CN219854174U - Clamping and positioning tool for detecting leg support of aviation seat - Google Patents
Clamping and positioning tool for detecting leg support of aviation seat Download PDFInfo
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- CN219854174U CN219854174U CN202321118772.6U CN202321118772U CN219854174U CN 219854174 U CN219854174 U CN 219854174U CN 202321118772 U CN202321118772 U CN 202321118772U CN 219854174 U CN219854174 U CN 219854174U
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- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 230000000712 assembly Effects 0.000 claims description 3
- 238000000429 assembly Methods 0.000 claims description 3
- 238000001514 detection method Methods 0.000 abstract description 6
- 238000009434 installation Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model relates to the technical field of clamp equipment, in particular to a clamping and positioning tool for detecting an aviation seat leg support, which comprises a base, wherein a first vertical positioning column matched with a first vertical hinge hole, a second vertical positioning column matched with a second vertical hinge hole, a first horizontal positioning component matched with a first horizontal positioning groove, a second horizontal positioning component matched with a second horizontal positioning groove, a third horizontal positioning component matched with a third horizontal positioning groove, a fourth horizontal positioning component matched with a fourth horizontal positioning groove, vertical positioning support blocks matched with each vertical positioning hole and a plurality of pressing components for pressing aviation seat leg support workpieces from above are arranged on the base. The utility model has reasonable structural design, and the components are cooperatively matched, so that the workpiece of the leg support of the aero seat can be effectively clamped and positioned, and the subsequent detection operation of the detection tool is facilitated.
Description
Technical Field
The utility model relates to the technical field of clamp equipment, in particular to a clamping and positioning tool for detecting an aviation seat leg support.
Background
The aviation seat leg support is provided with a plurality of fixed positions, and if one of the fixed positions deviates, the component cannot be installed and used, so that a corresponding gauge is designed according to the characteristic to ensure the installation accuracy. Before the gauge detects, the gauge needs to be clamped and positioned effectively by using a clamping and positioning tool.
The conventional clamping and positioning tool has the defects in the using process that the conventional clamping and positioning tool cannot provide effective clamping and positioning for the leg support of the aero seat as shown in fig. 3-4, and is inconvenient for the subsequent detection operation of the detection tool. Therefore, there is a need for an improved and optimized conventional clamping and positioning tool.
Disclosure of Invention
The utility model aims to solve the problems in the prior art and provides a clamping and positioning tool for detecting an aviation seat leg support.
In order to achieve the technical purpose and the technical effect, the utility model is realized by the following technical scheme:
the utility model provides an aviation seat leg support detects with centre gripping location frock, this centre gripping location frock is used for carrying out centre gripping location to aviation seat leg support work piece, aviation seat leg support work piece includes first frame, second frame, first link and second link bear, first frame has set gradually first vertical hinge hole, first horizontal constant head tank, first vertical constant head tank, second horizontal constant head tank and second vertical constant head tank from the front to the back, second frame has set gradually second vertical hinge hole, fourth horizontal constant head tank, third vertical constant head tank and fourth vertical constant head tank from the front to the back, first frame is close to first horizontal constant head tank and second frame is connected with first link near between second horizontal constant head tank, be connected with the second link between the other end of first frame and second frame, second link is located near first frame and has seted up third horizontal constant head tank, second frame is located near second link and is equipped with the hinge lug of taking the fifth locating hole;
the clamping and positioning tool comprises a base, wherein a first vertical positioning column matched with a first vertical hinge hole, a second vertical positioning column matched with a second vertical hinge hole, a first horizontal positioning assembly matched with a first horizontal positioning groove, a second horizontal positioning assembly matched with a second horizontal positioning groove, a third horizontal positioning assembly matched with a third horizontal positioning groove, a fourth horizontal positioning assembly matched with a fourth horizontal positioning groove, vertical positioning supporting blocks matched with each vertical positioning hole and a plurality of pressing assemblies used for pressing the leg support workpiece of the aero seat from the upper side are arranged on the base.
Further, in the clamping and positioning tool for detecting the leg support of the aero seat, the first bearing frame is a straight line frame, and the second bearing frame is an arc frame.
Furthermore, in the clamping and positioning tool for detecting the leg support of the aero seat, all parts in the workpiece of the leg support of the aero seat are of an integrated structure and are made of aluminum alloy materials.
Further, in the clamping and positioning tool for detecting the leg support of the aero seat, each horizontal positioning assembly is composed of a mounting block and a positioning push rod, the mounting block is fixed on the base, the positioning push rod is fixed on the mounting block, and the movable end of the positioning push rod is matched with the corresponding horizontal positioning groove in shape.
Further, in the clamping and positioning tool for detecting the leg support of the aero seat, the positioning push rod is a pneumatic push rod, an electric push rod or a hydraulic push rod.
Furthermore, in the clamping and positioning tool for detecting the leg support of the aero seat, the pressing component is a pneumatic rapid pressing clamp, an electric rapid pressing clamp or a hydraulic rapid pressing clamp.
