CN104444937A - Combined lifting mechanism - Google Patents

Combined lifting mechanism Download PDF

Info

Publication number
CN104444937A
CN104444937A CN201410700901.1A CN201410700901A CN104444937A CN 104444937 A CN104444937 A CN 104444937A CN 201410700901 A CN201410700901 A CN 201410700901A CN 104444937 A CN104444937 A CN 104444937A
Authority
CN
China
Prior art keywords
lifting mechanism
lead screw
power transmission
force transfer
screw
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
CN201410700901.1A
Other languages
Chinese (zh)
Other versions
CN104444937B (en
Inventor
吴国平
余洪
王福平
邓昕
巴洪
李皊
胡秀军
杨力萌
阿西达
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.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
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 Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201410700901.1A priority Critical patent/CN104444937B/en
Publication of CN104444937A publication Critical patent/CN104444937A/en
Application granted granted Critical
Publication of CN104444937B publication Critical patent/CN104444937B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F7/00Lifting frames, e.g. for lifting vehicles; Platform lifts
    • B66F7/06Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement
    • B66F7/08Lifting frames, e.g. for lifting vehicles; Platform lifts with platforms supported by levers for vertical movement hydraulically or pneumatically operated

Landscapes

  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Geology (AREA)
  • Mechanical Engineering (AREA)
  • Structural Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

A combined lifting mechanism comprises a shear fork lifting mechanism body and a lead screw lifting mechanism body. In the shear fork lifting mechanism body, roller wheels are installed on a force transfer base, one end of each shear fork arm assembly is connected with a lead screw installed on the force transfer base, the other end of each shear fork arm assembly is connected with a lifting table, and a rotating rocker arm is installed on one side of the force transfer base and connected with the lead screw. In the lead screw lifting mechanism body, a trapezoidal lead screw penetrates through the lifting table and is hinged to the lead screw, and a hand wheel is installed on the trapezoidal lead screw. The initial installation height of the lead screw lifting mechanism body is increased through the shear fork lifting mechanism body, equipment can be lifted in a narrow space, the combined lifting mechanism is convenient and fast to use, and the maintaining efficiency of an airplane can be improved substantially. Furthermore, the force transfer base is provided with guide grooves, sleeves roll in the guide grooves of the force transfer base through bearings arranged at the two ends of each sleeve, in this way, the angle between square-tube shear fork arms is changed, ascending or descending of the lifting table is achieved, and the two lifting mechanism bodies do not depend on each other during ascending and descending; besides, the combined lifting mechanism is simple in structure and convenient and fast to use; meanwhile, as the roller wheels are arranged on the force transfer base, working efficiency can be effectively improved.

