CN110238975A - The nonmetallic drilling equipment of aircraft door glass and method - Google Patents
The nonmetallic drilling equipment of aircraft door glass and method Download PDFInfo
- Publication number
- CN110238975A CN110238975A CN201910584642.3A CN201910584642A CN110238975A CN 110238975 A CN110238975 A CN 110238975A CN 201910584642 A CN201910584642 A CN 201910584642A CN 110238975 A CN110238975 A CN 110238975A
- Authority
- CN
- China
- Prior art keywords
- model drilling
- die body
- door glass
- aircraft door
- body seat
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28D—WORKING STONE OR STONE-LIKE MATERIALS
- B28D1/00—Working stone or stone-like materials, e.g. brick, concrete or glass, not provided for elsewhere; Machines, devices, tools therefor
- B28D1/14—Working stone or stone-like materials, e.g. brick, concrete or glass, not provided for elsewhere; Machines, devices, tools therefor by boring or drilling
- B28D1/146—Tools therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28D—WORKING STONE OR STONE-LIKE MATERIALS
- B28D7/00—Accessories specially adapted for use with machines or devices of the preceding groups
- B28D7/04—Accessories specially adapted for use with machines or devices of the preceding groups for supporting or holding work or conveying or discharging work
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mining & Mineral Resources (AREA)
- Re-Forming, After-Treatment, Cutting And Transporting Of Glass Products (AREA)
Abstract
The invention proposes a kind of nonmetallic drilling equipment of aircraft door glass and methods.The device includes: die body seat, model drilling body, glue note bushing, drill bushing, fastening screw, technique bolt, compactor and press strip, in which: is arranged on die body seat fluted；Groove is for placing aircraft door glass and press strip；Model drilling body is used to for aircraft door glass being clipped in the middle with press strip with die body seat；Multiple fast compactors are disposed within one week around model drilling body on die body seat；Compactor is used to compress die body seat and model drilling body；Glue note bushing is installed on die body seat；The rivet hole location produced in model drilling body is turned over based on technique bolt is provided with drill bushing.The features such as present invention uses nonmetallic materials, light-weight, and difficulty of processing is small, and manufacturing cost is low.
Description
Technical field
The present invention relates to aviation field mechanical manufacturing technology more particularly to a kind of nonmetallic drilling equipments of aircraft door glass
And method.
Background technique
Aircraft door glass generally has the shape of curved surface, and difficulty is larger when drilling rivet hole to such hatch door glass.It is logical
It often, is all the aluminum or steel drill jig using particularly customized banding pattern face to the aircraft door glass of different curve shape.
Applicant it has been investigated that: when aircraft door glass volume is larger, curved surface curvature is larger, and Curvature varying is variable
When, the drill jig for needing to use just needs to consider more factors, such as the factors such as rigidity, machinability, volume weight of drill jig.
If there are drill jig difficulty of processing is big, processing less economical, weight causes greatly operability poor using aluminum or steel drill jig
The disadvantages of.
Summary of the invention
The purpose of the present invention is: propose a kind of nonmetallic drilling equipment of aircraft door glass and method, it is existing to solve
Aircraft door glass drill jig difficulty of processing is big, and processing is less economical, and weight leads to problems such as greatly operability poor.
In a first aspect, the invention proposes a kind of nonmetallic drilling equipments of aircraft door glass.The device includes:
Die body seat 1, model drilling body 2, glue note bushing 3, drill bushing 4, fastening screw 5, technique bolt 6, compactor 7 and press strip 9,
In:
It is arranged on die body seat 1 fluted；
Groove is for placing aircraft door glass and press strip 9；
Model drilling body 2 is used to for aircraft door glass and press strip 9 being clipped in the middle with die body seat 1；
Multiple fast compactors 7 are disposed within 2 one weeks around model drilling body on die body seat 1；
Compactor 7 is for compressing die body seat 1 and model drilling body 2；
Glue note bushing 3 is installed on die body seat 1；
The rivet hole location produced in model drilling body 2 is turned over based on technique bolt 6 is provided with drill bushing 4；
Die body seat 1 and model drilling body 2 are nonmetallic materials.
