CN203534824U - An inner and outer double-rotor fault simulation experiment table based on elastic foundation - Google Patents
An inner and outer double-rotor fault simulation experiment table based on elastic foundation Download PDFInfo
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- CN203534824U CN203534824U CN201320685732.XU CN201320685732U CN203534824U CN 203534824 U CN203534824 U CN 203534824U CN 201320685732 U CN201320685732 U CN 201320685732U CN 203534824 U CN203534824 U CN 203534824U
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Abstract
The utility model discloses an inner and outer double-rotor fault simulation experiment table based on elastic foundation and relates to an aeroengine experimental facility. The structure of the experiment table is mainly characterized in that an inner rotating shaft is disposed in an outer rotating shaft and the two rotating shafts have superposed central axes and are mechanically coupled by an intermediary supporting structure; that an inner rotor driving motor is disposed on an inner rotor driving motor seat and is connected with the inner rotating shaft through a main shaft coupling, that an inner rotor left wheel disc, an inner rotor left supporting structure, an inner rotor right wheel disc, and an inner rotor right supporting structure which are sleeved on the inner rotating shaft are successively connected along a central axis, and that an outer rotor left supporting structure, an outer rotor left wheel disc, an outer rotor right wheel disc which are sleeved on the outer rotating shaft are successively connected along a central axis. The experiment table employs elastic support with adjustable rigidity, and may detect influence of supporting rigidity on the power characteristics of the double rotors and simulate mechanical failures such as mass unbalance, rotor collision and friction, and support looseness of the double rotors of the aeroengine.
Description
Technical field
The utility model relates to aeromotor experimental provision, relates in particular to a kind of inner-outer birotor fault simulation experiment table based on elastic foundation.
Background technology
Aeromotor is the propulsion system of aircraft, and its health status and reliability effect the safety of flight.Along with the fast development of air-transport industry, complexity and the manufacturing cost of aircraft improve constantly, and aeromotor functional reliability becomes increasingly conspicuous on the impact of operation cost of enterprises.Therefore, for engine health is moved efficiently, save maintenance cost, just must understand the operation conditions of engine, grasp its Changing Pattern and trend, to critical component real-time state monitoring and fault diagnosis.
Fault Diagnosis of Aeroengines research at present biases toward the exploration of Fault Mechanism Analysis and diagnostic method mostly.Because aeromotor cost is high, test run cost is expensive, and theoretical checking often will be by means of fault simulation experiment table.The birotor experiment table of current domestic simulation aeroengine rotor fault is few.Existing birotor experiment table has also just retained this typical structure of aeromotor birotor, and to more random at epitrochanterian contrast locating for simulating the wheel disc of pneumatic plant and turbine stage blade, more do not have to consider the suffered aerodynamic force of actual aero-engine casing, elastic force to simulate.The experiment table that these have been simplified and the actual conditions deviation of engine are very big, have limited the experimental study of its fault characteristic.
Utility model content
The purpose of this utility model is just to overcome the shortcoming and defect that prior art exists, and a kind of inner-outer birotor fault simulation experiment table based on elastic foundation is provided.