Description

A kind of combination lifting mechanism
Technical field
The present invention relates to mechanical lifting gear technical field, particularly relate to a kind of combination lifting mechanism.
Background technology
In aircraft utilization handling labor, often to need under ventral loader-unloader in small space to carry equipment, and for the larger equipment of quality, be difficult to handling labor, usually needed by lifting mechanism, equipment larger for quality to be held up.At present conventional two kinds single lifting mechanisms: one is screw lift structure, has structure simple, can in small space the feature of lifting equipment, but lifting travel is by the restriction of installing elemental height; Two is scissor-type lifting mechanisms, but structure takes up room comparatively large, and use operation has certain limitation, is difficult to the installation requirements meeting small space.
Summary of the invention
Technical matters solved by the invention is to provide a kind of combination lifting mechanism, to solve the shortcoming in above-mentioned background technology.
Technical matters solved by the invention realizes by the following technical solutions:
A kind of combination lifting mechanism, comprises scissors fork elevating mechanism, screw lift structure; Wherein, in scissors fork elevating mechanism, roller is arranged on power transmission base, and scissor arm component one end is connected with the screw mandrel be arranged on power transmission base, and the other end is connected with bay-lift, rotates rocking arm and is arranged on power transmission base side, and be connected with screw mandrel; In screw lift structure, trapezoidal screw through bay-lift and screw mandrel hinged, handwheel is arranged on trapezoidal screw, by scissors fork elevating mechanism with the installation elemental height of enhancing screw lifting mechanism, can in small space lifting equipment, easy to use, the maintenance efficiency of aircraft can be increased substantially; In addition, power transmission base is provided with guide groove.
In the present invention, scissor arm component comprises a prescription pipe scissor arm, and is bolted between square tube scissor arm, has the advantage of stabilized structure, reliable, safe and efficient, failure rate is low; Simultaneously annex installing space size Selection square tube scissor brachium can be become short or adopt two-stage scissor with aircraft according to lifting travel.
In the present invention, screw mandrel is set with sleeve, sleeve embeds in the guide groove of power transmission base by the bearing that two ends are arranged, the screw mandrel on power transmission base is driven to rotate by rotating rocking arm, sleeve bearings at both ends is rolled in guide groove, thus the angle changed between square tube scissor arm realizes rise or the reduction of bay-lift.
In the present invention, power transmission base is provided with reinforced rib, is conducive to the stability of power transmission base.
In the present invention, trapezoidal screw is at right angle setting, takies volume little, can according to rest object and installing space size design pallet size thereof; Simultaneously the Design of length of trapezoidal screw will meet two aspects and requires: one is scissors fork elevating mechanism when dropping to minimum, can not contact to earth in trapezoidal screw bottom; Two is scissors fork elevating mechanism and screw lift structure two-stage lifting mechanism when all dropping to minimum, under installation car can enter into ventral.
In the present invention, roller is arranged on the bearing of power transmission base extension setting.
Beneficial effect: the present invention is combined by scissors fork elevating mechanism and screw lift structure, the bearing that sleeve is arranged by two ends rolls in the guide groove of power transmission base, thus the angle changed between square tube scissor arm realizes rise or the reduction of bay-lift, do not rely on mutually during the lifting of two-stage lifting mechanism; And structure is simple, easy to use, the maintenance efficiency of aircraft can be increased substantially; On power transmission base, be provided with roller simultaneously, effectively improve work efficiency.
Accompanying drawing explanation
Fig. 1 is the structural representation of preferred embodiment of the present invention.
Detailed description of the invention
The technological means realized to make the present invention, creation characteristic, reaching object and effect is easy to understand, below in conjunction with concrete diagram, setting forth the present invention further.
See the one combination lifting mechanism of Fig. 1, comprise scissors fork elevating mechanism 10, rotate rocking arm 11, screw mandrel 12, square tube scissor arm component 13, bolt 14, bay-lift 15, power transmission base 16, roller 17, screw lift structure 20, handwheel 21 and trapezoidal screw 22.
In scissors fork elevating mechanism 10, roller 17 is arranged on power transmission base 16, square tube scissor arm component 13 one end is connected with the screw mandrel 12 be arranged on power transmission base 16, the other end is connected with bay-lift 15, square tube scissor arm in square tube scissor arm component 13 is connected by bolt 14, rotate rocking arm 11 and be arranged on power transmission base 16 side, and be connected with screw mandrel 12; In real work, annex installing space size can be become to carry out appropriate design square tube scissor brachium with aircraft according to lifting travel short or adopt two-stage scissor, the screw mandrel 12 on power transmission base 16 is driven to rotate by rotating rocking arm 11, screw mandrel 12 is set with sleeve, sleeve bearings at both ends is rolled in the guide groove of power transmission base 16, thus between change scissor arm, angle realizes rise or the reduction of bay-lift 15.
In screw lift structure 20, trapezoidal screw 22 is hinged through bay-lift 15 and screw mandrel 12, handwheel 21 is arranged on trapezoidal screw 22, by the installation elemental height of scissors fork elevating mechanism 10 enhancing screw lifting mechanism 20, can in small space lifting equipment, easy to use, the maintenance efficiency of aircraft can be increased substantially.
In the present embodiment, trapezoidal screw 22 at right angle setting, its Design of length will meet two aspects and require: one is scissors fork elevating mechanism 10 when dropping to minimum, can not contact to earth in trapezoidal screw 22 bottom; Two is scissors fork elevating mechanisms 10 when all dropping to minimum with screw lift structure 20 two-stage lifting mechanism, under installation car can enter into ventral; By rotation hand wheel 21, trapezoidal screw 22 moved up and down thus drive pallet to rise or reduce, because trapezoidal screw 22 is at right angle setting, taking volume little, pallet size can be designed according to rest object and installing space size thereof simultaneously.
More than show and describe groundwork of the present invention and principal character and advantage of the present invention.The technical personnel of the industry should be understood; the present invention is not restricted to the described embodiments; what describe in above-described embodiment and specification sheets just illustrates principle of the present invention; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements all fall in the claimed scope of the invention.Application claims protection domain is defined by appending claims and equivalent thereof .