Second aspect, the invention proposes a kind of nonmetallic boring methods of aircraft door glass.This method includes following step
It is rapid:
The glass reinforced plastic working surface and rivet hole location on die body seat 1 are processed by numerically-controlled machine tool；
Model drilling body 2 processed is turned over, is padded on die body seat 1 by the thickness value of aircraft door glass and press strip 9 and adds certain thickness value
Padding turns over the type face for producing model drilling body 2 along rivet bore region with glass-reinforced plastic material, then borrows technique bolt 6 and turn over and produce drill jig
Rivet hole location on body 2 simultaneously inlays drill bushing 4；
Remove padding after turning over finishing drilling die body 2 processed；
Glue note bushing 3 is installed on die body seat 1, is fixed by clay 8, at the hole location of glue note bushing 3, positioning is borrowed and inserts
Pin 5 turns over the location hole for producing the model drilling body 2 of same belt transect glue note bushing 3.
The embodiment of the present invention can use nonmetallic materials, have light-weight, and difficulty of processing is small, the low equal spies of manufacturing cost
Point.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, will make below to required in the embodiment of the present invention
Attached drawing is briefly described, it is therefore apparent that drawings described below is only some embodiments of the present invention, for this
For the technical staff in field, without creative efforts, it can also be obtained according to these attached drawings other attached
Figure.
Fig. 1 is the structural schematic diagram of the nonmetallic drilling equipment of aircraft door glass of one embodiment of the invention；
Fig. 2 is the perspective view of the explosion of Fig. 1 of one embodiment of the invention；
Fig. 3 is the cross-sectional view of the first angle of Fig. 1 of one embodiment of the invention；
Fig. 4 is the cross-sectional view of the second angle of Fig. 1 of one embodiment of the invention.
Wherein: die body seat 1, model drilling body 2, glue note bushing 3, drill bushing 4, fastening screw 5, technique bolt 6 and fast compactor
7。
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.Obviously, described embodiment is
A part of the embodiment of the present invention, rather than whole embodiments.Based on the embodiments of the present invention, those skilled in the art
Without making creative work, every other embodiment obtained, shall fall within the protection scope of the present invention.
The feature and illustrative examples of various aspects of the invention is described more fully below.In following detailed description
In, many details are proposed, in order to provide complete understanding of the present invention.But come for those skilled in the art
It says it will be apparent that the present invention can be implemented in the case where not needing some details in these details.Below to reality
The description of example is applied just for the sake of providing and better understanding to of the invention by showing example of the invention.The present invention is never
It is limited to any specific setting and method set forth below, but covering finishes under the premise of without departing from the spirit of the present invention
Structure, method, any improvement of device, substitutions and modifications.In the the accompanying drawings and the following description, well known structure and skill is not shown
Art is unnecessary fuzzy to avoid causing to the present invention.
It should be noted that in the absence of conflict, the feature in the embodiment of the present invention and embodiment can be tied mutually
It closes, each embodiment mutually can be referred to and be quoted.The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 is the structural schematic diagram of the nonmetallic drilling equipment of aircraft door glass of one embodiment of the invention；Fig. 2 is this hair
The perspective view of the explosion of Fig. 1 of a bright embodiment.
Fig. 1, Fig. 2 are please referred to, most beneath is die body seat 1, and the aircraft door glass and press strip 9 for needing to drill rivet hole are placed
In on die body 1, the top is model drilling body 2, and aircraft door glass and press strip 9 are clipped in the middle by model drilling body 2 with die body seat 1, in mould
Fast compactor 7 is arranged within 2 one weeks for compressing model drilling body 2 around model drilling body in housing 1.
In some embodiments, the nonmetallic drilling equipment of aircraft door glass may include: die body seat 1, model drilling body 2, glue
Infuse bushing 3, drill bushing 4, fastening screw 5, technique bolt 6, compactor 7 and press strip 9.Wherein: being arranged on die body seat 1 fluted；It is recessed
Slot is for placing aircraft door glass and press strip 9；During model drilling body 2 and die body seat 1 are used to for aircraft door glass and press strip 9 being clipped in
Between；Multiple fast compactors 7 are disposed within 2 one weeks around model drilling body on die body seat 1；Compactor 7 is used for die body seat 1 and drill jig
Body 2 compresses；Glue note bushing 3 is installed on die body seat 1；The rivet hole location produced in model drilling body 2 is turned over based on technique bolt 6
It is provided with drill bushing 4；Die body seat 1 and model drilling body 2 are nonmetallic materials.
