CN104006965A - Screw type torque self-loading device - Google Patents

Screw type torque self-loading device Download PDF

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Publication number
CN104006965A
CN104006965A CN201410233313.1A CN201410233313A CN104006965A CN 104006965 A CN104006965 A CN 104006965A CN 201410233313 A CN201410233313 A CN 201410233313A CN 104006965 A CN104006965 A CN 104006965A
Authority
CN
China
Prior art keywords
output shaft
input shaft
shell
housing
control tube
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.)
Pending
Application number
CN201410233313.1A
Other languages
Chinese (zh)
Inventor
刘刚
赖锋
刘兆晶
王瑛
邹璇
黄莹莹
左晓镭
孙向志
王苏鸣
徐天龙
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.)
Harbin Guang Han power transmission Co., Ltd
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 CN201410233313.1A priority Critical patent/CN104006965A/en
Publication of CN104006965A publication Critical patent/CN104006965A/en
Pending legal-status Critical Current

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Abstract

The invention provides a screw type torque self-loading device. Trapezoidal threads are formed on the inner surface of a pipe wall of a shell. The shell is connected with a control tube through the trapezoidal threads in a threaded mode. A flat key groove is formed in one side of an inner hole of the control tube, and the flat key groove is connected with an input shaft in a sliding and matched mode through a guide key. A guide boss extends out from the left side of the inner hole of the control tube. The guide boss is connected with a screw guide groove formed in an output shaft in a clearance fit mode. The butt joint portions of the output shaft and the input shaft are connected through a push-and-pull bearing. The butt joint axial distance between the output shaft and the input shaft is determined according to the distance between step shafts on the shafts and the end caps arranged at the two ends of the shell. The portion, extending out of one end cap of the shell, of the output shaft and the portion, extending out of the other end cap of shell, of the input shaft are respectively provided with a flange. A plurality of countersinks are formed in the outer cylindrical surface of the shell in the circumferential direction. The outer cylindrical surface of the shell and a friction sheet control mechanism are connected in a matched mode. The screw type torque self-loading device is easy to machine, convenient to install and detach, small in size, light in weight, and capable of being used reliably for a long time.

Description

Spiral moment of torsion bootstrap loading device
technical field:
The present invention is a kind of charger of gear drive blocking test platform, is specifically related to a kind of spiral moment of torsion bootstrap loading device.
background technology:
Torque loading device is mainly used in load test on the road of key components and parts in marine system and aerospace system, Mobile Power Transmission test, the transmission test of high-precision high-speed equipment, the fields such as detection of high precision instrument, along with China is in recent years under the environment of the input construction of naval and air force and development proprietary technology equipment, demand and the application of charger constantly increase, and its type and technical parameter demand constantly improve.Some research institutions and institution of higher learning have all carried out research to blocking test platform technology and loader technology both at home and abroad, as U.S. Gleason company has just designed the mechanical close formula testing table of the loader that adopts train composition at the fifties.In addition, also have USSR (Union of Soviet Socialist Republics) central robot designing for manufacturing office, research centre, American National space agency (NASA) subordinate Golan, German Lun Ke company, AM General utility companies, Toyota Motor company, Illinois, US university, popular Skoda company etc., a large amount of research has all been carried out in the design that forms loader from the structure of testing table, and has formed certain Design Mode.At home, mainly that some colleges and universities and research institute have carried out research work as required in good time, do not form tandem product, development especially for High speed load device is domestic also in space state, the present invention is directed to the demand that in air line, key components and parts needs high speed blocking test to load, a kind of moment of torsion bootstrap loading device has been proposed, it is simple that this invention has mechanism, add carried convenient, in loading procedure, dynamic balance is good, be applicable to that hypervelocity blocking test platform loads and high-power under load test.
summary of the invention:
In order to meet the moment of torsion of high speed, high-power gear drive blocking test platform, load requirement, improve the loading efficiency of gear drive blocking test platform, the invention provides a kind of torque loading device for High Speed Gearing blocking test platform.
The present invention solves the problems of the technologies described above the technical scheme of taking to be: spiral moment of torsion bootstrap loading device, comprise housing, housing inner surface of tube wall has acme thread, housing is threaded with control tube by acme thread, control tube endoporus one side has between flat key groove and input shaft by feather key sliding connection, a guide ledges is extended in the endoporus left side of control tube, between guide ledges and the spiral guide slot of outputing on output shaft, clearance fit is connected, output shaft is connected by push-and-pull bearing with input shaft butted part, the axial distance of output shaft and input shaft docking is determined by the distance between the Step Shaft on axle and the end cap at housing two ends, output shaft and input shaft stretch out housing end plug and are partly respectively equipped with flange, housing outer cylinder surface circumferencial direction has some counterbores, housing outer cylinder surface and friction disc control gear are connected.
The present invention has following beneficial effect: the processing of this device is simple, easy installation and removal, volume are little, lightweight, can use stably in a long term.
accompanying drawing explanation:
Fig. 1 structural representation of the present invention.
1-output shaft in figure, 2-control tube, 3-housing, 4-push-and-pull bearing, 5-friction disc control gear, 6-feather key, 7-input shaft, 8-counterbore, 9-gathering sill, 10-acme thread, 11-guide ledges.
Embodiment:
Below in conjunction with accompanying drawing, the invention will be further described:
As shown in Figure 1, spiral moment of torsion bootstrap loading device, comprise housing 3, housing 3 inner surface of tube wall have acme thread 10, housing 3 is threaded with control tube 2 by acme thread 10, control tube 2 endoporus one sides have between flat key groove and input shaft 7 by feather key 6 sliding connections, a guide ledges 11 is extended in the endoporus left side of control tube 2, between guide ledges 11 and the spiral guide slot 9 of outputing on output shaft 1, clearance fit is connected, output shaft 1 is connected by push-and-pull bearing 4 with input shaft 7 butted parts, the axial distance of output shaft 1 and input shaft 7 docking is determined by the distance between the Step Shaft on axle and the end cap at housing 3 two ends, output shaft 1 and input shaft 7 stretch out housing 3 end caps and are partly respectively equipped with flange, housing 3 outer cylinder surface circumferencial directions have some counterbores 8, housing 3 outer cylinder surfaces and friction disc control gear 5 are connected.
Input shaft 7 is connected with blocking test system by two end flanges with output shaft 1, between input shaft 7 and output shaft 1, by control tube 2, be connected, power passes to output shaft 1 by input shaft 7 by control tube 2, during roll-shell 3, can realize the axially-movable of control tube 2, feather key 6 between control tube 2 and input shaft 7, restriction control tube 2 can only move axially along input shaft 7.Control tube 2 is when axially-movable, the guide ledges 11 of control tube front end is moved along output shaft spiral guide slot 9, spiral guide slot 9 on output shaft is arranged at an angle on output shaft 1 surface, like this at control tube 2 simultaneously in axial sliding, output shaft 1 circumferentially has certain rotation, can realize the axially-movable of control tube 2 when roll-shell 3.
Housing both sides are circumferentially with spanner interface, and manual wrench is inserted in counterbore 8, rotate backward housing 3, and housing 3 drives control tube 2 drawback movements by acme thread 10, and output shaft 1 reverse rotation is by the moment of torsion unloading loading.
Clockwise transmission when loader is seen from input end (right side), drives control tube 2 rotations by feather key 6 when input shaft 7 rotates, and control tube 2 drives output shaft 1 rotation by spiral guide slot 9, realizes power transmission.
Static loading process: input shaft 7 maintains static, manual wrench is inserted in counterbore 8, (from input end) roll-shell 3 counterclockwise, housing 3 drives control tube 2 to move to input end along axial direction by acme thread 10, when control tube 2 moves, guide ledges 11 is moved along gathering sill 9, drive output shaft 1 to clockwise rotate, system is loaded.The distance that the angle loading is moved by angle and the control tube 2 of spiral chute 9 determines.
Dynamic load process: during the clockwise transmission of whole loader, control 5 pairs of housings 3 of friction disc mechanism and apply certain friction force, make housing 3 and input shaft 7 produce speed discrepancy, control tube 2 is synchronizeed rotation with input shaft 7, therefore housing 3 has generation speed discrepancy with control tube 2, by screw thread, control tube 2 is moved towards input end, and then drive spiral guide slot 9 to rotate, output shaft 1 relative input shaft (7) is rotated and realize loading, loading velocity is by the decision of friction force size, and the large loading velocity of speed discrepancy that friction force makes greatly control tube 2 and housing 3 produce is just fast.
Uninstall process: when system experimentation is complete need to unload moment of torsion time, manual wrench is inserted in counterbore 8, (from input end) roll-shell 3 clockwise, housing 3 drives control tube 2 drawback movements by acme thread 10, and the relative input shaft 7 of output shaft 1 is rotated counterclockwise the moment of torsion loading is unloaded.
The more traditional charger structure compared of this charger is compact simple, and dynamic balance easy to process is better, can be applied in higher rotating speed blocking test.

