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 PDFInfo
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- 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
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- gear
- loader
- thrust
- output shaft
- axial
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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
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.
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).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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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)
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CN 201220706306 CN202939030U (en) | 2012-12-20 | 2012-12-20 | Closed axial loading test apparatus of helical gear thrust cone balancing device |
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CN202939030U true CN202939030U (en) | 2013-05-15 |
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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 |
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Cited By (4)
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 |
-
2012
- 2012-12-20 CN CN 201220706306 patent/CN202939030U/en not_active Expired - Fee Related
Cited By (5)
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 |
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Legal Events
Date | Code | Title | Description |
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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 |