CN209446262U - A kind of loacting test rack inertia variable fly wheel system - Google Patents
A kind of loacting test rack inertia variable fly wheel system Download PDFInfo
- Publication number
- CN209446262U CN209446262U CN201822027205.5U CN201822027205U CN209446262U CN 209446262 U CN209446262 U CN 209446262U CN 201822027205 U CN201822027205 U CN 201822027205U CN 209446262 U CN209446262 U CN 209446262U
- Authority
- CN
- China
- Prior art keywords
- flywheel
- shaft
- crane
- fly wheel
- wheel system
- 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
Links
Landscapes
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The utility model discloses a kind of loacting test rack inertia variable fly wheel system, including the first flywheel, the second flywheel, third flywheel and shaft, second flywheel is that interference fit is fixedly connected with the shaft;First flywheel, second flywheel and the third flywheel are disc-shaped structure;Described first and third flywheel inner side end on be equipped with boss, be designed with pit on two end faces of second flywheel;When need fly wheel system provide small rotary inertia when, only described second flywheel is rotated with the shaft, described first and third flywheel be placed on flywheel storing seat;When needing to increase the rotary inertia of fly wheel system, selects first flywheel or the third flywheel and second flywheel to connect and rotated with the shaft;The loacting test rack inertia variable fly wheel system can provide a variety of different Rotary Inertia of Flywheel to test different operating conditions, and the size of Rotary Inertia of Flywheel is unrestricted, can distribute rationally according to actual needs.
Description
Technical field
The utility model design is a kind of loacting test rack inertia variable fly wheel system.
Background technique
The same testing stand generally requires to simulate a variety of different loads, and load is simulated with flywheel, changes turning for flywheel
Dynamic inertia has just achieved the purpose that change load.Fly wheel system should not be influenced by revolving speed height and rotary inertia size, be both needed to
It is operational security, reliable.Existing variable inertia flywheel structure is difficult to meet this requirement.
Summary of the invention
The utility model design provides a kind of loacting test rack inertia variable fly wheel system, is wanted according to different operating condition of test
It asks, increases and decreases the quantity of flywheel accordingly to simulate different loads.The technical solution of the invention design is as follows:
A kind of loacting test rack inertia variable fly wheel system mainly includes the first flywheel, the second flywheel, third flywheel and is turned
Axis, second flywheel are that interference fit is fixedly connected with the shaft;First flywheel includes the first Flywheel disc, and described the
Two flywheels include the second Flywheel disc, and the third flywheel includes third Flywheel disc;Described first and third flywheel inner side end on
It is equipped with boss, is designed with pit on two end faces of second flywheel.When needing fly wheel system to provide small rotary inertia,
Only described second flywheel is rotated with the shaft, at this time described first and third flywheel be individually positioned in flywheel storing seat
One and flywheel storing seat two on.When needing to increase the rotary inertia of fly wheel system, first flywheel or the third are selected
Flywheel is cooperatively connected with second flywheel to be rotated with the shaft.The utility model design only with the third flywheel with
The second flywheel connection, is illustrated, the rest may be inferred by analogy for rotating the two together.Method are as follows: when testing stand is static,
By the mobile third flywheel of crane, so that the boss of the third flywheel inner side end and the second flywheel corresponding end surface
Pit cooperation, and pass through notch cuttype through hole two and threaded hole for the third flywheel and second flywheel with the screw two
Connection.In shaft rotation, second flywheel drives the third flywheel to rotate together.
Further, first flywheel, second flywheel and the third flywheel are disc-shaped structure;And it is described
Second flywheel is located at first flywheel and between the third flywheel.First flywheel and the third flywheel are equipped with
Notch cuttype through hole, lifting eye, the lifting eye be radially respectively provided at along flywheel described first and third flywheel excircle on;Institute
It states the second flywheel both ends of the surface and is designed with threaded hole.When second flywheel drives first flywheel to rotate together, described first
Flywheel and the shaft are clearance fits;Similarly, when second flywheel drives the third flywheel to rotate together, the third
Flywheel and the shaft are also clearance fit.
Further, the loacting test rack inertia variable fly wheel system further includes flywheel storing seat and bearing.The flywheel
Storage tray one and flywheel storing seat two are respectively used to first flywheel and third flywheel and do not rotate with second flywheel
When storage.The bearing is used to support the shaft and makes it that can only realize rotation.
Further, the loacting test rack inertia variable fly wheel system further includes crane and crane bracket.The crane packet
Include hanging ring, suspension hook, vehicle frame plate, nut, limit plate, bolt, pin shaft, wheel.The hanging ring can be threadingly attached to institute respectively
It states the lifting eye of the first flywheel or the third flywheel and is connect with the suspension hook.The suspension hook is equipped with spin-ended piece, the vehicle frame
Plate is equipped with guide hole, and described spin-ended piece cooperates with the guide hole, for limiting the rotation of the suspension hook;The limit plate passes through described
Two bolts are mounted on the vehicle frame plate, for limiting moving up and down for the nut;The suspension hook and the nut spiral shell
Line connection;Rotating the nut can be such that the suspension hook moves up and down.The crane bracket is used to support the crane, the crane
It is all provided with fluted on two curb girders of bracket, the wheel can be moved forward and backward on the groove.
The beneficial effect of the utility model design is: 1. same testing stands can provide a variety of different for the different operating conditions of test
Rotary Inertia of Flywheel;2. the size of Rotary Inertia of Flywheel is unrestricted, group can be optimized according to the size of realistic simulation load
It closes;3. easy to use: the system structure is easy, safe and reliable.
Detailed description of the invention
Fig. 1 is the three-dimensional structure decomposition diagram of the utility model design;
Fig. 2 is the decomposition diagram of crane in the utility model design;
Fig. 3 is the structure elevational schematic view of vehicle frame plate in the utility model design;
Fig. 4 is the structural schematic diagram of limit plate in the utility model design.
In attached drawing: 1. first flywheels, 11. notch cuttype through hole one, 12. lifting eyes, 2. second flywheels, 21. threaded holes, 3.
Three flywheels, 31. notch cuttype through hole two, 32. lifting eyes, 4. shafts, 51. screws one, 52. screws two, 61. flywheel storing seats one,
62. flywheel storing seat two, 71. bearings, 72. bearings, 8. crane brackets, 9. cranes, 91. hanging rings, 92. suspension hooks, 921. spin-ended pieces,
93. vehicle frame plate, 931. guide holes, 94. nuts, 95. limit plates, 96. bolts, 97. pin shafts, 98. wheels.
Specific embodiment
As shown in the picture, all equal structures of component are simple, reliable, easy to assembly in figure.
Flywheel quantity used can be not limited to three flywheels, can increase in shaft 4 according to actual needs different
The flywheel of rotary inertia, the utility model, which designs, only illustrates its working principle by taking three flywheels as an example.
The specific embodiment of the loacting test rack inertia variable fly wheel system is as follows:
The both ends of shaft 4 are supported on bearing block by two bearings 71 and 72 respectively.Reeded crane on two curb girders
Bracket 8 is placed on hold-down support.Limit plate 95 is mounted on vehicle frame plate 93 by two bolts 96.Crane 9 passes through 4 pin shafts 97
It is supported on 4 wheels 91, the rolling bearing inner ring in 4 wheels 91 is all made of interference fit with 4 pin shafts 97 respectively and connects
It connects.
When operating condition of test needs fly wheel system to provide small rotary inertia, only the second flywheel 2 is rotated with shaft 4,
First flywheel 1 and third flywheel 3 are stored in flywheel storing seat 1, on flywheel storing seat 2 62 respectively.
When operating condition of test needs fly wheel system to increase rotary inertia, only connected with third flywheel 3 and the cooperation of the second flywheel 2
It connects, is illustrated for rotating the two together, the rest may be inferred by analogy.In loacting test rack stationary state, by hanging ring 91 and
The lifting eye 32 of three flywheels 3 cooperates with suspension hook 92 again after being connected through a screw thread;Nut 94 is rotated clockwise, suspension hook 92 slings third
Flywheel 3 up vertically moves;Rotating nuts 94 counterclockwise, then third flywheel 3 vertically moves down with suspension hook 92.Suspension hook 92
On spin-ended piece 921 cooperate with the guide hole 931 of vehicle frame plate 93, limit the rotation of suspension hook 92;Limit plate 95 passes through two bolts 96
It is mounted on vehicle frame plate 93, limitation nut 94 moves up and down;Suspension hook 92 is threadedly coupled with nut 94;Therefore, rotating nuts
94 can only be such that suspension hook 92 moves up and down.Rotating nuts 94 make third flywheel 3 be in proper height and position, make crane 9
Third flywheel 3 is played on crane bracket 8 slowly to move toward the direction close to the second flywheel 2, and makes 3 inner end of third flywheel
The boss in face is matched with the pit of 2 corresponding end surface of the second flywheel, then passes through notch cuttype through hole 2 31 and spiral shell with screw 2 52
Pit 21 connects firmly third flywheel 3 and the second flywheel 2 together.