The purpose of this utility model is achieved in that
The structure of the inner-outer birotor fault simulation experiment table based on elastic foundation is: in outer shaft, be provided with interior rotating shaft, both central axes, by intermediary's supporting structure mechanical couplings;
On elastic foundation, be provided with base;
Centre on base, from left to right, is respectively arranged with internal rotor drive motor support, the left supporting structure of internal rotor, the left supporting structure of outer rotor and the right supporting structure of internal rotor, is connected respectively by fastening bolt with base;
On internal rotor drive motor support, be provided with internal rotor drive motor, internal rotor drive motor is connected with interior rotating shaft by lead spindle, and the left supporting structure of internal rotor left wheel disk, internal rotor, internal rotor right wheel disk and the right supporting structure of internal rotor that are enclosed within interior rotating shaft are connected successively along central axis; The left supporting structure of outer rotor, outer rotor left wheel disk and the outer rotor right wheel disk that are enclosed within on outer shaft are connected successively along central axis;
Before on base, from left to right, be disposed with front outer rotor drive motor support, last supporting structure and the first two supporting structure, outer rotor drive motor before being provided with on front outer rotor drive motor support, front outer rotor drive motor, front shaft coupling, last supporting structure, front belt pulley and the first two supporting structure are connected successively along front axis;
After on base, from left to right, be disposed with rear outer rotor drive motor support, a rear supporting structure and rear two supporting structures, outer rotor drive motor after being provided with on rear outer rotor drive motor support, rear outer rotor drive motor, rear shaft coupling, a rear supporting structure, a rear belt pulley, rear two belt pulleys and rear two supporting structures are connected successively along posterior axis;
Outer shaft is by being arranged on the front belt pulley in front axis and posterior axis, a rear belt pulley, rear two belt pulleys respectively by front belt, a rear belt and rear two belt drives;
Front vibrator is installed on the front end of base, and perpendicular to central axis, right vibrator is installed on the right-hand member of base, is parallel to central axis;
To touch the device that rubs and be arranged on wheel disc to be measured position, and make to touch the interior ring that rubs and be enclosed in the periphery of wheel disc to be measured, and rub and be 90 ° on outer shroud two piezoelectric velocity sensors are installed touching touching of the device that rubs;
An eddy current displacement sensor is respectively installed near interior rotating shaft and outer shaft.
Compared with prior art, the utlity model has following advantage and good effect:
1, adopt the elastic bearing of adjustable rigidity, can test the impact of support stiffness on birotor kinematic behavior;
2, can simulate the mechanical faults such as the mass unbalance of aeromotor birotor, rotor rubbing and pedestal looseness;
3, employing is touched the device that rubs and is simulated rubbing;
4, the adjustable elastic foundation of elasticity, is used for simulating the outer suffered elastic force of casing;
5, adopt vibrator, be arranged in and axially vertical with parallel direction, in order to simulate casing vibration.
Accompanying drawing explanation
Fig. 1 is the structural representation (main looking) of this experiment table;
Fig. 2 is the structural representation (overlooking) of this experiment table;
Fig. 3 is the structural representation (side-looking) of this experiment table;
Fig. 4 .1 is the structural representation (main looking) that touches the device that rubs.
Fig. 4 .2 is the structural representation (side-looking) that touches the device that rubs.
In figure:
00-elastic foundation; 01-base; 02-internal rotor drive motor support;
03-internal rotor drive motor; 04-lead spindle; 05-interior rotating shaft;
06-internal rotor left wheel disk; The left supporting structure of 07-internal rotor;
The left supporting structure of 08-outer rotor; 09-outer shaft; 10-outer rotor left wheel disk;
11-outer rotor right wheel disk; 12-intermediary supporting structure;
13-internal rotor right wheel disk; The right supporting structure of 14-internal rotor;
15-1-front outer rotor drive motor, 15-2-rear outer rotor drive motor;
16-1-last supporting structure, 16-2-the first two supporting structure,
16-3-rear supporting structure, 16-4-rear two supporting structures;
17-1-front belt pulley, 17-2-rear belt pulley, 17-3-rear two belt pulleys;
18-1-front belt, 18-2-rear belt, 18-3-rear two belts;
19-1-front vibrator, 19-2-right vibrator;
20-touch the device that rubs, 20-1-the touch bearing that rubs, 20-2-the touch outer shroud that rubs,
20-3-the touch interior ring that rubs, 20-4-touch mount screw;
21-1-front shaft coupling, 21-2-rear shaft coupling;
22-1-front outer rotor drive motor support, 22-2-rear outer rotor drive motor support;
A-eddy current displacement sensor;
B-piezoelectric velocity sensor.
Embodiment
Below in conjunction with drawings and Examples, describe in detail.
