CN209532784U - A kind of milling tool suitable for airplane parts - Google Patents
A kind of milling tool suitable for airplane parts Download PDFInfo
- Publication number
- CN209532784U CN209532784U CN201920168739.1U CN201920168739U CN209532784U CN 209532784 U CN209532784 U CN 209532784U CN 201920168739 U CN201920168739 U CN 201920168739U CN 209532784 U CN209532784 U CN 209532784U
- Authority
- CN
- China
- Prior art keywords
- tooling ontology
- airplane parts
- milling tool
- tooling
- processing plate
- 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
Links
Landscapes
- Toys (AREA)
Abstract
The utility model provides a kind of milling tool suitable for airplane parts, it is able to use special tooling and carries out Set and Positioning, it is bonded part type face tightly with tooling upper surface, it is easy to process, guarantee that product qualification rate is high, the milling tool includes tooling ontology, the section of tooling ontology is I-shaped, the top surface of tooling ontology is provided with mounting hole, mounting hole is arranged on the quadrangle of tooling ontology, the top surface of tooling ontology is additionally provided with processing plate, the quadrangle of processing plate is connect by mounting hole with tooling ontology, the shape for processing plate is complementary with the stationary plane of airplane parts, it is evacuation region that the top at the top and tooling ontology that process plate, which has the part of distance, evacuation is provided with multiple threaded holes on region.
Description
Technical field
The utility model relates to part manufacture fields, in particular to a kind of milling work suitable for airplane parts
Dress.
Background technique
In the prior art, the shape of many aircrafts part is not a plane, is all much that curved surface is either recessed
Type face made of the plane combination of convex injustice, parts fixation location difficulty, product qualification rate is low, and processing efficiency is low.
Utility model content
The purpose of this utility model is to provide a kind of milling tools suitable for airplane parts, are able to use dedicated
Tooling carries out Set and Positioning, is bonded part type face tightly with tooling upper surface, easy to process, guarantees that product qualification rate is high.
The embodiments of the present invention are achieved in that
A kind of milling tool suitable for airplane parts, the milling tool include tooling ontology, the section of tooling ontology
For I-shaped, the top surface of tooling ontology is provided with mounting hole, and mounting hole is arranged on the quadrangle of tooling ontology, tooling ontology
Top surface is additionally provided with processing plate, and the quadrangle for processing plate is connect by mounting hole with tooling ontology, processes the shape and aircraft zero of plate
The stationary plane of part is complementary, and the top at the top and tooling ontology that process plate has the part of distance for evacuation region, avoids region
On be provided with multiple threaded holes.
In the preferred embodiment of the utility model, above-mentioned mounting hole includes dowel hole and hold-down apertures, 1 dowel hole
It is one group with 1 hold-down apertures to be respectively distributed on the quadrangle of tooling ontology.
In the preferred embodiment of the utility model, the bottom of above-mentioned tooling ontology is provided with fixation hole, and fixing piece passes through
Fixation hole is connect with machining tool.
In the preferred embodiment of the utility model, the side of above-mentioned tooling ontology is provided with 1 or multiple holes for hoist.
In the preferred embodiment of the utility model, escape groove is provided in the middle part of above-mentioned processing plate.
In the preferred embodiment of the utility model, above-mentioned evacuation region is bonded with the stationary plane of airplane parts.
The beneficial effect of the utility model embodiment is: milling tool in the present embodiment is I-shaped, and top surface is used
It is connected in airplane parts, bottom surface with machining tool due to connecting, and top surface is provided with mounting hole, and mounting hole is for connecting processing
The stationary plane of plate, the shape and airplane parts of processing plate is complementary, so that the stationary plane of milling tool top surface and airplane parts is bonded,
It is provided with threaded hole on evacuation region to be used to reinforce airplane parts, airplane parts is prevented to be subjected to displacement in process, thus
Airplane parts are fixed positioned on milling tool well.
Detailed description of the invention
It, below will be to use required in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
Attached drawing be briefly described, it should be understood that the following drawings illustrates only some embodiments of the utility model, therefore should not be by
Regard the restriction to range as, for those of ordinary skill in the art, without creative efforts, may be used also
To obtain other relevant attached drawings according to these attached drawings.
Fig. 1 is the milling tool positive structure diagram of the utility model embodiment；
Fig. 2 is the overlooking structure diagram of the utility model embodiment milling tool.
Icon: 100- tooling ontology；200- processes plate；110- avoids region；111- threaded hole；210- dowel hole；
220- hold-down apertures；130- fixation hole；140- hole for hoist；150- pressing plate groove；230- escape groove.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Usually here in attached drawing description and
The component of the utility model embodiment shown can be arranged and be designed with a variety of different configurations.
