[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN106404342A - Dynamic loading device for rotary shaft balance - Google Patents

Dynamic loading device for rotary shaft balance Download PDF

Info

Publication number
CN106404342A
CN106404342A CN201611029401.5A CN201611029401A CN106404342A CN 106404342 A CN106404342 A CN 106404342A CN 201611029401 A CN201611029401 A CN 201611029401A CN 106404342 A CN106404342 A CN 106404342A
Authority
CN
China
Prior art keywords
balance
rotary shaft
power output
loading device
dynamic loading
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.)
Granted
Application number
CN201611029401.5A
Other languages
Chinese (zh)
Other versions
CN106404342B (en
Inventor
吴福章
别云朋
钱志高
田斌
赵亮亮
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.)
Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center
Original Assignee
Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center
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 Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center filed Critical Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center
Priority to CN201611029401.5A priority Critical patent/CN106404342B/en
Publication of CN106404342A publication Critical patent/CN106404342A/en
Application granted granted Critical
Publication of CN106404342B publication Critical patent/CN106404342B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06Measuring arrangements specially adapted for aerodynamic testing
    • G01M9/062Wind tunnel balances; Holding devices combined with measuring arrangements

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

The invention discloses a dynamic loading device for a rotary shaft balance, which comprises a rack, a driving motor arranged on the rack and a power output shaft arranged on the upper end face of the rack, and is characterized in that a power output end of the driving motor is connected to the power output shaft through a belt, one end of the power output shaft is connected to a dynamic loading device through the rotary shaft balance, and the other end of the power output shaft is connected to a slip ring electricity introducing device through a coupling. The dynamic loading device disclosed by the invention solves a loading problem of domestic rotary shaft balances, improves the measurement accuracy of the rotary shaft balance, and fills a gap in domestic related fields; and compared with similar products abroad, the dynamic loading device is better in efficiency-cost ratio, more convenient in use and low in maintenance cost.