Claims (1)

1. a spiral moment of torsion bootstrap loading device, comprise housing (3), it is characterized in that: housing (3) inner surface of tube wall has acme thread (10), housing (3) is threaded with control tube (2) by acme thread (10), control tube (2) endoporus one side has between flat key groove and input shaft (7) by feather key (6) sliding connection, a guide ledges (11) is extended in the endoporus left side of control tube (2), between guide ledges (11) and the spiral guide slot (9) of outputing on output shaft (1), clearance fit is connected, output shaft (1) is connected by push-and-pull bearing (4) with input shaft (7) butted part, the axial distance of output shaft (1) and input shaft (7) docking is determined by the distance between the Step Shaft on axle and the end cap at housing (3) two ends, output shaft (1) and input shaft (7) stretch out housing (3) end cap and are partly respectively equipped with flange, housing (3) outer cylinder surface circumferencial direction has some counterbores (8), housing (3) outer cylinder surface and friction disc control gear (5) are connected.
CN201410233313.1A 2014-05-29 2014-05-29 Screw type torque self-loading device Pending CN104006965A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410233313.1A CN104006965A (en) 2014-05-29 2014-05-29 Screw type torque self-loading device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410233313.1A CN104006965A (en) 2014-05-29 2014-05-29 Screw type torque self-loading device

Publications (1)

Publication Number Publication Date
CN104006965A true CN104006965A (en) 2014-08-27

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410233313.1A Pending CN104006965A (en) 2014-05-29 2014-05-29 Screw type torque self-loading device

Country Status (1)

Country Link
CN (1) CN104006965A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4435988A (en) * 1981-07-13 1984-03-13 The Geolograph Company Apparatus for indicating critical torque load
JPS61155930A (en) * 1984-12-28 1986-07-15 Sakai Seisakusho:Kk Torque detection sensor of rotary transmission mechanism
CN1789759A (en) * 2005-12-19 2006-06-21 湖南大学 Circulating ball type automatic loader
CN2881598Y (en) * 2006-03-09 2007-03-21 中国船舶重工集团公司第七一一研究所 Screw type load shelf
CN101339094A (en) * 2008-09-01 2009-01-07 洛阳工铭机电设备有限公司 Helicopter automatic tilting device large-sized thin-wall bearing intelligent checking analytical method and device
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
CN203837913U (en) * 2014-05-29 2014-09-17 中国船舶重工集团公司第七�三研究所 Spiral torque self-loading device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4435988A (en) * 1981-07-13 1984-03-13 The Geolograph Company Apparatus for indicating critical torque load
JPS61155930A (en) * 1984-12-28 1986-07-15 Sakai Seisakusho:Kk Torque detection sensor of rotary transmission mechanism
CN1789759A (en) * 2005-12-19 2006-06-21 湖南大学 Circulating ball type automatic loader
CN2881598Y (en) * 2006-03-09 2007-03-21 中国船舶重工集团公司第七一一研究所 Screw type load shelf
CN101339094A (en) * 2008-09-01 2009-01-07 洛阳工铭机电设备有限公司 Helicopter automatic tilting device large-sized thin-wall bearing intelligent checking analytical method and device
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
CN203837913U (en) * 2014-05-29 2014-09-17 中国船舶重工集团公司第七�三研究所 Spiral torque self-loading device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王正玲: "螺旋滚珠式机械加载器在封闭试验台中的应用", 《实验技术与管理》, vol. 10, no. 4, 31 December 1993 (1993-12-31), pages 50 - 54 *

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
ASS Succession or assignment of patent right

Owner name: HARBIN GUANGHAN POWER TECHNOLOGY DEVELOPMENT CO.,

Free format text: FORMER OWNER: CHINA SHIPBUILDING INDUSTRY CORPORATION THE 7TH 03 RESEARCH CENTER

Effective date: 20150407

C41 Transfer of patent application or patent right or utility model
TA01 Transfer of patent application right

Effective date of registration: 20150407

Address after: 150000, No. 35, Honghu Road, Yingbin Road, Harbin, Heilongjiang, 7

Applicant after: Harbin Guang Han power transmission Co., Ltd

Address before: 150000 No. 35, Honghu Road, Yingbin Road, Harbin hi tech Development Zone, Heilongjiang, China

Applicant before: No.703 Inst. China Ship Heavy Industry Group Co.

C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140827