CN202939030U - Closed axial loading test apparatus of helical gear thrust cone balancing device - Google Patents

Closed axial loading test apparatus of helical gear thrust cone balancing device Download PDF

Info

Publication number
CN202939030U
CN202939030U CN 201220706306 CN201220706306U CN202939030U CN 202939030 U CN202939030 U CN 202939030U CN 201220706306 CN201220706306 CN 201220706306 CN 201220706306 U CN201220706306 U CN 201220706306U CN 202939030 U CN202939030 U CN 202939030U
Authority
CN
China
Prior art keywords
gear
loader
thrust
output shaft
axial
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.)
Expired - Fee Related
Application number
CN 201220706306
Other languages
Chinese (zh)
Inventor
于东洋
叶盛鉴
赵勇
刘永恒
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.)
703th Research Institute of CSIC
Original Assignee
703th Research Institute of CSIC
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 703th Research Institute of CSIC filed Critical 703th Research Institute of CSIC
Priority to CN 201220706306 priority Critical patent/CN202939030U/en
Application granted granted Critical
Publication of CN202939030U publication Critical patent/CN202939030U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Abstract

The utility model discloses a closed axial loading test apparatus of a helical gear thrust cone balancing device. The apparatus comprises a motor, a test gear box comprising an input shaft and an output gear, an accompanied test gear box comprising the input shaft and the output gear, a coupling, a torque loader and a hydraulic axial thrust loader. The axial thrust loader is mainly formed by an outer sheath of the loader, box bodies and a rolling bearing. During the test, the motor is started so that gear apparatuses in the two box bodies carry out transmission and simultaneously the loader is used to generate a pair of relative torques to end portions of output shafts in the two box bodies. At this time, an elastic shaft and other parts generate elastic torsion and torsional deformation is generated. The accompanied test gear box and the test gear box transmit the torque so as to realize power enclosing. Pressure oil is entered into an oil chamber through an oil inlet channel. A mechanical sealing ring and a rotation sealing ring make the pressure oil do not leak from a joint so that two shaft ends generate the thrust and axial loading is realized to be performed on the thrust cone.

