CN105782186A - Fixing device for airplane cap-shaped piece - Google Patents
Fixing device for airplane cap-shaped piece Download PDFInfo
- Publication number
- CN105782186A CN105782186A CN201610295752.4A CN201610295752A CN105782186A CN 105782186 A CN105782186 A CN 105782186A CN 201610295752 A CN201610295752 A CN 201610295752A CN 105782186 A CN105782186 A CN 105782186A
- Authority
- CN
- China
- Prior art keywords
- cap
- fixing device
- keeper
- aircraft
- eyelid covering
- 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
Links
- 210000000744 eyelid Anatomy 0.000 claims description 31
- 238000005516 engineering process Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
- F16B5/0291—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the threaded element being driven through the edge of a sheet plate with its axis in the plane of the plate
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/07—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of multiple interengaging protrusions on the surfaces, e.g. hooks, coils
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Clamps And Clips (AREA)
Abstract
The invention discloses a fixing device for an airplane cap-shaped piece. The periphery of the airplane cap-shaped piece is covered with a skin. The fixing device comprises a fixture body, a plurality of protection blocks, a plurality of cap-shaped piece positioning pieces and a plurality of connector positioning pieces, wherein the fixture body is used for supporting the cap-shaped piece covered with the skin, the periphery of the skin is surrounded by the protection blocks which are used for fixing the skin to the fixture body, the cap-shaped piece positioning pieces are fixed to the cap-shaped piece, and the connector positioning pieces are located on the cap-shaped piece. Each cap-shaped piece positioning piece is provided with a first positioning piece body fixed to the skin and a second positioning piece body fixed to the cap-shaped piece. According to the fixing device for the airplane cap-shaped piece, the skin is fixed to the fixture body through the protection blocks, the direction of the cap-shaped piece is fixed through the cap-shaped piece positioning pieces, and the fixing device is simple in structure, easy to use and capable of solving the cementing positioning problem of the cap-shaped piece and the skin.
Description
Technical field
The invention belongs to aircraft assembling riveting technology, relate to the fixing device of a kind of aircraft cap.
Background technology
Cap is widely used in aircraft, and this type of part is usually made by plastic cement brake forming at normal temperatures.Existing typically via the aircraft skin that is arranged around at cap, aircraft skin is the one layer of aluminium alloy making aircraft have good aerodynamic characteristics, and the effect of aircraft skin is to maintain aircraft configuration, so as to have good aerodynamic characteristics.By aircraft skin, cap being positioned, pressurize and glued joint fixing, its fixed form is more complicated.
Summary of the invention
For prior art Problems existing, it is an object of the invention to provide the fixing device of the aircraft cap of the splicing orientation problem of a kind of simple in construction, easy-to-use, solution cap and eyelid covering.
The fixing device of the present invention a kind of aircraft cap; the surrounding of aircraft cap is coated with by eyelid covering, including: support the clamp body of the cap being coated with by eyelid covering, be looped around around eyelid covering and for the multiple protection blocks this eyelid covering being fixed on clamp body, the multiple cap keepers being fixed on this cap and multiple joint keepers of being positioned on this cap；Wherein, each cap keeper is provided with the first keeper being fixed on eyelid covering and the second keeper being fixed on cap.
Further, also including multiple first screw, this first screw is on correspondence protection block and eyelid covering location extremely described clamp body.
Further, described second keeper is hook.
Further, described second keeper hooks and is located on cap.
Further, described cap keeper is respectively provided at the opposite sides of eyelid covering and cap, and every side is provided with multiple hat keeper.
Further, also including the second screw, each first keeper is by the fixing eyelid covering of two the second screws.
Further, described joint keeper is located on a side of hat keeper.
Further, described clamp body is square, and it is positioned at the bottom of this fixing device.
Further, cap and described clamp body are oppositely arranged, and the base area of cap is less than the surface area of clamp body.
The present invention is by protecting block to be fixed on clamp body by eyelid covering, by the direction of the fixing cap of cap keeper；Present configuration is simple, easy-to-use, solves the splicing orientation problem of cap and eyelid covering.
Accompanying drawing explanation
Fig. 1 is the front view of the fixing device of cap of the present invention；
Fig. 2 is the top view of the fixing device of cap of the present invention；
Fig. 3 is the Fig. 2 sectional view at A-A place；
Fig. 4 is the Fig. 2 sectional view at B-B place.
Wherein, 1-clamp body, 2-protect block, 3-cap keeper, 31-the first keeper, 32-the second keeper, 4-joint keeper, 5-the first screw, 6-the second screw.
Detailed description of the invention
Below, with reference to accompanying drawing, the present invention is more fully illustrated, shown in the drawings of the exemplary embodiment of the present invention.But, the present invention can be presented as multiple multi-form, is not construed as the exemplary embodiment being confined to describe here.And it is to provide these embodiments, so that the present invention is fully and completely, and will fully convey the scope of the invention to those of ordinary skill in the art.
For ease of illustrating, here can use such as " on ", the space relative terms such as D score " left side " " right side ", be used for shown in figure a element or the feature relation relative to another element or feature is described.It should be understood that except the orientation shown in figure, spatial terminology is intended to include device different azimuth in use or operation.Such as, if the device in figure is squeezed, be stated as the element being positioned at other elements or feature D score will be located into other elements or feature " on ".Therefore, exemplary term D score can comprise upper and lower both orientation.Device can otherwise position (90-degree rotation or be positioned at other orientation), relatively illustrates used herein of space correspondingly to explain.
As shown in Figures 1 to 4, the fixing device of the present invention a kind of aircraft cap, the surrounding of aircraft cap 100 is coated with by eyelid covering 200, and this fixing device is used for adopting fixing cap 100 and eyelid covering 200.
This fixing device includes: supports the clamp body 1 of the cap being coated with by eyelid covering, be looped around around eyelid covering 200 and for the multiple protection blocks 2 being fixed on by eyelid covering on clamp body 1, the multiple cap keepers 3 being fixed on this cap 100 and the multiple joint keepers 4 being positioned on this cap and being used for fitting joint.
This clamp body 1 is in square, and it is positioned at the bottom of this fixing device.Cap 100 and this clamp body 1 are oppositely arranged, and the base area of cap 100 is less than the surface area of clamp body 1.
Protection block 2 is for positioning the surrounding of eyelid covering 200.In the present embodiment, it is provided with by four protection blocks 2.This fixing device is additionally provided with multiple first screw 5, and the first screw 5 sequentially protects block 2 and eyelid covering 200, and location is to clamp body 1, it is achieved eyelid covering 200 is fixed on clamp body 1 by protection block 2.
Cap keeper 3 is positioned on cap 100 and eyelid covering 200, and this hat keeper 3 is arranged on the opposite sides of clamp body 1, and in the present embodiment, every side is provided with 9 cap keepers.
Each hat keeper 3 is provided with the first keeper 31 and the second keeper 32 being connected with this first keeper 31.Wherein, each first keeper 31 fixes eyelid covering 200 by two the second screws 6；Second keeper 32 is hook, and this second keeper 32 hooks and is located on cap 200, to position the horizontal direction of cap 200.
Joint keeper 4 is located on a side of hat keeper 200, in the present embodiment, is provided with 4 joint keepers；Joint (not shown) is connected on this joint keeper 4.
The present invention is by protecting block to be fixed on clamp body by eyelid covering, by the direction of the fixing cap of cap keeper；Present configuration is simple, easy-to-use, solves the splicing orientation problem of cap and eyelid covering.
Claims (9)
1. the fixing device of an aircraft cap; the surrounding of aircraft cap is coated with by eyelid covering; it is characterized in that, including: support the clamp body of the cap being coated with by eyelid covering, be looped around around eyelid covering and for the multiple protection blocks this eyelid covering being fixed on clamp body, the multiple cap keepers being fixed on this cap and multiple joint keepers of being positioned on this cap；Wherein, each cap keeper is provided with the first keeper being fixed on eyelid covering and the second keeper being fixed on cap.
2. the fixing device of aircraft cap according to claim 1, it is characterised in that: also including multiple first screw, this first screw is on correspondence protection block and eyelid covering location extremely described clamp body.
3. the fixing device of aircraft cap according to claim 1, it is characterised in that: described second keeper is hook.
4. the fixing device of aircraft cap according to claim 3, it is characterised in that: described second keeper hooks and is located on cap.
5. the fixing device of aircraft cap according to claim 1, it is characterised in that: described cap keeper is respectively provided at the opposite sides of eyelid covering and cap, and every side is provided with multiple hat keeper.
6. the fixing device of aircraft cap according to claim 1, it is characterised in that: also including the second screw, each first keeper is by the fixing eyelid covering of two the second screws.
7. the fixing device of aircraft cap according to claim 1, it is characterised in that: described joint keeper is located on a side of hat keeper.
8. the fixing device of aircraft cap according to claim 1, it is characterised in that: described clamp body is square, and it is positioned at the bottom of this fixing device.
9. the fixing device of aircraft cap according to claim 1, it is characterised in that: cap and described clamp body are oppositely arranged, and the base area of cap is less than the surface area of clamp body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610295752.4A CN105782186B (en) | 2016-05-06 | 2016-05-06 | The fixing device of aircraft cap |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610295752.4A CN105782186B (en) | 2016-05-06 | 2016-05-06 | The fixing device of aircraft cap |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105782186A true CN105782186A (en) | 2016-07-20 |
| CN105782186B CN105782186B (en) | 2017-10-13 |
Family
ID=56401685
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610295752.4A Active CN105782186B (en) | 2016-05-06 | 2016-05-06 | The fixing device of aircraft cap |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105782186B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111452991A (en) * | 2019-01-20 | 2020-07-28 | 成都飞机工业（集团）有限责任公司 | Gluing positioning method for control surface of composite material airplane with multiple joints |
| CN111452990A (en) * | 2019-01-20 | 2020-07-28 | 成都飞机工业（集团）有限责任公司 | Gluing positioning method for control surface of composite material airplane with multiple joints |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009185961A (en) * | 2008-02-08 | 2009-08-20 | Seiko Epson Corp | Fixing device and fixing method |
| US20090320337A1 (en) * | 2008-06-30 | 2009-12-31 | Giovanni Biondan | Device and method for fixing commemorative and similar inscriptions |
| CN202623291U (en) * | 2012-05-10 | 2012-12-26 | 浙江西子航空工业有限公司 | Mold for metal bonding of aluminum honeycombs |
| CN104259513A (en) * | 2014-09-16 | 2015-01-07 | 沈阳飞机工业（集团）有限公司 | Skin stretch part automatic hole production device and method |
| CN104595332A (en) * | 2013-10-31 | 2015-05-06 | 鸿富锦精密工业（深圳）有限公司 | Fixing device having stud |
| CN204843945U (en) * | 2015-07-14 | 2015-12-09 | 中航飞机股份有限公司西安飞机分公司 | Aircraft rib conformal device |
-
2016
- 2016-05-06 CN CN201610295752.4A patent/CN105782186B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009185961A (en) * | 2008-02-08 | 2009-08-20 | Seiko Epson Corp | Fixing device and fixing method |
| US20090320337A1 (en) * | 2008-06-30 | 2009-12-31 | Giovanni Biondan | Device and method for fixing commemorative and similar inscriptions |
| CN202623291U (en) * | 2012-05-10 | 2012-12-26 | 浙江西子航空工业有限公司 | Mold for metal bonding of aluminum honeycombs |
| CN104595332A (en) * | 2013-10-31 | 2015-05-06 | 鸿富锦精密工业（深圳）有限公司 | Fixing device having stud |
| CN104259513A (en) * | 2014-09-16 | 2015-01-07 | 沈阳飞机工业（集团）有限公司 | Skin stretch part automatic hole production device and method |
| CN204843945U (en) * | 2015-07-14 | 2015-12-09 | 中航飞机股份有限公司西安飞机分公司 | Aircraft rib conformal device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111452991A (en) * | 2019-01-20 | 2020-07-28 | 成都飞机工业（集团）有限责任公司 | Gluing positioning method for control surface of composite material airplane with multiple joints |
| CN111452990A (en) * | 2019-01-20 | 2020-07-28 | 成都飞机工业（集团）有限责任公司 | Gluing positioning method for control surface of composite material airplane with multiple joints |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105782186B (en) | 2017-10-13 |
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