The beneficial effects of the utility model are as follows:
the utility model has reasonable structural design, and mainly comprises a base, a first vertical positioning column, a second vertical positioning column, a first horizontal positioning assembly, a second horizontal positioning assembly, a third horizontal positioning assembly, a fourth horizontal positioning assembly, a plurality of vertical positioning supporting blocks and a plurality of pressing assemblies, wherein all the components are matched in a cooperative manner, so that an aviation seat leg support workpiece can be effectively clamped and positioned, and the inspection tool is convenient to carry out subsequent detection operation.
Of course, it is not necessary for any one product to practice the utility model to achieve all of the advantages set forth above at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic perspective view of the present utility model in use;
FIG. 2 is a schematic top view of the present utility model in use;
FIG. 3 is a schematic perspective view of an aircraft seat leg rest workpiece in accordance with the present utility model;
FIG. 4 is a schematic top view of an aircraft seat leg rest workpiece in accordance with the present utility model;
FIG. 5 is a schematic perspective view of a clamping and positioning tool according to the present utility model;
FIG. 6 is a schematic top view of a clamping and positioning tool according to the present utility model;
in the drawings, the list of components represented by the various numbers is as follows:
1-aviation seat leg support work piece, 101-first bearing frame, 102-second bearing frame, 103-first connecting frame, 104-second connecting frame, 105-first vertical hinge hole, 106-first horizontal positioning groove, 107-first vertical positioning hole, 108-second horizontal positioning groove, 109-second vertical positioning hole, 110-third horizontal positioning groove, 111-second vertical hinge hole, 112-fourth horizontal positioning groove, 113-third vertical positioning hole, 114-fourth vertical positioning hole, 115-hinged ear plate, 116-fifth vertical positioning hole, 2-base, 3-first vertical positioning column, 4-second vertical positioning column, 5-first horizontal positioning component, 6-second horizontal positioning component, 7-third horizontal positioning component, 8-fourth horizontal positioning component, 9-pressing component, 10-vertical positioning support block.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-6, the present embodiment is a clamping and positioning tool for detecting an aero-seat leg support, which is used for clamping and positioning an aero-seat leg support workpiece 1. The aviation seat leg support workpiece 1 comprises a first bearing frame 101, a second bearing frame 102, a first connecting frame 103 and a second connecting frame 104, wherein the first bearing frame 101 is sequentially provided with a first vertical hinge hole 105, a first horizontal positioning groove 106, a first vertical positioning hole 107, a second horizontal positioning groove 108 and a second vertical positioning hole 109 from front to back, and the second bearing frame 102 is sequentially provided with a second vertical hinge hole 111, a fourth horizontal positioning groove 112, a third vertical positioning hole 113 and a fourth vertical positioning hole 114 from front to back. A first connecting frame 103 is connected between the position of the first bearing frame 101 close to the first horizontal positioning groove 106 and the position of the second bearing frame 102 close to the second horizontal positioning groove 112, and a second connecting frame 104 is connected between the other ends of the first bearing frame 101 and the second bearing frame 102. The second connecting frame 104 is provided with a third horizontal positioning groove 110 near the first bearing frame 101, and the second bearing frame 102 is provided with a hinged lug plate 115 with a fifth vertical positioning hole 116 near the second connecting frame 104.
In this embodiment, the clamping and positioning fixture comprises a base 2, wherein a first vertical positioning column 3 matched with a first vertical hinge hole 105, a second vertical positioning column 4 matched with a second vertical hinge hole 111, a first horizontal positioning component 5 matched with a first horizontal positioning groove 106, a second horizontal positioning component 6 matched with a second horizontal positioning groove 108, a third horizontal positioning component 7 matched with a third horizontal positioning groove 110, a fourth horizontal positioning component 8 matched with a fourth horizontal positioning groove 112, vertical positioning supporting blocks 10 matched with each vertical positioning hole and a plurality of pressing components 9 used for pressing the leg support workpiece of the aero seat from above are installed on the base 2.
In this embodiment, the first carrier 101 is a straight line frame, and the second carrier 102 is an arc frame. The components in the aviation seat leg support workpiece 1 are of an integrated structure and are made of aluminum alloy materials.
In this embodiment, every horizontal positioning component comprises installation piece and location push rod, and the installation piece is fixed on the base, and the location push rod is fixed on the installation piece, and the expansion end of location push rod and the horizontal constant head tank shape that corresponds mutually support. The positioning push rod is a pneumatic push rod, an electric push rod or a hydraulic push rod.
In this embodiment, the pressing component 9 is a pneumatic quick press, an electric quick press, or a hydraulic quick press.
One specific application of this embodiment is: this aviation seat leg support detects with centre gripping location frock mainly comprises base 2, first vertical reference column 3, the vertical reference column 4 of second, first horizontal locating component 5, second horizontal locating component 6, third horizontal locating component 7, fourth horizontal locating component 8, a plurality of vertical location supporting shoe 10 and a plurality of pressure subassembly 9 that support, and each part cooperates, can carry out effectual centre gripping location to aviation seat leg support work piece 1, and the gauge of being convenient for carries out subsequent detection operation.