One, the structure of experiment table
1, overall
As Fig. 1, 2, 3, this experiment table comprises elastic foundation 00, base 01, internal rotor drive motor support 02, internal rotor drive motor 03, lead spindle 04, interior rotating shaft 05, internal rotor left wheel disk 06, the left supporting structure 07 of internal rotor, the left supporting structure 08 of outer rotor, outer shaft 09, outer rotor left wheel disk 10, outer rotor right wheel disk 11, intermediary's supporting structure 12, internal rotor right wheel disk 13, the right supporting structure 14 of internal rotor, front outer rotor drive motor 15-1, rear outer rotor drive motor 15-2, last supporting structure 16-1, the first two supporting structure 16-2, a rear supporting structure 16-3, rear two supporting structure 16-4, front belt pulley 17-1, a rear belt pulley 17-2, rear two belt pulley 17-3, front belt 18-1, a rear belt 18-2, rear two belt 18-3, front vibrator 19-1, right vibrator 19-2, touch the device 20 that rubs, front shaft coupling 21-1, rear shaft coupling 21-2, front outer rotor drive motor support 22-1, rear outer rotor drive motor support 22-2, eddy current displacement sensor A and piezoelectric velocity sensor B,
Its position and annexation are:
In outer shaft 09, be provided with interior rotating shaft 05, both central axes, by intermediary's supporting structure 12 mechanical couplings;
On elastic foundation 00, be provided with base 01;
Centre on base 01, from left to right, is respectively arranged with internal rotor drive motor support 02, the left supporting structure 07 of internal rotor, the left supporting structure 08 of outer rotor and the right supporting structure 14 of internal rotor, is connected respectively by fastening bolt with base 01;
On internal rotor drive motor support 02, be provided with internal rotor drive motor 03, internal rotor drive motor 03 is connected with interior rotating shaft 05 by lead spindle 04, and the left supporting structure 07 of internal rotor left wheel disk 06, internal rotor, internal rotor right wheel disk 13 and the right supporting structure 14 of internal rotor that are enclosed within interior rotating shaft 05 are connected successively along central axis; The left supporting structure 08 of outer rotor, the outer rotor left wheel disk 10 that are enclosed within on outer shaft 09 are connected along central axis successively with outer rotor right wheel disk 11;
Before on base 01, from left to right, be disposed with front outer rotor drive motor support 22-1, last supporting structure 16-1 and the first two supporting structure 16-2, outer rotor drive motor 15-1 before being provided with on front outer rotor drive motor support 22-1, front outer rotor drive motor 15-1, front shaft coupling 21-1, last supporting structure 16-1, front belt pulley 17-1 and the first two supporting structure 16-2 are connected successively along front axis;
After on base 01, from left to right, be disposed with rear outer rotor drive motor support 22-2, a rear supporting structure 16-3 and rear two supporting structure 16-4, outer rotor drive motor 15-2 after being provided with on rear outer rotor drive motor support 22-2, rear outer rotor drive motor 15-2, rear shaft coupling 21-2, a rear supporting structure 16-3, a rear belt pulley 17-2, rear two belt pulley 17-3 and rear two supporting structure 16-4 are connected successively along posterior axis;
Front vibrator 19-1 is installed on the front end of base 01, and perpendicular to central axis, right vibrator 19-2 is installed on the right-hand member of base 01, is parallel to central axis;
To touch the device 20 that rubs and be arranged on wheel disc to be measured position, and make to touch the interior ring 20-3 that rubs and be enclosed in the periphery of wheel disc to be measured, and rub and be 90 ° on outer shroud 20-2 two piezoelectric velocity sensor B are installed touching the touching of device 20 of rubbing;
An eddy current displacement sensor A is respectively installed near interior rotating shaft 05 and outer shaft 09.