In some embodiments, the type face of model drilling body 2 is to turn over the type face produced with glass-reinforced plastic material along rivet bore region.
The type face can be irregular type face, for example, curved surface.
In some embodiments, the bulk of model drilling body 2 is within the scope of 900mm × 500mm × 100mm.
In some embodiments, 2 thickness value of model drilling body is more than or equal to 10mm and is less than or equal to 15mm.Preferably, model drilling body 2
Thickness value is 12mm.
In some embodiments, 2 width value of model drilling body is more than or equal to 25mm and is less than or equal to 35mm.Preferably, model drilling body 2
Thickness value is 30mm.
Applicant it has been investigated that the three-dimensional size of model drilling body 2 have to the drill jig in later period and drilling it is very big
Influence, for example, thickness is too thick not only to will increase weight, cause processing difficulties, can also strengthen rigidity, reduce elasticity, increase and clamp
The difficulty of aircraft door glass operation is also easy to damage glass.
Fig. 3 is the cross-sectional view of the first angle of Fig. 1 of one embodiment of the invention；Fig. 4 is Fig. 1 of one embodiment of the invention
The cross-sectional view of second angle.
Drill jig manufacturing process can be as follows:
S1: the glass reinforced plastic working surface and rivet hole location on die body seat 1 are processed by numerically-controlled machine tool.
S2: turning over model drilling body 2 processed, refering to the A-A cross-sectional view of Fig. 3, by the thickness value of aircraft door glass and press strip 9 in die body
Pad plus the padding of certain thickness value, the type face for producing model drilling body 2 is turned over along rivet bore region with glass-reinforced plastic material on seat 1, to protect
Card model drilling body 2 has enough rigidity and considers light weight requirements, and thickness value is about 12mm, width about 30mm, then again
Technique bolt 6 is borrowed to turn over the rivet hole location produced in model drilling body 2 and inlay drill bushing 4.
Remove padding after turning over finishing drilling die body 2 processed, 2 weight of 900mm × 500mm × 100mm model drilling body less than 4 jin,
It is very light.
S3: being location structure schematic diagram of the model drilling body 2 on die body seat 1, in die body seat 1 refering to the B-B cross-sectional view of Fig. 4
On glue note bushing 3 is installed, fixed by clay 8, at the hole location of glue note bushing 3, borrow fastening screw 5 and turn over and produces same belt transect glue
Infuse the location hole of the model drilling body 2 of bushing 3.
Drill jig is used to drill the process brief introduction of aircraft door glass Yu 9 rivet hole location of press strip:
S1: it will be positioned in groove that aircraft door glass is placed on die body seat 1 with press strip 9.
S2: model drilling body 2 is placed in the top of die body seat 1 and aircraft door glass and press strip 9, and fixed with fastening screw 5
On die body seat 1, it is sandwiched in aircraft door glass and press strip 9 between die body seat 1 and model drilling body 2.
S3: pull fast compactor 7 compress model drilling body 2 be allowed to firmly be posted by it is fixed on die body seat 1.
S4: rivet hole is carried out with press strip 9 to aircraft door glass using the drill bushing 4 in model drilling body 2 and is drilled.
S5: completing bore operation, successively opens fast compactor 7, pulls out fastening screw 5, removes model drilling body 2, i.e., desirable
The aircraft door glass and press strip 9 that rivet hole drills are completed out.
The drill jig of foregoing invention embodiment can be manufactured once, can be repeatedly used, it is possible to reduce processing cost is reduced
The wasting of resources.
Finally it should be noted that: the above embodiments are merely illustrative of the technical solutions of the present invention, but protection of the invention
Range is not limited thereto, and anyone skilled in the art in the technical scope disclosed by the present invention, can be thought easily
It is modified or replaceed to various equivalent, these, which are modified or replaceed, should all be included within the scope of the present invention.
Claims (10)
1. a kind of nonmetallic drilling equipment of aircraft door glass characterized by comprising
Die body seat (1), model drilling body (2), glue infuse bushing (3), drill bushing (4), fastening screw (5), technique bolt (6), compactor (7)
With press strip (9), in which:
It is arranged on die body seat (1) fluted；
Groove is for placing aircraft door glass and press strip (9)；
Model drilling body (2) is used to for aircraft door glass and press strip (9) being clipped in the middle with die body seat (1)；
Multiple fast compactors (7) are disposed within (2) one weeks around model drilling body on die body seat (1)；
Compactor (7) is used to compress die body seat (1) and model drilling body (2)；
Glue note bushing (3) is installed on die body seat (1)；
The rivet hole location produced on model drilling body (2) is turned over based on technique bolt (6) is provided with drill bushing (4)；
Die body seat (1) and model drilling body (2) are nonmetallic materials.
2. the apparatus according to claim 1, which is characterized in that wherein:
The type face of model drilling body (2) is to turn over the type face produced with glass-reinforced plastic material along rivet bore region.
3. the apparatus according to claim 1, which is characterized in that wherein:
The bulk of model drilling body (2) is within the scope of 900mm × 500mm × 100mm.
4. the apparatus according to claim 1, which is characterized in that wherein:
Model drilling body (2) thickness value is more than or equal to 10mm and is less than or equal to 15mm.
5. device according to claim 4, which is characterized in that wherein:
Model drilling body (2) thickness value is 12mm.
6. the apparatus according to claim 1, which is characterized in that wherein:
Model drilling body (2) width value is more than or equal to 25mm and is less than or equal to 35mm.
7. device according to claim 4, which is characterized in that wherein:
Model drilling body (2) thickness value is 30mm.
8. a kind of nonmetallic boring method of aircraft door glass, special for device described in any one of claim 1-7
Sign is, method includes the following steps:
The glass reinforced plastic working surface and rivet hole location on die body seat (1) are processed by numerically-controlled machine tool；
Model drilling body processed (2) are turned over, is padded on die body seat (1) by the thickness value of aircraft door glass and press strip (9) and adds certain thickness value
Padding, the type face for producing model drilling body (2) is turned over glass-reinforced plastic material along rivet bore region, then borrow technique bolt (6) and turn over system
The rivet hole location in model drilling body (2) and inlay drill bushing (4) out；
Remove padding after turning over finishing drilling die body (2) processed；
Glue note bushing (3) is installed on die body seat (1), fixed by clay (8), at the hole location of glue note bushing (3), it is fixed to borrow
Position bolt (5) turns over the location hole for producing the model drilling body (2) of same belt transect glue note bushing (3).
9. according to the method described in claim 8, it is characterized by further comprising:
Aircraft door glass and press strip (9) are placed in the groove on die body seat (1) Nei and positioned；
Model drilling body (2) is placed in the top of die body seat (1) and aircraft door glass and press strip (9), and fixed with fastening screw (5)
On die body seat (1), it is sandwiched in aircraft door glass and press strip (9) between die body seat (1) and model drilling body (2)；
Pull compactor (7) compress model drilling body (2) be allowed to firmly be posted by it is fixed on die body seat (1)；
Rivet hole is carried out with press strip (9) to aircraft door glass using the drill bushing (4) on model drilling body (2) to drill；
Bore operation is completed, fast compactor (7) is successively opened, pulls out fastening screw (5), removes model drilling body (2), and take out
Complete the aircraft door glass and press strip (9) that rivet hole drills.
10. method according to the claims, which is characterized in that further include:
The padding added with specified thickness value is padded on die body seat (1) by the thickness value of aircraft door glass and press strip (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910584642.3A CN110238975A (en) | 2019-07-01 | 2019-07-01 | The nonmetallic drilling equipment of aircraft door glass and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910584642.3A CN110238975A (en) | 2019-07-01 | 2019-07-01 | The nonmetallic drilling equipment of aircraft door glass and method |
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| Publication Number | Publication Date |
|---|---|
| CN110238975A true CN110238975A (en) | 2019-09-17 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910584642.3A Pending CN110238975A (en) | 2019-07-01 | 2019-07-01 | The nonmetallic drilling equipment of aircraft door glass and method |
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|---|---|---|---|---|
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2019
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Application publication date: 20190917 |