Description

The closed axial load testing machine of a kind of spiral gear thrust cone balance device
Technical field:
The utility model belongs to a kind of test unit of testing thrust balancing device usability used in screw-wheel gearing, is specifically related to the closed axial load testing machine of a kind of spiral gear thrust cone balance device.
Background technology:
Thrust balancing device is widely used in cogwheel gearing, is mainly used to transmit, bear the axial thrust that the gear engagement produces, and present thrust balancing device mainly comprises thrust cone balance device and thrust bearing.For the thrust bearing test, because the thrust cone balance device is relatively less in the application of engineering field, so about the test unit of test thrust cone balance device properties also seldom, the charger of existing test unit about in this respect is all open, it exists, and size is large, weight is large, complex structure, load unsettled problem, and be difficult to satisfy the testing requirements of high speed thrust cone device, its application all has certain limitation, is restricting the development of thrust load testing machine.
The utility model content:
The purpose of this utility model is to provide the closed axial load testing machine of a kind of spiral gear thrust cone balance device, and its thrust charger volume is little, lightweight, simple in structure, loading is stable, has improved the test reliability of thrust cone balance device.
the purpose of this utility model is achieved in the following ways: the closed axial load testing machine of this spiral gear thrust cone balance device, comprise motor, the test gear case, accompany the examination gear case, shaft coupling, torque loader, the axial thrust loader, motor connects by the primary input axial at shaft coupling one-level input gear place in gear case with test, primary input axial is connected with the secondary input shaft of accompanying the secondary input gear place of examination in gear case by torque loader, one-level input gear and the one-level output gear engagement of testing in gear case, secondary input gear and the secondary output gear engagement of accompanying in the examination gear case, the both sides of one-level output gear and secondary output gear are equipped with the thrust cone for balancing axial thrust, the bevelling, inside edge of thrust cone forms the conical surface, be respectively equipped with the conical surface matching surface that the conical surface with thrust cone matches respectively with on the one-level input gear of both engagements and the both sides of the edge of secondary input gear, be provided with the axial thrust loader between the secondary output shaft at the one-level output shaft at one-level output gear place and secondary output gear place, described axial thrust loader comprises casing, the loader overcoat, rolling bearing, the loader overcoat is connected with the secondary output shaft with the one-level output shaft by connecting spline, the loader overcoat by rolling bearing by case supports, the center of loader overcoat is provided with oil pocket, oil pocket is between one-level output shaft and secondary output shaft, the top of loader overcoat is provided with the oil inlet passage that is communicated with oil pocket, oil inlet passage stretches out and runs through oil pocket, the contact position of loader overcoat and casing is provided with rotating seal ring.
Preferably, described loader overcoat is provided with mechanical seal ring respectively and between one-level output shaft and secondary output shaft.
The beneficial effects of the utility model are: the closed axial load testing machine of this spiral gear thrust cone balance device, the parts such as the axial thrust charger by arranging, torque loader, make this test unit not only can realize the sealing of torsion pass power, solved simultaneously the problem that test unit axially loads, its thrust charger volume is little, lightweight, simple in structure, loading is stable, has improved the test reliability of thrust cone balance device.
Description of drawings:
Fig. 1 is one-piece construction schematic diagram of the present utility model.
Fig. 2 is the structural representation of axial thrust charger of the present utility model.
Embodiment:
Be described further below in conjunction with accompanying drawing 1 and 2 pairs of embodiments of the present utility model of accompanying drawing.
the closed axial load testing machine of this spiral gear thrust cone balance device, comprise motor 1, test gear case 2, accompany examination gear case 3, shaft coupling 4, torque loader 5, axial thrust loader 6, motor 1 connects by the primary input axial 11 at interior one-level input gear 7 places of shaft coupling 4 and test gear case 2, primary input axial 11 is connected with the secondary input shaft 12 at secondary input gear 8 places in accompanying examination gear case 3 by torque loader 5, one-level input gear 7 and one-level output gear 9 engagements of testing in gear case 2, secondary input gear 8 and secondary output gear 10 engagements of accompanying in examination gear case 3, the both sides of one-level output gear 9 and secondary output gear 10 are equipped with the thrust cone 15 for balancing axial thrust, the bevelling, inside edge of thrust cone 15 forms the conical surface, be respectively equipped with the conical surface matching surface that the conical surface with thrust cone 15 matches respectively with on the one-level input gear 7 of both engagements and the both sides of the edge of secondary input gear 8, be provided with axial thrust loader 6 between the secondary output shaft 14 at the one-level output shaft 13 at one-level output gear 9 places and secondary output gear 10 places, described axial thrust loader 6 comprises casing 6-1, loader overcoat 6-2, rolling bearing 6-3, loader overcoat 6-2 is connected with secondary output shaft 14 with one-level output shaft 13 by connecting spline, loader overcoat 6-2 is supported by casing 6-1 by rolling bearing 6-3, the center of loader overcoat 6-2 is provided with oil pocket 6-4, oil pocket 6-4 is between one-level output shaft 13 and secondary output shaft 14, the top of loader overcoat 6-2 is provided with the oil inlet passage 6-5 that is communicated with oil pocket 6-4, oil inlet passage 6-5 stretches out and runs through oil pocket 6-4, the contact position of loader overcoat 6-2 and casing 6-1 is provided with rotating seal ring 6-6.Described loader overcoat is provided with mechanical seal ring 6-7 respectively and between one-level output shaft 13 and secondary output shaft 14.
Axial thrust loader 6 in the utility model be respectively with the test gear case 2 one-level output shaft 13 and accompany the examination gear case 3 secondary output shaft 14 be connected, can realize that the thrust cone 15 that one-level output gear 9 and secondary output gear 10 both sides arrange is respectively carried out axial thrust to be loaded, the pressure oil of the main outer section of its thrust is controlled, can be according to different demands to the test unit applied thrust, under different thrusts to the usability research experiment of thrust cone.
during test run, starter motor 1, make test gear case 2 and accompany the cogwheel gearing in examination gear case 3 to begin to carry out gear drive, apply a pair of relative moment of torsion by axial thrust loader 6 to one-level output shaft 13 and secondary output shaft 14 simultaneously, this moment, one-level output shaft 13 and secondary output shaft 14 and other parts produced the elastic torsion distortion, test gear case 2 tries all transmitting torques of gear case 3 with accompanying like this, realize the power sealing, its detailed process is: external pressure oil enters oil pocket 6-4 by oil inlet passage 6-5, rotating seal ring 6-6 and mechanical seal ring 6-7 form the oil pocket of sealing, make pressure oil can not reveal from the junction, outside pressure oil forms thrust, thereby make the two axial ends of one-level output shaft 13 and secondary output shaft 14 produce thrust, realization is carried out the loading of axial thrust to thrust cone 15.Draw the various performance parameters of thrust cone 15 by loading experiment, as temperature, fastness to rubbing etc., lubricity etc., for the later stage equipment Design provides reference frame.

Claims (2)