2, working mechanism
Rotating shaft 05 in internal rotor drive motor 03 drives by lead spindle 04, internal rotor left wheel disk 06 and internal rotor right wheel disk 13, be used for simulating rotating speed and the moment of low pressure rotor;
Internal rotor left wheel disk 06 and internal rotor right wheel disk 13 are arranged on respectively the right and left of interior rotating shaft 05 by expansion coupling sleeve, outer rotor left wheel disk 10 and outer rotor right wheel disk 11 are arranged on respectively the right and left of outer shaft 09 by expansion coupling sleeve, periphery at above-mentioned four wheel discs is provided with evenly distributed hole, in order to balancing bolt to be installed, comes analog-quality uneven;
By touching the device 20 that rubs, carry out rub experiment, acquisition difference is touched the form of rubbing, difference is touched the position of rubbing, different support stiffness, different rotating speeds than the vibration signal under condition;
By regulating the balancing bolt on wheel disc to be measured, carry out mass unbalance experiment, obtain different quality amount of unbalance, different non-equilibrium site, different support stiffness and different rotating speeds than under vibration signal;
By artificially the fastening bolt of supporting structure being unclamped to a certain degree, and it is carried out to axial limiting, obtain different pedestal looseness position, different aeration level, different support stiffness, different rotating speeds than under vibration signal.
3, functional part
Following function parts rub device 20 with touching except elastic foundation 00, and other is conventional part; Or be standard component, directly buy; Or be simple structure designed, designed and processing.
* elastic foundation
Elastic foundation is connected to form up and down by cement platform, Compress Spring and ground;
Described cement platform is that a square cement is dull and stereotyped;
Before and after described Compress Spring comprises, two arrange totally 6 groups of springs; Each groups of springs comprises again the spring that three of left, center, right height and diameter successively decrease;
Described ground is a square mixed earth ground.
By making cement platform sinking certain distance, progressively make 6,12 and 18 spring segmentations have an effect, can change the support stiffness of elastic foundation.
* base 01 adopts cast iron process manufacture, has vibration resistance.
* internal rotor drive motor support 02, front outer rotor drive motor support 22-1, rear outer rotor drive motor support 22-2 are according to corresponding motor customization.
* internal rotor drive motor 03, front outer rotor drive motor 15-1, rear outer rotor drive motor 15-2 are direct current generator of the same type, can realize even rotating speed.
* lead spindle 04 is flexible coupling, can compensate by connection diaxon axis relativity shift, has bumper and absorbing shock performance.
* during interior rotating shaft 05, outer shaft 09 adopt, carbon quenched and tempered steel is manufactured, and has enough intensity and toughness.
* internal rotor left wheel disk 06, internal rotor right wheel disk 13, outer rotor left wheel disk 10 and outer rotor right wheel disk 11 all adopt 25Cr2MoV, have enough wearing qualities, are suitable for doing rub experiment.
* the left supporting structure 07 of internal rotor, the right supporting structure 14 of internal rotor and the left supporting structure 08 of outer rotor form by bearing, bearing and rotor cage type elastic support, by changing rotor cage type elastic support, adjust support stiffness.
* intermediary's supporting structure 12 consists of needle bearing, and radial structure is compact, is applicable to the radially restricted supporting result of installation dimension.
* last supporting structure 16-1, the first two supporting structure 16-2, a rear supporting structure 16-3, rear two supporting structure 16-4 form by bearing and bearing, and rigidity is non-adjustable.
* front belt pulley 17-1, a rear belt pulley 17-2, rear two belt pulley 17-3 are standard component, according to actual conditions, match.
* front belt 18-1, a rear belt 18-2, rear two belt 18-3 are flat belt, according to actual conditions, match.
* front vibrator 19-1 and right vibrator 19-2 are standard component, according to actual conditions, match.
* touch the device 20 that rubs
Touch the device 20 that rubs by touching the bearing 20-1 that rubs, touch the outer shroud 20-2 that rubs, touch to rub interior ring 20-3 and touch mount screw 20-4 and form;
Be provided with and touch the outer shroud 20-2 that rubs touching on the bearing 20-1 that rubs, in touching the outer shroud 20-2 that rubs, be provided with and touch the interior ring 20-3 that rubs, touch the center of circle of rubbing outer shroud 20-2 and touching the interior ring 20-3 that rubs and overlap, be evenly provided with and touch mount screw 20-4 touching on the outer shroud 20-2 that rubs.
Touching rubs outer shroud 20-2 and touch the interior ring 20-3 that rubs is formed by connecting by two semicircular ring respectively, detachable, is arranged on the periphery of wheel disc to be measured while being convenient to test.
Touching the interior ring 20-3 that rubs is arranged on and touches in the outer shroud 20-2 that rubs, axial restraint, makes to touch by touching mount screw 20-4 the interior ring 20-3 generation radial deformation that rubs, and changes and touches the gap of rubbing between interior ring 20-3 and institute's measuring wheel dish, manufacture is touched and is rubbed, can simulate single-point touch rub, 2 touch and rub and whole circle touches and rubs.
* front shaft coupling 21-1 and rear shaft coupling 21-2 are positive coupling, for connecting motor shaft and front and back driving shaft.
* eddy current displacement sensor A
Eddy current displacement sensor A is outsourcing standard component, for measuring vibrations signal.
* piezoelectric velocity sensor B
Piezoelectric velocity sensor B is outsourcing standard component, for measuring vibrations signal.
Two, the experimental technique of experiment table
1, rub experiment
1. will touch the device 20 that rubs and be arranged on wheel disc to be measured position, make to touch rub interior ring 20-3 be enclosed in wheel disc to be measured (can be in internal rotor left wheel disk 06, internal rotor right wheel disk 13, outer rotor left wheel disk 10 and outer rotor right wheel disk 11 any or several) periphery, touch the touching of device 20 of rubbing rub be 90 ° on outer shroud 20-2 and two piezoelectric velocity sensor B(be installed as Fig. 4 .1);
2. start three drive motor (internal rotor drive motor 03, front outer rotor drive motor 15-1 and rear outer rotor drive motor 15-2), stablizing outer rotor rotating speed is 3600rpm, internal rotor rotating speed is 3000rpm, inner and outer rotors rotating ratio 1.2, adjusting is touched mount screw 20-4 and is changed the deflection touch the interior ring 20-3 that rubs, measure respectively single-point touch rub, 2 touch and rub and whole circle touches the vibration signal that touches the outer shroud 20-2 that rubs while rubbing;
3. close three drive motor, conversion supporting structure (can be in internal rotor front support structure 07, internal rotor rear support structure 14 and outer rotor front support structure 08 any or several) in rotor cage type elastic support, support stiffness is changed, start three drive motor, measure respectively single-point touch rub, 2 touch and rub and whole circle touches the vibration signal that touches the outer shroud 20-2 that rubs while rubbing;
4. change inner and outer rotors rotating speed, raise or reduce inner and outer rotors rotating ratio, measure respectively single-point touch rub, 2 touch and rub and whole circle touches the vibration signal that touches the outer shroud 20-2 that rubs while rubbing;
Its experiment meaning is: acquisition difference is touched the form of rubbing, difference is touched the position of rubbing, different support stiffness, different rotating speeds ratio and adds the vibration signal under exciting force condition.
2, mass unbalance experiment
5. change inner and outer rotors rotating speed, raise or reduce inner and outer rotors rotating ratio, measure the vibration signal of inner and outer rotors horizontal and vertical direction;
Its experiment meaning is: obtain different quality amount of unbalance, different non-equilibrium site, different support stiffness, different rotating speeds ratio and add the vibration signal under exciting force condition.
3, pedestal looseness experiment
an eddy current displacement sensor A is respectively installed near interior rotating shaft 05 and outer shaft 09, and position as shown in Figure 1 and Figure 2;
close three drive motor, conversion supporting structure (can be in internal rotor front support structure 07, internal rotor rear support structure 14 and outer rotor front support structure 08 any or several) in rotor cage type elastic support, support stiffness is changed, start three drive motor, measure the signal of the vibration of inner and outer rotors vertical direction;
5. change inner and outer rotors rotating speed, raise or reduce inner and outer rotors rotating ratio, measure the signal of the vibration of inner and outer rotors vertical direction;
Its experiment meaning is: obtain different pedestal looseness position, different aeration level, different support stiffness, different rotating speeds than and and add the vibration signal under exciting force condition.
4, touch rub, the experiment of mass unbalance, pedestal looseness can carry out individually or simultaneously.
Claims (3)
1. the inner-outer birotor fault simulation experiment table based on elastic foundation, is characterized in that:
In outer shaft (09), be provided with interior rotating shaft (05), both central axes, by intermediary's supporting structure (12) mechanical couplings;
On elastic foundation (00), be provided with base (01);
Centre on base (01), from left to right, be respectively arranged with internal rotor drive motor support (02), the left supporting structure of internal rotor (07)), the left supporting structure of outer rotor (08) and the right supporting structure of internal rotor (14), by fastening bolt, be connected with base (01) respectively;
On internal rotor drive motor support (02), be provided with internal rotor drive motor (03), internal rotor drive motor (03) is connected with interior rotating shaft (05) by lead spindle (04), and the internal rotor left wheel disk (06), the left supporting structure of internal rotor (07), internal rotor right wheel disk (13) and the right supporting structure of internal rotor (14) that are enclosed within interior rotating shaft (05) are connected successively along central axis; The left supporting structure of outer rotor (08), outer rotor left wheel disk (10) and the outer rotor right wheel disk (11) that are enclosed within on outer shaft (09) are connected successively along central axis;
Before base (01), from left to right, be disposed with front outer rotor drive motor support (22-), last supporting structure (16-1) and the first two supporting structure (16-2), on front outer rotor drive motor support (22-1), be provided with front outer rotor drive motor (15-1), front outer rotor drive motor (15-1), front shaft coupling (21-1), last supporting structure (16-1), front belt pulley (17-1) and the first two supporting structure (16-2) are connected successively along front axis;
After base (01), from left to right, be disposed with rear outer rotor drive motor support (22-2), a rear supporting structure (16-3) and rear two supporting structures (16-4), on rear outer rotor drive motor support (22-2), be provided with rear outer rotor drive motor (15-2), rear outer rotor drive motor (15-2), rear shaft coupling (21-2), a rear supporting structure (16-3), a rear belt pulley (17-2), rear two belt pulleys (17-3) and rear two supporting structures (16-4) are connected successively along posterior axis;
Outer shaft (09) is driven by front belt (18-1), a rear belt (18-2) and rear two belts (18-3) respectively by the front belt pulley (17-1), a rear belt pulley (17-2), rear two belt pulleys (17-3) that are arranged in front axis and posterior axis;
Front vibrator (19-1) is installed on the front end of base (01), and perpendicular to central axis, right vibrator (19-2) is installed on the right-hand member of base (01), is parallel to central axis;
Touch the device that rubs (20) and be arranged on wheel disc to be measured position, make to touch the interior ring (20-3) that rubs and be enclosed in the periphery of wheel disc to be measured, on the outer shroud that rubs (20-2), be 90 ° two piezoelectric velocity sensors (B) are installed touching touching of the device that rubs (20);
Near interior rotating shaft (05) and outer shaft (09), an eddy current displacement sensor (A) is respectively installed.
2. by inner-outer birotor fault simulation experiment table claimed in claim 1, it is characterized in that:
Described elastic foundation (00) is connected to form up and down by cement platform, Compress Spring and ground;
Described cement platform is that a square cement is dull and stereotyped;
Before and after described Compress Spring comprises, two arrange totally 6 groups of springs, and each groups of springs comprises again the spring that three of left, center, right height and diameter successively decrease;
Described ground is a square mixed earth ground.