Description

A kind of rotary shaft balance dynamic loading device
Technical field
The present invention relates to wind tunnel test field, a kind of specifically dynamic loading device of rotary shaft balance.
Background technology
Rotary shaft balance is mainly used in propeller aeroplane smooth impact wind tunnel test, can directly accurate measurement propeller carry Lotus.Rotary shaft balance calibration includes static loading and dynamic load, and static loading is identical with balance normal calibration, and dynamic load is then Need under certain rotating speed, balance imposed load to be calibrated, thus obtaining accurate balance formula.Rotary shaft balance dynamic load It is a new technical field of comparison at home, its specific device is not also shown in by domestic wind-tunnel at present, and external wind-tunnel has correlation Record., all within 10000 revs/min, external charger can be in balance for conventional rotary shaft balance rotating speed at present Apply rated load in the range of maximum speed.
Content of the invention
It is an object of the invention to provide a kind of dynamic loading device of rotary shaft balance, the rotating speed realizing balance can reach 10000 revs/min, and can realize the signal transmission of balance under this high-speed rotation in outside controller.
For achieving the above object, the present invention adopts the following technical scheme that:
A kind of rotary shaft balance dynamic loading device, including stand, the motor being arranged on stand, is arranged on stand upper end The power output shaft in face, the clutch end of described motor is connected on power output shaft by belt, and described power is defeated One end of shaft is connected with dynamic loading device by rotary shaft balance, and the other end of power output shaft is connected to by shaft coupling On slip ring electrical feedthrough;
Counterweight is loaded respectively with horizontal direction in vertical direction, described dynamic load on the outer tube of described dynamic loading device The outer barrel of device is provided with a set of rolling bearing, and described rotary shaft balance is connected with rolling bearing;
It is provided with holding wire, slided with the balance being arranged in dynamic loading device in one end of holding wire in described rotary balance axle Contact, the other end of holding wire is connected with slip ring electrical feedthrough after power output shaft.
In technique scheme, the clutch end of described motor is big belt wheel, and one end of power output shaft is Small pulley, described belt is connected in big belt wheel and small pulley.
In technique scheme, the surface of described two ends of rotary shaft balance is respectively arranged with the contact of holding wire Point, connects a holding wire between two contact points
In technique scheme, in described power output shaft, it is provided with wire casing, described holding wire is arranged in wire casing.
In technique scheme, it is provided with three wire casings in described power output shaft, is provided with each wire casing One road holding wire.
In technique scheme, connecing of three holding wires is respectively arranged with the surface of two ends of rotary shaft balance Contact, two corresponding contact points connect a holding wire.
In technique scheme, the contact point of described rotary shaft balance one end and balance sliding contact, power output shaft The other end and slip ring electrical feedthrough sliding contact.
Compared with prior art, the invention has the beneficial effects as follows:
Which solves the difficult problem that state's inner rotary shaft balance loads, improve the precision of rotary shaft balance measurement, fill up The blank of domestic association area.
With same kind of products at abroad contrast, more preferably, using more convenient, maintenance cost is low for efficiency-cost ratio.
Brief description
Fig. 1 is the structural representation of the present invention;
Wherein:1 is stand, and 2 is dynamic load scale pan, and 3 is dynamic loading device, and 4 is rotary shaft balance, and 5 is power output Axle, 6 is small pulley, and 7 is belt, and 8 is shaft coupling, and 9 is slip ring electrical feedthrough, and 10 is big belt wheel, and 11 is motor, and 12 is stand Wheel, 13 is jacking screw rod, and 14 is to load directive wheel.
Specific embodiment
Below in conjunction with the accompanying drawings, the present invention is described in detail.
In order that the objects, technical solutions and advantages of the present invention become more apparent, below in conjunction with drawings and Examples, right The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only in order to explain the present invention, and It is not used in the restriction present invention.
As shown in figure 1, in order to ensure balance can normally run it is necessary to have for passive stand, stand It is welded using rectangle steel, stand not only plays the effect for supporting balance, also act as and drive balance for fixing support The dynamical system rotating.
One motor is fixed with stand, motor is used for providing power output, by big belt wheel by power By on belt transport to small pulley, and small pulley is connected with power output shaft, thus by the power output band of motor Dynamic power output shaft rotates.
Balance uses rotary shaft balance in the present invention, and one end of power output shaft is connected to by rotary shaft balance In dynamic loading device, the power output shaft other end is connected to slip ring by shaft coupling and prints on electrical equipment.Described dynamic loading device Including an outer tube, pass through rolling bearing and rotary shaft sky flushconnection, described outer tube and the rotation being connected with outer tube in outer tube Axle balance in its natural state with plane-parallel.It is connected with the load(ing) point being provided with both direction, a side in outer barrel surface It is connected dynamic load scale pan to the direction vertical with outer tube horizontal positioned, it is loaded in vertical direction;Another will Dynamic load scale pan is connected with the end of outer tube, by loading directive wheel, its outer tube is loaded in the horizontal direction.Work as rotation Rotating shaft balance, in rotation process, can measure the data in both direction by loading.
Rotary shaft balance is freely rotatable in outer tube, and the power applying therefore on outer tube needs defeated by balance by holding wire Go out, the point that balance is contacted with dynamic loading device is exactly the test point of balance, in order to ensure to rotate in rotary shaft balance During signal can export it is therefore desirable to balance is internal and power output shaft inside setting groove make the gentle power in rotary shaft sky Output shaft is hollow axle, and holding wire is from laying in groove so that holding wire and power output shaft rotate together with rotary shaft balance. And signal testing point is set in rotary shaft balance table, holding wire is connected with signal testing point.In the other end of power output, in order to Signal transmission in holding wire is gone out, the surface of power output shaft is also equipped with signal testing point, each signal testing A signal testing point on point corresponding rotation axle balance, shaft coupling is passed through at this end that then power output shaft has signal testing point It is connected with slip ring electrical feedthrough, power output shaft is ceaselessly rotated by shaft coupling in rotation process in slip ring electrical feedthrough Rotating signal is changed into spacing wave, slip ring electrical feedthrough will not be driven in rotation process to rotate, and signal testing point and cunning Signal transmission is gone out by ring electrical feedthrough directly contact by slip ring electrical feedthrough.
In whole system running, the only gentle power output shaft in rotary shaft sky of actual rotation, by driving electricity The driving of machine enables whole rotary shaft balance to reach 10000 revs/min, then it is being carried out add by dynamic loading device Carry different counterweights so that rotary shaft balance can be tested in the little test index of dynamic environment.
The driving of the rotary shaft balance of the present invention relies on belt transmission to realize, and can reduce motor whirling vibration to balance Impact is it is adaptable to precision rotation measurement part drives.Using frequency control motor, it is possible to achieve under rotary shaft balance different rotating speeds The requirement loading is it is ensured that the measurement range of balance;Using the power output shaft with bearing, ensure that output and the letter of power The transmission of number line;The use of slip ring electrical feedthrough, it is ensured that rotating signal transmission, prevents balance signal from disturbing;Using built-in bearing Dynamic load cylinder is it is ensured that apply stable rotating signal to balance;Dynamic load counterweight adopt locking mechanism it is ensured that Counterweight will not be shaked out under shock and vibration;Package unit adopts human engineering optimization design, facilitates the operations such as counterweight plus-minus.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention Any modification, equivalent and improvement made within god and principle etc., should be included within the scope of the present invention.