Therefore, requirement is not intended to limit to the detailed description of the embodiments of the present invention provided in the accompanying drawings below
The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model
Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all
Belong to the range of the utility model protection.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
It is in the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, or
The utility model product using when the orientation or positional relationship usually put, be merely for convenience of description the utility model and letter
Change description, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific orientation construct and
Operation, therefore should not be understood as limiting the present invention.In addition, term " first ", " second ", " third " etc. are only used for area
Divide description, is not understood to indicate or imply relative importance.
In addition, the terms such as term "horizontal", "vertical", " pendency " are not offered as requiring component abswolute level or pendency, and
It is that can be slightly tilted.It is not to indicate the structure if "horizontal" only refers to that its direction is more horizontal with respect to for "vertical"
It has to fully horizontally, but can be slightly tilted.
In the description of the present invention, it should also be noted that, unless otherwise clearly defined and limited, term " is set
Set ", " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or it is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, intermediary can also be passed through
It is indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
First embodiment
Referring to Figure 1-2, the present embodiment provides a kind of milling tool suitable for airplane parts, which includes
The section of tooling ontology 100, tooling ontology 100 is I-shaped, and the top surface of tooling ontology 100 is provided with mounting hole, mounting hole
It is arranged on the quadrangle of tooling ontology 100, the top surface of tooling ontology 100 is additionally provided with processing plate 200, processes the quadrangle of plate 200
It is connect by mounting hole with tooling ontology 100, the shape for processing plate 200 is complementary with the stationary plane of airplane parts, processing plate 200
It is evacuation region 110 that top and the top of tooling ontology 100, which have the part of distance, avoids and is provided with multiple spiral shells on region 110
Pit 111.
Milling tool in the present embodiment is I-shaped, top surface for being connected with airplane parts, bottom surface due to add
The connection of work lathe, top surface are provided with mounting hole, and mounting hole processes the shape and airplane parts of plate 200 for connecting processing plate 200
Stationary plane it is complementary so that the stationary plane of milling tool top surface and airplane parts is bonded, avoids and be provided with threaded hole on region 110
111, for reinforcing airplane parts, prevent airplane parts to be subjected to displacement in process, so that airplane parts are fixed fixed well
Position is on milling tool.
More specifically, the mounting hole in the present embodiment includes 220,1 dowel hole of dowel hole 210 and hold-down apertures
210 and 1 hold-down apertures 220 are one group and are respectively distributed on the quadrangle of tooling ontology 100.Dowel hole 210 is for processing plate 200
Positioning, the connection that hold-down apertures 220 are used to reinforce processing plate 200 prevent from processing 200 alice of plate, aircraft zero of grinding away
Part.
More specifically, the bottom of the tooling ontology 100 in the present embodiment is provided with fixation hole 130, and fixing piece passes through solid
Determine hole 130 to connect with machining tool, fixation hole 130 with machining tool for connecting.The side of tooling ontology 100 in the present embodiment
Middle face is pressing plate groove 150, and tooling ontology 100 is reinforced by pressing plate.
More specifically, the side of the tooling ontology 100 in the present embodiment is provided with 1 or multiple holes for hoist 140, hangs
Hole 140 is filled for installation or disassembling fixture.
More specifically, the middle part of the processing plate 200 in the present embodiment is provided with escape groove 230, keeping away in the present embodiment
It allows slot 230 to be 1 rectangle, can be set to escape groove 230 of different shapes on processing plate 200 in other embodiments, use
It is bonded in the stationary plane for guaranteeing airplane parts with processing plate 200.It may be set to be multiple rectangles in other embodiments, as long as
It is that the stationary plane of airplane parts and the state of the processing fitting of plate 200 belong to same technical concept.Evacuation in the present embodiment
Region 110 is also bonded with the stationary plane of airplane parts.
In conclusion milling tool in the present embodiment is I-shaped, top surface with airplane parts for connecting, bottom surface
Due to connecting with machining tool, top surface is provided with mounting hole, mounting hole for connecting processing plate 200, process plate 200 shape and
The stationary plane of airplane parts is complementary, so that the stationary plane of milling tool top surface and airplane parts is bonded, avoids and is arranged on region 110
There is threaded hole 111 for reinforcing airplane parts, prevents airplane parts to be subjected to displacement in process, so that airplane parts are fine
Be fixed positioned on milling tool.