When the first flywheel 1 connected firmly with the second flywheel 2 needs to be moved on one on flywheel storing seat not with the second flywheel 2 one
When playing rotation, under loacting test rack stationary state, it is connected through a screw thread hanging ring 91 and the lifting eye 12 of the first flywheel 1, is hung
Ring and the cooperation of suspension hook 92 on ring 91 sling the first flywheel 1, unload all 4 screws 1 later, then make on crane bracket 8
Crane 9 plays the first flywheel 1 and slowly moves toward the direction far from the second flywheel 2, and the first flywheel 1 is made to be in flywheel storing
The surface of seat 1, last rotating nuts 94 fall in the first flywheel 1 slowly on flywheel storing seat 1.Third flywheel 3
It is moved on flywheel storing seat 2 62 that be moved to the operating method of flywheel storing seat 1 with the first flywheel 1 identical.
Claims (4)
1. a kind of loacting test rack inertia variable fly wheel system, which is characterized in that including the first flywheel (1), the second flywheel (2),
Three flywheels (3), shaft (4), screw one, two (51,52), flywheel storing seat one, two (61,62), bearing (71,72), crane branch
Frame (8) and crane (9);Second flywheel (2) is that interference fit is fixedly connected with the shaft (4);First flywheel
(1), second flywheel (2) and the third flywheel (3) are respectively equipped with notch cuttype through hole one, threaded hole, notch cuttype through hole two
(11,21,31);First flywheel (1) and the third flywheel (3) are respectively equipped with lifting eye (12,32);First flywheel
It (1) include the first Flywheel disc, second flywheel (2) includes the second Flywheel disc, and the third flywheel (3) includes third flywheel
Disk;Boss, two end faces of second flywheel (2) are equipped on first flywheel (1) and third flywheel (3) inner side end
On be designed with pit;By the movement of the crane (9), make the boss and described second of third flywheel (3) inner side end
The pit of flywheel (2) corresponding end surface cooperates, and passes through the notch cuttype through hole two (31) and the spiral shell with the screw two (52)
The third flywheel (3) connect by pit (21) with second flywheel (2);First flywheel (1) and second flywheel
(2) it is cooperatively connected and the third flywheel (3) is identical as the second flywheel (2) mating connection method;When the needs flywheel
When system provides small rotary inertia, only described second flywheel (2) rotates together with the shaft (4), first flywheel (1)
It is individually positioned on the flywheel storing seat one (61) and flywheel storing seat two (62) with third flywheel (3);When needing to increase institute
When stating fly wheel system rotary inertia, first flywheel (1) or the third flywheel (3) is selected to match with second flywheel (2)
Conjunction is connected to rotate with the shaft (4).
2. loacting test rack inertia variable fly wheel system as described in claim 1, which is characterized in that first flywheel (1), institute
Stating the second flywheel (2) and the third flywheel (3) is disc-shaped structure;And second flywheel (2) is located at described first and flies
It takes turns between (1) and the third flywheel (3);The lifting eye (12,32) is radially respectively provided at first flywheel (1) along flywheel
And on the excircle of the third flywheel (3);It is described when second flywheel (2) drives first flywheel (1) to rotate together
First flywheel (1) and the shaft (4) are clearance fits;Similarly, second flywheel (2) drives the third flywheel (3) one
When playing rotation, the third flywheel (3) and the shaft (4) are also clearance fit.
3. loacting test rack inertia variable fly wheel system as claimed in claim 2, which is characterized in that the flywheel storing seat one,
Two (61,62) are respectively used to first flywheel (1) and the third flywheel (3) and do not rotate with second flywheel (2)
When storage;The bearing (71,72) is used to support the shaft (4) and makes it that can only realize rotation.