3. by inner-outer birotor fault simulation experiment table claimed in claim 1, it is characterized in that:
Described touch the device that rubs (20) by touching the bearing that rubs (20-1), touch the outer shroud that rubs (20-2), touch to rub interior ring (20-3) and touch mount screw (20-4) and form;
Be provided with and touch the outer shroud that rubs (20-2) touching on the bearing that rubs (20-1), in touching the outer shroud that rubs (20-), be provided with and touch the interior ring (20-3) that rubs, the center of circle of touching the outer shroud that rubs (20-2) and touching the interior ring (20-3) that rubs overlaps, and is evenly provided with and touches mount screw (20-4) touching on the outer shroud that rubs (20-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201320685732.XU CN203534824U (en) | 2013-10-31 | 2013-10-31 | An inner and outer double-rotor fault simulation experiment table based on elastic foundation |
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| CN201320685732.XU CN203534824U (en) | 2013-10-31 | 2013-10-31 | An inner and outer double-rotor fault simulation experiment table based on elastic foundation |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103528824A (en) * | 2013-10-31 | 2014-01-22 | 华中科技大学 | Elastic foundation based internal and external dual-rotor fault simulation experiment table |
| CN105278349A (en) * | 2015-11-23 | 2016-01-27 | 哈尔滨工业大学 | Aero-engine simulation test bed on the basis of birotor simplified dynamic model design |
| CN105841960A (en) * | 2016-03-23 | 2016-08-10 | 大连理工大学 | Aero engine medium bearing dual rotor test stand loading method |
| CN108519235A (en) * | 2018-03-17 | 2018-09-11 | 北京化工大学 | Air impeller drive-type birotor testing stand |
| CN108663214A (en) * | 2018-04-28 | 2018-10-16 | 北京航天动力研究所 | A kind of support component and test method for the experiment of high speed rotor analog simulation |
| CN108760284A (en) * | 2018-08-24 | 2018-11-06 | 哈尔滨电气股份有限公司 | A kind of Multifunctional rotor experiment test device |
| CN115855356A (en) * | 2022-11-24 | 2023-03-28 | 中国核动力研究设计院 | Experimental device and method for supporting cylindrical extrusion film force measurement |
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- 2013-10-31 CN CN201320685732.XU patent/CN203534824U/en not_active Withdrawn - After Issue
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103528824A (en) * | 2013-10-31 | 2014-01-22 | 华中科技大学 | Elastic foundation based internal and external dual-rotor fault simulation experiment table |
| CN103528824B (en) * | 2013-10-31 | 2015-09-30 | 华中科技大学 | Based on the inner-outer birotor fault simulation experiment table of elastic foundation |
| CN105278349A (en) * | 2015-11-23 | 2016-01-27 | 哈尔滨工业大学 | Aero-engine simulation test bed on the basis of birotor simplified dynamic model design |
| CN105278349B (en) * | 2015-11-23 | 2018-12-11 | 哈尔滨工业大学 | Aero-engine simulation test stand based on the design of birotor reduced mechanism |
| CN105841960A (en) * | 2016-03-23 | 2016-08-10 | 大连理工大学 | Aero engine medium bearing dual rotor test stand loading method |
| CN105841960B (en) * | 2016-03-23 | 2018-10-16 | 大连理工大学 | Aero-engine intershaft bearing birotor testing stand loading method |
| CN108519235A (en) * | 2018-03-17 | 2018-09-11 | 北京化工大学 | Air impeller drive-type birotor testing stand |
| CN108663214A (en) * | 2018-04-28 | 2018-10-16 | 北京航天动力研究所 | A kind of support component and test method for the experiment of high speed rotor analog simulation |
| CN108760284A (en) * | 2018-08-24 | 2018-11-06 | 哈尔滨电气股份有限公司 | A kind of Multifunctional rotor experiment test device |
| CN108760284B (en) * | 2018-08-24 | 2024-02-13 | 哈尔滨电气股份有限公司 | Multifunctional rotor experiment testing device |
| CN115855356A (en) * | 2022-11-24 | 2023-03-28 | 中国核动力研究设计院 | Experimental device and method for supporting cylindrical extrusion film force measurement |
| CN115855356B (en) * | 2022-11-24 | 2024-04-02 | 中国核动力研究设计院 | Experimental device and method for measuring force of supporting cylinder extrusion film |
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