Present specification describes the example of the embodiments of the present invention, it is not meant to that these embodiments illustrate and describe
All possible forms of the utility model.It should be understood that the embodiment in specification can be implemented with a variety of alternative forms.Attached drawing without
It needs drawn to scale；Some features can be zoomed in or out to show the details of particular elements.Disclosed specific structure and function are thin
Section is not taken by way of limitation explanation, and those skilled in the art is only instructed to implement the representative base of the utility model in a variety of forms
Plinth.It will be understood to one skilled in the art that can be with one or more with reference to multiple features that either figure illustrates and describes
The feature combination illustrated in other attached drawings is to form the embodiment for not yet explicitly illustrating or describing.The assemblage characteristic offer of explanation is used for
The representative embodiment of typical case.However, can root with the multiple combinations of the consistent feature of introduction of the utility model and modification
According to needing for specific application or implementation.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (6)
1. a kind of milling tool suitable for airplane parts, which is characterized in that the milling tool includes tooling ontology, described
The section of tooling ontology is I-shaped, and the top surface of the tooling ontology is provided with mounting hole, and the mounting hole is arranged described
On the quadrangle of tooling ontology, the top surface of the tooling ontology is additionally provided with processing plate, and the quadrangle of the processing plate passes through the peace
Dress hole is connect with the tooling ontology, and the shape of the processing plate is complementary with the stationary plane of airplane parts, the top of the processing plate
It is evacuation region that portion and the top of the tooling ontology, which have the part of distance, is provided with multiple screw threads on the evacuation region
Hole.
2. the milling tool according to claim 1 suitable for airplane parts, which is characterized in that the mounting hole includes
Dowel hole and hold-down apertures, 1 dowel hole and 1 hold-down apertures are one group and are respectively distributed to the tooling ontology
On quadrangle.
3. the milling tool according to claim 1 suitable for airplane parts, which is characterized in that the tooling ontology
Bottom is provided with fixation hole, and fixing piece passes through the fixation hole and connect with machining tool.
4. the milling tool according to claim 1 suitable for airplane parts, which is characterized in that the tooling ontology
Side is provided with 1 or multiple holes for hoist.
5. the milling tool according to claim 1 suitable for airplane parts, which is characterized in that in the processing plate
Portion is provided with escape groove.
6. the milling tool according to claim 1 suitable for airplane parts, which is characterized in that the evacuation region with
The stationary plane of the airplane parts is bonded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920168739.1U CN209532784U (en) | 2019-01-31 | 2019-01-31 | A kind of milling tool suitable for airplane parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920168739.1U CN209532784U (en) | 2019-01-31 | 2019-01-31 | A kind of milling tool suitable for airplane parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209532784U true CN209532784U (en) | 2019-10-25 |
Family
ID=68272558
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920168739.1U Active CN209532784U (en) | 2019-01-31 | 2019-01-31 | A kind of milling tool suitable for airplane parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209532784U (en) |
-
2019
- 2019-01-31 CN CN201920168739.1U patent/CN209532784U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209532784U (en) | A kind of milling tool suitable for airplane parts | |
| CN109434106A (en) | A kind of increasing material support construction | |
| CN209255837U (en) | A kind of increasing material support construction | |
| CN209288813U (en) | It is a kind of for installing the fixture of pump body module | |
| CN209532783U (en) | A kind of contour localization tooling suitable for airplane parts | |
| CN209394229U (en) | A kind of guard ring welding tooling suitable for beam pumping unit | |
| CN209532723U (en) | A kind of expanded type assembled tool suitable for screw blade | |
| CN209532782U (en) | A kind of processing tool suitable for universal hole system | |
| CN209439257U (en) | A kind of guard ring bending fixture suitable for beam pumping unit | |
| CN213685847U (en) | Levelness adjusting device | |
| CN208929710U (en) | A kind of workbench for airplane parts | |
| CN204167457U (en) | The microwave-medium resonance device of radio-frequency module | |
| CN208131775U (en) | A kind of mold fast-positioning device | |
| CN209088676U (en) | A kind of attachment device of servo motor and motor cabinet | |
| CN208262290U (en) | Modified processing center machine tool pedestal | |
| CN111805910A (en) | Cutting die for 3D printer | |
| CN107498610B (en) | Circular blade and cutting tool with accurate positioning structure | |
| CN209532201U (en) | A kind of expanded type Universal Jig tooling | |
| CN220243545U (en) | Composite bracket for fixing landing gear and test bench | |
| CN211363907U (en) | Jig for glass printing | |
| CN205393903U (en) | Water platform frame with adjustable a height for welding tool set -up mould | |
| CN208429228U (en) | A kind of unmanned plane connection structure and unmanned plane | |
| CN107841783A (en) | A kind of upper plated film support plate | |
| CN209303835U (en) | A kind of chamfer machining auxiliary device | |
| CN208467748U (en) | Cavity body structure workbench |
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: 611330 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee after: Chengdu chaohepur Aviation Technology Co.,Ltd. Address before: 611330 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee before: CHENGDU JIAODA PUER INDUSTRIAL Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 611330 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee after: Chengdu Chaohepu Aviation Technology Co.,Ltd. Address before: 611330 No. 18, Ganxi Road, Industrial Development Zone, Jinyuan Town, Dayi County, Chengdu, Sichuan Patentee before: Chengdu chaohepur Aviation Technology Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder |