CN214733999U - Big arm section bar structure of lifting mechanism - Google Patents

Big arm section bar structure of lifting mechanism Download PDF

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Publication number
CN214733999U
CN214733999U CN202120270398.6U CN202120270398U CN214733999U CN 214733999 U CN214733999 U CN 214733999U CN 202120270398 U CN202120270398 U CN 202120270398U CN 214733999 U CN214733999 U CN 214733999U
Authority
CN
China
Prior art keywords
big arm
section bar
lifting mechanism
lifting
boom
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.)
Active
Application number
CN202120270398.6U
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Chinese (zh)
Inventor
单萍
王健
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.)
Jiangsu Tianyi Aviation Industry Co Ltd
Original Assignee
Jiangsu Tianyi Airport Special Equipment 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.)
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Publication date
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Priority to CN202120270398.6U priority Critical patent/CN214733999U/en
Application granted granted Critical
Publication of CN214733999U publication Critical patent/CN214733999U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to airport lifting device field discloses a lifting mechanism big arm section bar structure, two fixed cross supports on the frame, and the support is including lifting big arm, and its characterized in that lifts big arm both ends and is the arc structure, lifts and has seted up a plurality of through-holes on the big arm. The volume is obviously reduced, and the requirement of operation intensity is met.

Description

Big arm section bar structure of lifting mechanism
The technical field is as follows:
the utility model belongs to airport lifting device field, concretely relates to lifting mechanism forearm section bar structure.
Background art:
the existing trip of people is mostly realized by adopting airplane flight, a large-arm section bar is a main section bar of a lifting mechanism of airport equipment, a fork frame type structure formed by the section bars is fixed on a frame, and the opening angle of the fork frame type structure is changed by utilizing an oil cylinder so as to achieve the lifting effect. The box on the large arm and the load thereof have relatively large weight, so the requirements on the strength and the stability of the large arm are relatively high. As shown in fig. 1 and 2, the existing large arm section bar is generally of a hollow structure, and has unreasonable structure and poor strength, so that the lifting requirements of airports are difficult to load.
The utility model has the following contents:
the utility model aims at overcoming prior art's defect, provides a lifting mechanism forearm section bar structure, relates to lifting equipment, specifically is a structure based on section bar structure's change self is strengthened, makes the section bar of lifting usefulness at the apparent reduction in volume, and reaches the requirement of operation intensity.
In order to solve the technical problem, the utility model provides a following technical scheme:
the utility model provides a lifting mechanism big arm section bar structure, two crossing supports of fixing on the frame, the support is including lifting big arm 1, its characterized in that, lifts big arm both ends and is the arc structure, lifts to have seted up a plurality of through-holes on the big arm.
Preferably, the lifting boom 1 is of an integral middle-shaped structure and is composed of flat plates with channel steel fixedly welded on both sides.
Preferably, the flat sheet width is greater than the channel width.
Preferably, the channel steel is a bent groove type plate.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model adopts the material to be folded into the channel steel type, and the structure is utilized to strengthen the first step; two bending groove type panels are fixed on a flat plate, and the integral structural strength is further improved.
Drawings
FIG. 1 shows a normal profile used in the past;
figure 2 is a cross-sectional view of a normal profile.
FIG. 3 is a plan view of the boom section of the lifting mechanism of the present invention;
FIG. 4 is a sectional view of a boom section of the lifting mechanism of the present invention;
Detailed Description
For a better explanation of the invention, reference is made to the following detailed description taken in conjunction with the accompanying drawings.
The embodiment is shown in fig. 3-4, a profile structure of a large arm of a lifting mechanism, which comprises two crossed brackets fixed on a frame, wherein each bracket comprises a lifting large arm 1, two ends of each lifting large arm are of arc structures, and a plurality of through holes are formed in each lifting large arm. The lifting boom 1 is of an integral middle-shaped structure and is composed of flat plates with channel steel fixedly welded on two sides. The width of the flat plate is larger than that of the channel steel, and the channel steel is a bent groove type plate.
This novel combined section bar self intensity, in addition the reinforcing combination welding of muscle board-like for holistic intensity, rigidity obtain promoting.
The above description is only for the purpose of illustrating embodiments of the present invention and should not be taken as limiting the invention, and any modifications, equivalents, improvements and the like made by those skilled in the art within the spirit and principle of the present invention should be included in the scope of the present invention.

Claims (4)

1. The utility model provides a lifting mechanism big arm section bar structure, two crossing supports of fixing on the frame, the support is including lifting big arm, its characterized in that lifts big arm both ends and is the arc structure, lifts to have seted up a plurality of through-holes on the big arm.
2. The boom structure of claim 1, wherein the boom 1 is a unitary medium-shaped structure, and is made of a flat plate with channel steel welded to both sides.
3. The boom section structure of claim 2 wherein the width of the flat section is greater than the width of the channel.
4. The boom structure of claim 2, wherein the channel is a bent channel type plate.
CN202120270398.6U 2021-02-01 2021-02-01 Big arm section bar structure of lifting mechanism Active CN214733999U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120270398.6U CN214733999U (en) 2021-02-01 2021-02-01 Big arm section bar structure of lifting mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120270398.6U CN214733999U (en) 2021-02-01 2021-02-01 Big arm section bar structure of lifting mechanism

Publications (1)

Publication Number Publication Date
CN214733999U true CN214733999U (en) 2021-11-16

Family

ID=78643203

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120270398.6U Active CN214733999U (en) 2021-02-01 2021-02-01 Big arm section bar structure of lifting mechanism

Country Status (1)

Country Link
CN (1) CN214733999U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 224001 No.2 Hangkong Road, high tech Industrial Zone, Jianhu County, Yancheng City, Jiangsu Province

Patentee after: Jiangsu Tianyi Aviation Industry Co.,Ltd.

Address before: 224001 No.2 Hangkong Road, high tech Industrial Zone, Jianhu County, Yancheng City, Jiangsu Province

Patentee before: JIANGSU TIANYI AIRPORT SPECIAL EQUIPMENT Co.,Ltd.

CP01 Change in the name or title of a patent holder
EE01 Entry into force of recordation of patent licensing contract

Assignee: Jiangsu Tianyi Airport Equipment Maintenance Service Co.,Ltd.

Assignor: Jiangsu Tianyi Aviation Industry Co.,Ltd.

Contract record no.: X2023980044219

Denomination of utility model: A lifting mechanism with large arm profile structure

Granted publication date: 20211116

License type: Common License

Record date: 20231024

EE01 Entry into force of recordation of patent licensing contract