The preferred embodiments of the utility model disclosed above are intended only to assist in the explanation of the utility model. The preferred embodiments are not exhaustive or to limit the utility model to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best understand and utilize the utility model. The utility model is limited only by the claims and the full scope and equivalents thereof.
Claims (6)
1. The clamping and positioning tool for detecting the leg support of the aero seat is characterized in that the clamping and positioning tool is used for clamping and positioning the leg support workpiece of the aero seat, the leg support workpiece of the aero seat comprises a first bearing frame, a second bearing frame, a first connecting frame and a second connecting frame, the first bearing frame is sequentially provided with a first vertical hinge hole, a first horizontal positioning groove, a first vertical positioning hole, a second horizontal positioning groove and a second vertical positioning hole from front to back, the second bearing frame is sequentially provided with a second vertical hinge hole, a fourth horizontal positioning groove, a third vertical positioning hole and a fourth vertical positioning hole from front to back, a first connecting frame is connected between the position of the first bearing frame close to the first horizontal positioning groove and the position of the second bearing frame close to the second horizontal positioning groove, a second connecting frame is connected between the other ends of the first bearing frame and the second bearing frame, the second connecting frame is positioned close to the first bearing frame and is provided with a third horizontal positioning groove, and the second bearing frame is positioned close to the second connecting frame and is provided with a fifth hinge lug hole;
the clamping and positioning tool comprises a base, wherein a first vertical positioning column matched with a first vertical hinge hole, a second vertical positioning column matched with a second vertical hinge hole, a first horizontal positioning assembly matched with a first horizontal positioning groove, a second horizontal positioning assembly matched with a second horizontal positioning groove, a third horizontal positioning assembly matched with a third horizontal positioning groove, a fourth horizontal positioning assembly matched with a fourth horizontal positioning groove, vertical positioning supporting blocks matched with each vertical positioning hole and a plurality of pressing assemblies used for pressing the leg support workpiece of the aero seat from the upper side are arranged on the base.
2. The clamping and positioning tool for detecting an air seat leg support according to claim 1, wherein: the first bearing frame is a straight line frame, and the second bearing frame is an arc-shaped frame.
3. The clamping and positioning tool for detecting an air seat leg support according to claim 1, wherein: all parts in the aviation seat leg support workpiece are of an integrated structure and are made of aluminum alloy materials.
4. The clamping and positioning tool for detecting an air seat leg support according to claim 1, wherein: each horizontal positioning assembly consists of a mounting block and a positioning push rod, the mounting block is fixed on the base, the positioning push rod is fixed on the mounting block, and the movable end of the positioning push rod is matched with the corresponding horizontal positioning groove in shape.
5. The clamping and positioning tool for detecting the leg rest of the aerochair according to claim 4, wherein the clamping and positioning tool is characterized in that: the positioning push rod is a pneumatic push rod, an electric push rod or a hydraulic push rod.
6. The clamping and positioning tool for detecting an air seat leg support according to claim 1, wherein: the pressing component is a pneumatic quick pressing clamp, an electric quick pressing clamp or a hydraulic quick pressing clamp.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321118772.6U CN219854174U (en) | 2023-05-11 | 2023-05-11 | Clamping and positioning tool for detecting leg support of aviation seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321118772.6U CN219854174U (en) | 2023-05-11 | 2023-05-11 | Clamping and positioning tool for detecting leg support of aviation seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219854174U true CN219854174U (en) | 2023-10-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321118772.6U Active CN219854174U (en) | 2023-05-11 | 2023-05-11 | Clamping and positioning tool for detecting leg support of aviation seat |
Country Status (1)
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| CN (1) | CN219854174U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117139847A (en) * | 2023-10-31 | 2023-12-01 | 常州市蓝托金属制品有限公司 | Intelligent welding device and method for production and processing of aviation seat armrests |
| CN117226308A (en) * | 2023-11-15 | 2023-12-15 | 常州市蓝托金属制品有限公司 | Clamping and positioning tool and method for processing seat armrest support |
| CN118090405A (en) * | 2024-04-28 | 2024-05-28 | 常州市蓝托金属制品有限公司 | Bearing capacity detection device and method for airplane seat dining table board |
-
2023
- 2023-05-11 CN CN202321118772.6U patent/CN219854174U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117139847A (en) * | 2023-10-31 | 2023-12-01 | 常州市蓝托金属制品有限公司 | Intelligent welding device and method for production and processing of aviation seat armrests |
| CN117139847B (en) * | 2023-10-31 | 2024-01-26 | 常州市蓝托金属制品有限公司 | Intelligent welding device and method for production and processing of aviation seat armrests |
| CN117226308A (en) * | 2023-11-15 | 2023-12-15 | 常州市蓝托金属制品有限公司 | Clamping and positioning tool and method for processing seat armrest support |
| CN117226308B (en) * | 2023-11-15 | 2024-03-01 | 常州市蓝托金属制品有限公司 | Clamping and positioning tool and method for processing seat armrest support |
| CN118090405A (en) * | 2024-04-28 | 2024-05-28 | 常州市蓝托金属制品有限公司 | Bearing capacity detection device and method for airplane seat dining table board |
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