4. loacting test rack inertia variable fly wheel system as claimed in claim 3, which is characterized in that the crane (9) includes hanging
Ring (91), suspension hook (92), vehicle frame plate (93), nut (94), limit plate (95), bolt (96), pin shaft (97), wheel (98);Institute
Stating hanging ring (91) can be connect by screw thread with the lifting eye (12,32), and the ring on hanging ring (91) can cooperate with suspension hook (92);Institute
State the connection of hanging ring (91) for first flywheel (1) or the third flywheel (3) and the suspension hook (92);The suspension hook
(92) it is equipped with spin-ended piece (921), the vehicle frame plate (93) is equipped with guide hole (931), spin-ended piece (921) and the guide hole
(931) cooperate, for limiting the rotation of the suspension hook (92);The limit plate (95) is mounted on by described two bolts (96)
On the vehicle frame plate (93), for limiting moving up and down for the nut (94);The suspension hook (92) and the nut (94) are used
It is threadedly coupled;Rotating the nut (94) can be such that the suspension hook (92) moves up and down;The crane bracket (8) is used to support described
Two curb girders of crane (9), the crane bracket (8) are equipped with groove, and the wheel (93) can be moved forward and backward on the groove;
The crane (9) passes through all 4 pin shafts (97) and is supported on 4 wheels (91), in 4 wheels (91)
Rolling bearing inner ring and 4 pin shafts (97) are interference fit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822027205.5U CN209446262U (en) | 2018-12-05 | 2018-12-05 | A kind of loacting test rack inertia variable fly wheel system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822027205.5U CN209446262U (en) | 2018-12-05 | 2018-12-05 | A kind of loacting test rack inertia variable fly wheel system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209446262U true CN209446262U (en) | 2019-09-27 |
Family
ID=68012217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201822027205.5U Expired - Fee Related CN209446262U (en) | 2018-12-05 | 2018-12-05 | A kind of loacting test rack inertia variable fly wheel system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN209446262U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109387360A (en) * | 2018-12-05 | 2019-02-26 | 西南交通大学 | Loacting test rack inertia variable fly wheel system |
-
2018
- 2018-12-05 CN CN201822027205.5U patent/CN209446262U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109387360A (en) * | 2018-12-05 | 2019-02-26 | 西南交通大学 | Loacting test rack inertia variable fly wheel system |
CN109387360B (en) * | 2018-12-05 | 2023-12-26 | 西南交通大学 | Variable inertia flywheel system of fixed test bed |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106855462B (en) | A kind of Combined Loading device for robot joint speed reducer performance test | |
CN104792532B (en) | Thrust bearing equipment test device peculiar to vessel | |
CN105352732B (en) | A kind of compound static(al) and fatigue tester of aerial engine fan axis | |
CN206872309U (en) | A kind of electromechanical liquid unitary rotary hoister | |
CN207585912U (en) | It is a kind of simple type rotor, bearing fault simulation test bed | |
CN206856983U (en) | It is a kind of can be with the quadrotor of center-of-gravity regulating | |
CN209446262U (en) | A kind of loacting test rack inertia variable fly wheel system | |
CN104165725A (en) | Automatic precise counterweight loading mechanism of torque standard machine | |
CN109387360A (en) | Loacting test rack inertia variable fly wheel system | |
CN105223015A (en) | A kind of low-speed big inertia brake test unit with speed reduction unit | |
CN104180991B (en) | Comprehensive performance testing machine for ultra-high speed oil bearing | |
CN203913876U (en) | The electric rotary body that a kind of lazy Susan is used | |
CN106482939A (en) | A kind of general-purpose vertical Loading for actuator testing stand | |
CN105865785A (en) | Slewing bearing fatigue testing machine capable of applying axial force and bending moment | |
CN205593740U (en) | Owner rotor shaft loading device goes straight up to based on equivalence blade | |
CN105667827A (en) | Universal undercarriage mounting cart | |
CN104291158B (en) | A kind of steel wire rope coiler and steel wire disk are around unfolding device | |
CN207483171U (en) | A kind of tooling turned over for turbine rotor with lifting by crane vertically | |
CN106829722A (en) | Large-scale Wind Turbines variable propeller gearbox installation tool | |
CN116223033A (en) | High-speed antifriction bearing lubrication experiment table | |
CN207336067U (en) | A kind of low dynamic stiffness for rotary axis longitudinally loads exciting device | |
CN104913867A (en) | Rotary support load torque analysis test apparatus | |
CN204373906U (en) | A kind of radial loading device of shaft element load test | |
CN207636242U (en) | A kind of rotor high-speed balancing roller bearings device | |
CN204649335U (en) | A kind of pivoting support load torque analytical test device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190927 Termination date: 20201205 |