Claims (7)

1. a kind of rotary shaft balance dynamic loading device is it is characterised in that including stand, the motor being arranged on stand, setting Put the power output shaft in stand upper surface, the clutch end of described motor is connected to power output shaft by belt On, one end of described power output shaft is connected with dynamic loading device by rotary shaft balance, and the other end of power output shaft leads to Cross shaft coupling to be connected on slip ring electrical feedthrough;
Counterweight is loaded respectively with horizontal direction in vertical direction, described dynamic load on the outer tube of described dynamic loading device The outer barrel of device is provided with a set of rolling bearing, and described rotary shaft balance is connected with rolling bearing;
It is provided with holding wire, slided with the balance being arranged in dynamic loading device in one end of holding wire in described rotary balance axle Contact, the other end of holding wire is connected with slip ring electrical feedthrough after power output shaft.
2. a kind of rotary shaft balance dynamic loading device according to claim 1 is it is characterised in that described motor Clutch end is big belt wheel, and one end of power output shaft is small pulley, and described belt is connected in big belt wheel and small pulley.
3. a kind of rotary shaft balance dynamic loading device according to claim 1 is it is characterised in that described rotary shaft balance The contact point of holding wire is respectively arranged with the surface of two ends, between two contact points, connects a holding wire.
4. a kind of rotary shaft balance dynamic loading device according to claim 3 is it is characterised in that described power output shaft Inside it is provided with wire casing, described holding wire is arranged in wire casing.
5. a kind of rotary shaft balance dynamic loading device according to claim 4 is it is characterised in that described power output shaft Inside it is provided with three wire casings, in each wire casing, be provided with a road holding wire.
6. a kind of rotary shaft balance dynamic loading device according to claim 5 is it is characterised in that in rotary shaft balance two The contact point of three holding wires is respectively arranged with the surface of individual end, two corresponding contact points connect a holding wire.
7. according to a kind of arbitrary described rotary shaft balance dynamic loading device of claim 3~6 it is characterised in that described rotation The contact point of axle balance one end and balance sliding contact, the other end of power output shaft and slip ring electrical feedthrough sliding contact.
CN201611029401.5A 2016-11-22 2016-11-22 Rotary shaft translation dynamic loading device Active CN106404342B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611029401.5A CN106404342B (en) 2016-11-22 2016-11-22 Rotary shaft translation dynamic loading device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611029401.5A CN106404342B (en) 2016-11-22 2016-11-22 Rotary shaft translation dynamic loading device

Publications (2)

Publication Number Publication Date
CN106404342A true CN106404342A (en) 2017-02-15
CN106404342B CN106404342B (en) 2020-05-08

Family

ID=58081575

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611029401.5A Active CN106404342B (en) 2016-11-22 2016-11-22 Rotary shaft translation dynamic loading device

Country Status (1)

Country Link
CN (1) CN106404342B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107462395A (en) * 2017-08-16 2017-12-12 中国空气动力研究与发展中心超高速空气动力研究所 Interference coefficient calibration method between a kind of balance component
CN108344556A (en) * 2018-04-28 2018-07-31 中国空气动力研究与发展中心超高速空气动力研究所 A kind of hypersonic wind tunnel balance dynamic characteristic verifying attachment
CN119197986A (en) * 2024-11-26 2024-12-27 中国空气动力研究与发展中心低速空气动力研究所 A six-component dynamic calibration load application device for a rotating axis balance

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020088268A1 (en) * 2001-01-08 2002-07-11 Parker Peter A. Single vector calibration system for multi-axis load cells and method for calibrating a multi-axis load cell
KR20090052094A (en) * 2007-11-20 2009-05-25 한국항공우주연구원 External wind tunnel calibration device
CN104374567A (en) * 2013-08-13 2015-02-25 南车戚墅堰机车车辆工艺研究所有限公司 Rotation torque, radial force and axial force comprehensive loading test method and device
CN204228251U (en) * 2014-12-12 2015-03-25 中国航空工业空气动力研究院 For the charger of wind-tunnel hexa-atomic rod-type balance dynamic calibration
CN105021337A (en) * 2015-07-30 2015-11-04 中国航空工业集团公司哈尔滨空气动力研究所 Propeller driving rotation force measuring apparatus and force measuring method
CN205120335U (en) * 2015-11-27 2016-03-30 中国航空工业集团公司沈阳空气动力研究所 Balance loading head of link model calibration
CN105571813A (en) * 2015-12-29 2016-05-11 中国航天空气动力技术研究院 Wind tunnel balance single-vector calibration loading mechanism
CN106053009A (en) * 2016-07-05 2016-10-26 中国空气动力研究与发展中心超高速空气动力研究所 Piezoelectric balance calibration loading sleeve
CN206348127U (en) * 2016-11-22 2017-07-21 中国空气动力研究与发展中心低速空气动力研究所 A kind of rotary shaft balance dynamic loading device

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020088268A1 (en) * 2001-01-08 2002-07-11 Parker Peter A. Single vector calibration system for multi-axis load cells and method for calibrating a multi-axis load cell
KR20090052094A (en) * 2007-11-20 2009-05-25 한국항공우주연구원 External wind tunnel calibration device
CN104374567A (en) * 2013-08-13 2015-02-25 南车戚墅堰机车车辆工艺研究所有限公司 Rotation torque, radial force and axial force comprehensive loading test method and device
CN204228251U (en) * 2014-12-12 2015-03-25 中国航空工业空气动力研究院 For the charger of wind-tunnel hexa-atomic rod-type balance dynamic calibration
CN105021337A (en) * 2015-07-30 2015-11-04 中国航空工业集团公司哈尔滨空气动力研究所 Propeller driving rotation force measuring apparatus and force measuring method
CN205120335U (en) * 2015-11-27 2016-03-30 中国航空工业集团公司沈阳空气动力研究所 Balance loading head of link model calibration
CN105571813A (en) * 2015-12-29 2016-05-11 中国航天空气动力技术研究院 Wind tunnel balance single-vector calibration loading mechanism
CN106053009A (en) * 2016-07-05 2016-10-26 中国空气动力研究与发展中心超高速空气动力研究所 Piezoelectric balance calibration loading sleeve
CN206348127U (en) * 2016-11-22 2017-07-21 中国空气动力研究与发展中心低速空气动力研究所 A kind of rotary shaft balance dynamic loading device

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
周全: ""变负载情况下风洞应变天平动态特性研究"", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *
张洋 等: ""内埋武器分离试验天平动态校准试验研究"", 《中国空气动力学会测控技术专委会第六届四次学术交流会论文集》 *
杨恩霞 等: ""低速风洞旋转天平试验装置的设计"", 《应用科技》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107462395A (en) * 2017-08-16 2017-12-12 中国空气动力研究与发展中心超高速空气动力研究所 Interference coefficient calibration method between a kind of balance component
CN107462395B (en) * 2017-08-16 2019-03-19 中国空气动力研究与发展中心超高速空气动力研究所 Interference coefficient calibration method between a kind of balance component
CN108344556A (en) * 2018-04-28 2018-07-31 中国空气动力研究与发展中心超高速空气动力研究所 A kind of hypersonic wind tunnel balance dynamic characteristic verifying attachment
CN119197986A (en) * 2024-11-26 2024-12-27 中国空气动力研究与发展中心低速空气动力研究所 A six-component dynamic calibration load application device for a rotating axis balance
CN119197986B (en) * 2024-11-26 2025-02-28 中国空气动力研究与发展中心低速空气动力研究所 A six-component dynamic calibration load application device for a rotating axis balance

Also Published As

Publication number Publication date
CN106404342B (en) 2020-05-08

Similar Documents

Publication Publication Date Title
CN101487751B (en) Measuring apparatus for frictional moment of bearing under different axial loads and rotation speeds
CN201364215Y (en) Friction moment measuring device of bearing under different axial loads and rotating speed
CN106017928B (en) Bearing swinging test device
CN206348127U (en) A kind of rotary shaft balance dynamic loading device
CN104848990B (en) A kind of ultraprecise dynamic poise device suitable for miniature rotor
CN203100949U (en) Rolling bearing friction moment measuring device under low-speed medium-heavy load
CN106404342A (en) Dynamic loading device for rotary shaft balance
CN107314851A (en) Linear motor thrust testing device and the method using the measurement device force oscillation
CN111964864B (en) Balance rotation calibration loading device and calibration loading method for wind tunnel test bed of helicopter
CN105092236B (en) A kind of device and method for testing eddy current damper damping due to rotation coefficient
CN107719696A (en) A kind of dynamic characteristics synchronous testing device of axially compact type aircraft propeller
CN103528741A (en) Device and method for testing friction torque of bearing under actual working condition
CN107884185A (en) Single-stage double helical tooth planetary drive dynamics features Testbed
CN109342060A (en) The test device of axial bearing foil
CN107356369A (en) A kind of hydraulic dynamometer measures calibration system
CN205209615U (en) Controllable formula aircraft weighting device
CN102607749A (en) Device for measuring friction moment of roller bearing
CN110542556A (en) A tilting pad sliding bearing test box, test bench and test method
CN110426147A (en) The device and method of deep groove ball bearing moment of friction are measured under gravity or microgravity
CN210487269U (en) Tilting pad sliding bearing test box and test bench
CN111805497A (en) An electric manual three-axis turntable
CN207114093U (en) A kind of hydraulic dynamometer measures calibration system
CN209102378U (en) The test device of axial bearing foil
CN203606053U (en) Testing device for friction torque under actual working condition of bearing
CN203376110U (en) Torque verification device of torque sensor

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant