-07 | 燕山大学 | Internal oscillation type fatique tester for joint bearing of automatic clinometer of helicopter rotary swing |
CN201247149Y (en) * | 2008-09-01 | 2009-05-27 | 洛阳工铭机电设备有限公司 | Intelligent detection analytical apparatus for large-sized thin-wall bearing of helicopter rotor control assembly |
CN104344954A (en) * | 2014-10-28 | 2015-02-11 | 燕山大学 | Fatigue test machine for self lubricating joint bearing in flexible propeller hub rotor wing |
CN104729846A (en) * | 2015-04-07 | 2015-06-24 | 中国直升机设计研究所 | Automatic inclinator nonrotating ring fatigue test device |
CN106768920A (en) * | 2016-11-29 | 2017-05-31 | 中国直升机设计研究所 | A kind of fatigue experimental device |
-
2018
- 2018-10-31 CN CN201811282484.8A patent/CN109187019B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4089211A (en) * | 1976-11-01 | 1978-05-16 | United Technologies Corporation | Elastomeric bearing test machine |
CN1818598A (en) * | 2006-03-17 | 2006-08-16 | 燕山大学 | Externally swing joint-bearing fatigue experimental apparatus of automatic rotor oblique device for helicopter |
CN2876754Y (en) * | 2006-03-17 | 2007-03-07 | 燕山大学 | Internal oscillation type fatique tester for joint bearing of automatic clinometer of helicopter rotary swing |
CN201247149Y (en) * | 2008-09-01 | 2009-05-27 | 洛阳工铭机电设备有限公司 | Intelligent detection analytical apparatus for large-sized thin-wall bearing of helicopter rotor control assembly |
CN104344954A (en) * | 2014-10-28 | 2015-02-11 | 燕山大学 | Fatigue test machine for self lubricating joint bearing in flexible propeller hub rotor wing |
CN104729846A (en) * | 2015-04-07 | 2015-06-24 | 中国直升机设计研究所 | Automatic inclinator nonrotating ring fatigue test device |
CN106768920A (en) * | 2016-11-29 | 2017-05-31 | 中国直升机设计研究所 | A kind of fatigue experimental device |
Non-Patent Citations (1)
Title |
---|
"直升机旋翼系统弹性轴承刚度特性试验方法研究";黄晓东 等;《机械强度》;20120228;第34卷(第2期);第270-273页 |
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