1. closed axial load testing machine of spiral gear thrust cone balance device, it is characterized in that: comprise motor (1), test gear case (2), accompany examination gear case (3), shaft coupling (4), torque loader (5), axial thrust loader (6), motor (1) connects by the primary input axial (11) at interior one-level input gear (7) place of shaft coupling (4) and test gear case (2), primary input axial (11) is connected with the secondary input shaft (12) at secondary input gear (8) place in accompanying examination gear case (3) by torque loader (5), one-level input gear (7) and one-level output gear (9) engagement of testing in gear case (2), secondary input gear (8) and secondary output gear (10) engagement of accompanying in examination gear case (3), the both sides of one-level output gear (9) and secondary output gear (10) are equipped with the thrust cone (15) for balancing axial thrust, the bevelling, inside edge of thrust cone (15) forms the conical surface, be respectively equipped with the conical surface matching surface that the conical surface with thrust cone (15) matches respectively with on the one-level input gear (7) of both engagements and the both sides of the edge of secondary input gear (8), be provided with axial thrust loader (6) between the secondary output shaft (14) at the one-level output shaft (13) at one-level output gear (9) place and secondary output gear (10) place, described axial thrust loader (6) comprises casing (6-1), loader overcoat (6-2), rolling bearing (6-3), loader overcoat (6-2) is connected with secondary output shaft (14) with one-level output shaft (13) by connecting spline, loader overcoat (6-2) is supported by casing (6-1) by rolling bearing (6-3), the center of loader overcoat (6-2) is provided with oil pocket (6-4), oil pocket (6-4) is between one-level output shaft (13) and secondary output shaft (14), the top of loader overcoat (6-2) is provided with the oil inlet passage (6-5) that is communicated with oil pocket (6-4), oil inlet passage (6-5) stretches out and runs through oil pocket (6-4), loader overcoat (6-2) is provided with rotating seal ring (6-6) with the contact position of casing (6-1).
2. the closed axial load testing machine of a kind of spiral gear thrust cone balance device as claimed in claim 1, it is characterized in that: described loader overcoat is provided with mechanical seal ring (6-7) respectively and between one-level output shaft (13) and secondary output shaft (14).
CN 201220706306 2012-12-20 2012-12-20 Closed axial loading test apparatus of helical gear thrust cone balancing device Expired - Fee Related CN202939030U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220706306 CN202939030U (en) 2012-12-20 2012-12-20 Closed axial loading test apparatus of helical gear thrust cone balancing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220706306 CN202939030U (en) 2012-12-20 2012-12-20 Closed axial loading test apparatus of helical gear thrust cone balancing device

Publications (1)

Publication Number Publication Date
CN202939030U true CN202939030U (en) 2013-05-15

Family

ID=48323263

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220706306 Expired - Fee Related CN202939030U (en) 2012-12-20 2012-12-20 Closed axial loading test apparatus of helical gear thrust cone balancing device

Country Status (1)

Country Link
CN (1) CN202939030U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103018042A (en) * 2012-12-20 2013-04-03 中国船舶重工集团公司第七�三研究所 Closed type axial loading testing apparatus of bevel wheel thrust cone balancing device
CN106840655A (en) * 2017-02-10 2017-06-13 中国航发沈阳发动机研究所 A kind of spiral bevel gear tooth root fatigue experimental device
CN109141874A (en) * 2018-09-29 2019-01-04 济南大学 A kind of Power close type herringbone bear experimental rig
CN109752182A (en) * 2019-01-30 2019-05-14 中国北方车辆研究所 Involute cylindrical gear integrated experiment device for dynamic and quasi-static test

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103018042A (en) * 2012-12-20 2013-04-03 中国船舶重工集团公司第七�三研究所 Closed type axial loading testing apparatus of bevel wheel thrust cone balancing device
CN106840655A (en) * 2017-02-10 2017-06-13 中国航发沈阳发动机研究所 A kind of spiral bevel gear tooth root fatigue experimental device
CN106840655B (en) * 2017-02-10 2019-04-26 中国航发沈阳发动机研究所 A kind of spiral bevel gear tooth root fatigue experimental device
CN109141874A (en) * 2018-09-29 2019-01-04 济南大学 A kind of Power close type herringbone bear experimental rig
CN109752182A (en) * 2019-01-30 2019-05-14 中国北方车辆研究所 Involute cylindrical gear integrated experiment device for dynamic and quasi-static test

Similar Documents

Publication Publication Date Title
CN103018042A (en) Closed type axial loading testing apparatus of bevel wheel thrust cone balancing device
CN202939030U (en) Closed axial loading test apparatus of helical gear thrust cone balancing device
CN103033360A (en) Helical gear thrust cone balancing device open type axial loading test device
CN104374567B (en) Rotation torque, radial load and axial force synthesis load test method and device
CN202545696U (en) High-power two-stage speed-increasing planet gearbox
MX2018000722A (en) Hybrid vehicle.
CN202274057U (en) Differential mechanism with high gear ratio
CN202939029U (en) Open-type axial loading test apparatus of helical gear thrust cone balancing device
CN110132576B (en) Gear box test bench
CN202612486U (en) Fracturing pump driving device for planetary reduction box
CN203224356U (en) Gearbox gear contact pattern driver shaft load transmission device
CN202080850U (en) Synchronous high-precision mechanical cylinder
ATE525594T1 (en) COMPENSATOR FOR A VEHICLE
CN203560360U (en) Hypoid gear reducer
CN200996442Y (en) Conjugated double-outlet reversed gearbox
CN114252264B (en) Planetary row needle roller bearing test device and method
CN106195225B (en) Speed increaser assembly
CN215262420U (en) Gear fatigue testing device for new energy power assembly differential mechanism
CN204647163U (en) With the helical teeth input planet gear case of output rack
CN213117314U (en) Roller way climbing speed reducer
CN201925454U (en) Special speed reducer for roller way in hot area
CN104502098B (en) General bevel gear box mechanical close formula testing stand
CN103016630A (en) Three-branch two-stage speed-reducing helical gear transmission device for power of ship
CN203275085U (en) Gearbox and central transmission test bench
CN204603372U (en) With the hydraulic drilling machine of equilibrium function

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130515

Termination date: 20131220