Claims (6)

1. combine a lifting mechanism, comprise scissors fork elevating mechanism, screw lift structure; It is characterized in that, in scissors fork elevating mechanism, roller is arranged on power transmission base, and scissor arm component one end is connected with the screw mandrel be arranged on power transmission base, and the other end is connected with bay-lift, rotates rocking arm and is arranged on power transmission base side, and be connected with screw mandrel; In screw lift structure, trapezoidal screw through bay-lift and screw mandrel hinged, handwheel is arranged on trapezoidal screw; In addition, power transmission base is provided with guide groove.
2. one combination lifting mechanism according to claim 1, it is characterized in that, scissor arm component comprises a prescription pipe scissor arm, and is bolted between square tube scissor arm.
3. one combination lifting mechanism according to claim 1, is characterized in that, screw mandrel is set with sleeve.
4. one combination lifting mechanism according to claim 3, it is characterized in that, the bearing that sleeve is arranged by two ends embeds in the guide groove of power transmission base.
5. one combination lifting mechanism according to claim 1, is characterized in that, power transmission base is provided with reinforced rib.
6. one combination lifting mechanism according to claim 1, it is characterized in that, trapezoidal screw is at right angle setting.
CN201410700901.1A 2014-11-28 2014-11-28 One kind combination elevating mechanism Active CN104444937B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410700901.1A CN104444937B (en) 2014-11-28 2014-11-28 One kind combination elevating mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410700901.1A CN104444937B (en) 2014-11-28 2014-11-28 One kind combination elevating mechanism

Publications (2)

Publication Number Publication Date
CN104444937A true CN104444937A (en) 2015-03-25
CN104444937B CN104444937B (en) 2017-11-03

Family

ID=52891809

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410700901.1A Active CN104444937B (en) 2014-11-28 2014-11-28 One kind combination elevating mechanism

Country Status (1)

Country Link
CN (1) CN104444937B (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105645306A (en) * 2016-01-12 2016-06-08 深圳市华星光电技术有限公司 Lifting device
CN106835991A (en) * 2017-02-25 2017-06-13 江西省公路工程检测中心 A kind of overhead bridge construction climbing device
CN107054687A (en) * 2017-06-19 2017-08-18 沈阳飞机工业(集团)有限公司 A kind of big stroke aircraft bracket of low clearance
CN107140574A (en) * 2017-06-26 2017-09-08 江苏木盟智能科技有限公司 Combined type lifting platform and mobile robot
WO2018171104A1 (en) * 2017-03-21 2018-09-27 深圳市鑫宝临五金有限公司 Lifting mechanism
CN108638556A (en) * 2018-03-23 2018-10-12 合肥国轩高科动力能源有限公司 Discharging device of roller press
CN110127403A (en) * 2018-02-02 2019-08-16 海德堡印刷机械股份公司 Stacking apparatus for page
CN111482933A (en) * 2020-04-21 2020-08-04 郑秀菊 Ground support device for dismounting airborne radar
CN112524526A (en) * 2020-11-30 2021-03-19 九江职业技术学院 Multifunctional ambient light simulation device for indoor design

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285992A (en) * 1992-07-14 1994-02-15 Brown Ronald G Adjustable step stool
JP2002159539A (en) * 2000-11-27 2002-06-04 Toshiba Corp Bed device for medical device
CN101195467A (en) * 2007-12-28 2008-06-11 上海微电子装备有限公司 Shear type hoisting device
CN202687873U (en) * 2012-06-11 2013-01-23 东方电气集团东方汽轮机有限公司 Shear fork lifting type on-site maintenance platform
CN103613045A (en) * 2013-11-28 2014-03-05 国家电网公司 Manual lifting platform
CN103776736A (en) * 2014-02-20 2014-05-07 许虹怡 Lining viscosity measurement instrument
CN104016264A (en) * 2014-06-11 2014-09-03 济南华北升降平台制造有限公司 Lifting platform for steel mill maintenance
CN204281190U (en) * 2014-11-28 2015-04-22 江西洪都航空工业集团有限责任公司 A kind of combination lifting mechanism

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285992A (en) * 1992-07-14 1994-02-15 Brown Ronald G Adjustable step stool
JP2002159539A (en) * 2000-11-27 2002-06-04 Toshiba Corp Bed device for medical device
CN101195467A (en) * 2007-12-28 2008-06-11 上海微电子装备有限公司 Shear type hoisting device
CN202687873U (en) * 2012-06-11 2013-01-23 东方电气集团东方汽轮机有限公司 Shear fork lifting type on-site maintenance platform
CN103613045A (en) * 2013-11-28 2014-03-05 国家电网公司 Manual lifting platform
CN103776736A (en) * 2014-02-20 2014-05-07 许虹怡 Lining viscosity measurement instrument
CN104016264A (en) * 2014-06-11 2014-09-03 济南华北升降平台制造有限公司 Lifting platform for steel mill maintenance
CN204281190U (en) * 2014-11-28 2015-04-22 江西洪都航空工业集团有限责任公司 A kind of combination lifting mechanism

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105645306A (en) * 2016-01-12 2016-06-08 深圳市华星光电技术有限公司 Lifting device
CN106835991A (en) * 2017-02-25 2017-06-13 江西省公路工程检测中心 A kind of overhead bridge construction climbing device
WO2018171104A1 (en) * 2017-03-21 2018-09-27 深圳市鑫宝临五金有限公司 Lifting mechanism
CN107054687A (en) * 2017-06-19 2017-08-18 沈阳飞机工业(集团)有限公司 A kind of big stroke aircraft bracket of low clearance
CN107140574A (en) * 2017-06-26 2017-09-08 江苏木盟智能科技有限公司 Combined type lifting platform and mobile robot
CN110127403A (en) * 2018-02-02 2019-08-16 海德堡印刷机械股份公司 Stacking apparatus for page
CN108638556A (en) * 2018-03-23 2018-10-12 合肥国轩高科动力能源有限公司 Discharging device of roller press
CN111482933A (en) * 2020-04-21 2020-08-04 郑秀菊 Ground support device for dismounting airborne radar
CN112524526A (en) * 2020-11-30 2021-03-19 九江职业技术学院 Multifunctional ambient light simulation device for indoor design

Also Published As

Publication number Publication date
CN104444937B (en) 2017-11-03

Similar Documents

Publication Publication Date Title
CN104444937A (en) Combined lifting mechanism
CN102704664B (en) Self-lifting quick transferring platform
CN204138268U (en) A kind of lifting table
CN103010658B (en) A kind of rise and fall roller device
CN103272892A (en) Straightener capable of changing rolls quickly
CN204038338U (en) The tower roller conveyor of spiral
CN103663257A (en) Electric lifting platform
CN204281190U (en) A kind of combination lifting mechanism
CN205527540U (en) Novel manual hydraulic lifting platform
CN202704929U (en) Bidirectional mechanical lifting jack
CN204237530U (en) A kind of small size light platform car
CN204848016U (en) Portable cantilever crane of platform truck
CN204185147U (en) Three-dimensional adjustable hoisting crane
CN204297966U (en) Adjustable glass suspension transferring machine
CN205032909U (en) Fan aggregate erection is with special pressure equipment machine
CN205677557U (en) A kind of scissor drilling tool lifting device
CN204324164U (en) A kind of warming plate conveying roll
CN208648593U (en) A kind of four cylinder lifting devices for mine underground work
CN204702153U (en) A kind of adjustable height movable conveyer
CN202208625U (en) Hydraulic lifting platform of hydraulic control system
CN206901681U (en) A kind of hydraulic elevating platform
CN205555887U (en) Double -girder crane
CN204220713U (en) A kind of coiler bottom working roll elevating mechanism
CN205166881U (en) Lift platform with safe support
CN204777559U (en) Discharge apparatus

Legal Events

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