CN106516156A - Shape-preserving jackstay of aircraft transparent part - Google Patents
Shape-preserving jackstay of aircraft transparent part Download PDFInfo
- Publication number
- CN106516156A CN106516156A CN201611079946.7A CN201611079946A CN106516156A CN 106516156 A CN106516156 A CN 106516156A CN 201611079946 A CN201611079946 A CN 201611079946A CN 106516156 A CN106516156 A CN 106516156A
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- China
- Prior art keywords
- conformal
- strut
- fixed pattern
- mass activity
- activity type
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- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to a shape-preserving jackstay of an aircraft transparent part and belongs to the field of aircraft transparent part manufacturing. The shape-preserving jackstay can be of three structural types, namely an outer fixed type shape-preserving jackstay, an inner fixed type shape-preserving jackstay or an overall movable type shape-preserving jackstay. According to the shape-preserving jackstay of the aircraft transparent part, by using the shape-preserving jackstay, the deflecting deformation of the transparent part during storage can be prevented, and the shape-preserving jackstay can be used for deflecting low-heat shape righting of an oriented organic glass transparent part.
Description
Technical field
The present invention relates to a kind of conformal strut of aircraft transparencies, belongs to aircraft transparencies manufacture field.
Background technology
Advanced war craft Transparent Parts are typically curve form, lucite material.The molding of perspex transparent part and
Processing can produce certain residual stress, and this can cause Transparent Parts to deform due to Stress Release during storage.Therefore thoroughly
After bright part is manufactured, need to preserve under stable environment, to be subsequently assembled on aircraft hatchcover or windscreen.
The content of the invention
A kind of present invention aim at provide aircraft transparencies conformal strut, it is an object of the invention to aircraft transparencies support
Bar is opened file location for Transparent Parts and is fixed, and keeps Transparent Parts to open a grade size in storage, it can also be used to which oriented organo glass is saturating
The orthopedic fixation of bright part.
The present invention to achieve these goals, is adopted the following technical scheme that：
A kind of conformal strut of aircraft transparencies, its conformal pole structure have three kinds of fixed types, respectively：Outer fixed pattern is conformal
Strut, the conformal strut of interior fixed pattern or the conformal strut of mass activity type；
The conformal strut of the outer fixed pattern is bilateral symmetry：The outer side shield of outer fixed pattern of the conformal strut of outer fixed pattern is adopted
It is welded and fixed, the distance between medial surface of the outer side shield of two symmetrical outer fixed patterns opens a grade size for conformal Transparent Parts；
Outer fixed pattern inner side baffle is that perforating movable is installed, and screws spiral shell button in the inner side of outer fixed pattern inner side baffle equipped with first, first
The two ends of strut are tapped near outer fixed pattern inner side baffle；
The conformal strut of the interior fixed pattern is bilateral symmetry：In the outer side shield of the interior fixed pattern of the conformal strut of interior fixed pattern it is
Perforating movable is installed, interior fixed pattern inner side baffle for being welded and fixed, on the outside of two symmetrical interior fixed pattern inner side baffles between
Distance opens a grade size for conformal Transparent Parts, screws spiral shell button, the second strut in the outside of the outer side shield of interior fixed pattern equipped with second
Two ends it is tapped near the outer side shield of interior fixed pattern；
The conformal strut of the mass activity type is bilateral symmetry：On the outside of the mass activity type of the conformal strut of mass activity type
Baffle plate and mass activity type inner side baffle are perforating movable installation, on the inside of the outer side shield of mass activity type and mass activity type
The outermost of baffle plate and most inner side screw spiral shell button equipped with the 3rd, the two ends of the 3rd strut are all tapped.
Further, the region for contacting with conformal Transparent Parts in the baffle plate of the conformal strut of three kinds of fixed types is pasted with rubber
Plate or flannelette.
Left baffle is installed in metallic rod, grade size is opened using being welded and fixed or screw activity according to aircraft transparencies.
Baffle plate pastes rubber sheet or flannelette with Transparent Parts contact surface so that be difficult to scratch Transparent Parts surface when contacting with Transparent Parts.It is living
Dynamic baffle plate perforate, through support bar, screws tight knob control position and screws by screwing.Strut of the present invention is divided into outer fixation, interior
Fixed, three kinds of versions of mass activity.
Beneficial effects of the present invention
The present invention uses the conformal strut, can prevent open shelves of the Transparent Parts in storage from deforming, can be used for orienting organic glass
Glass Transparent Parts to open grade low grade fever orthopedic.
Description of the drawings
Fig. 1 is the facade structures schematic diagram of the present invention conformal strut of outer fixed pattern；
Fig. 2 is the facade structures schematic diagram of the conformal strut of fixed pattern in the present invention；
Fig. 3 is the facade structures schematic diagram of the conformal strut of mass activity type of the present invention；
Fig. 4 is the structural representation of the present invention conformal strut of outer fixed pattern；
Fig. 5 is the structural representation of the conformal strut of fixed pattern in the present invention；
Fig. 6 is the structural representation of the conformal strut of mass activity type of the present invention；
Fig. 7 is side plate schematic shapes of the present invention；
Fig. 8 is pasted with rubber slab or flannelette for side of the present invention（14）Structural representation.
Specific embodiment
1 ~ 8 describe the present invention below in conjunction with the accompanying drawings：
The conformal strut of aircraft transparencies is mainly used with the sufficiently rigid upright bar of steel, and two baffle plates are respectively installed at its two ends
Spiral shell button is screwed with some.By screwing the gap between spiral shell button controllable register, so as to by aircraft transparencies end face clamping, reach guarantor
Shape purpose.The conformal pole structure has three types, and its view is shown in Fig. 1-Fig. 6.
A kind of conformal strut of aircraft transparencies, the conformal pole structure have three kinds of fixed types, respectively：Outer fixed pattern is protected
Shape strut, the conformal strut of interior fixed pattern or the conformal strut of mass activity type；
The conformal strut of the outer fixed pattern is bilateral symmetry：The outer side shield 1 of outer fixed pattern of the conformal strut of outer fixed pattern is adopted
With being welded and fixed, the distance between medial surface of the outer side shield 1 of two symmetrical outer fixed patterns opens a grade chi for conformal Transparent Parts 3
It is very little；Outer fixed pattern inner side baffle 2 is installed for perforating movable, screws spiral shell button in the inner side of outer fixed pattern inner side baffle 2 equipped with first
4, the two ends of the first strut 5 are tapped near outer fixed pattern inner side baffle 2；
The conformal strut of the interior fixed pattern is bilateral symmetry：In the outer side shield 6 of the interior fixed pattern of the conformal strut of interior fixed pattern
Install for perforating movable, interior fixed pattern inner side baffle 7 for being welded and fixed, on the outside of two symmetrical interior fixed pattern inner side baffles 7 it
Between distance be that conformal Transparent Parts open a grade size, screw spiral shell button 8 in the outside of the outer side shield 6 of interior fixed pattern equipped with second, the
The two ends of two struts 9 are tapped near the outer side shield 6 of interior fixed pattern；
The conformal strut of the mass activity type is bilateral symmetry：On the outside of the mass activity type of the conformal strut of mass activity type
Baffle plate 10 and mass activity type inner side baffle 11 are perforating movable installation, in the outer side shield 10 of mass activity type and mass activity
The outermost of type inner side baffle 11 and most inner side screw spiral shell button 12 equipped with the 3rd, the two ends of the 3rd strut 13 are all tapped.
The region contacted with conformal Transparent Parts in the baffle plate of the conformal strut of three kinds of fixed types is pasted with rubber slab or flannelette
14。
Paste δ=1～2mm's with FN303 or other rubbers based adhesives in the region that conformal strut epipleural is contacted with Transparent Parts
Rubber slab or flannelette, as shown in Fig. 8 14.The shape of side plate can shape can also be other type shapes as shown in Figure 7,
Its bottom surface should be plane.It can be metal or engineering plastics etc. to screw spiral shell button material, internal tapping.
Claims (2)
1. the conformal strut of a kind of aircraft transparencies, it is characterised in that：The conformal pole structure has three kinds of fixed types, respectively：
The conformal strut of outer fixed pattern, the conformal strut of interior fixed pattern or the conformal strut of mass activity type；
The conformal strut of the outer fixed pattern is bilateral symmetry：The outer side shield of outer fixed pattern of the conformal strut of outer fixed pattern（1）
Using being welded and fixed, the outer side shield of two symmetrical outer fixed patterns（1）The distance between medial surface be conformal Transparent Parts（3）'s
Open a grade size；Outer fixed pattern inner side baffle（2）Install for perforating movable, in outer fixed pattern inner side baffle（2）Inner side equipped with the
One screws spiral shell button（4）, the first strut（5）Two ends near outer fixed pattern inner side baffle（2）It is tapped；
The conformal strut of the interior fixed pattern is bilateral symmetry：In the outer side shield of the interior fixed pattern of the conformal strut of interior fixed pattern
（6）Install for perforating movable, interior fixed pattern inner side baffle（7）For being welded and fixed, two symmetrical interior fixed pattern inner side baffles（7）
A grade size is opened for conformal Transparent Parts in the distance between outside, in the outer side shield of interior fixed pattern（6）Outside screw equipped with second
Spiral shell button（8）, the second strut（9）Two ends near the outer side shield of interior fixed pattern（6）It is tapped；
The conformal strut of the mass activity type is bilateral symmetry：On the outside of the mass activity type of the conformal strut of mass activity type
Baffle plate（10）With mass activity type inner side baffle（11）Perforating movable installation is, in the outer side shield of mass activity type（10）With it is whole
Body active type inner side baffle（11）Outermost and most inner side screw spiral shell button equipped with the 3rd（12）, the 3rd strut（13）Two ends all
It is tapped.
2. the conformal strut of aircraft transparencies according to claim 1, it is characterised in that：
The region contacted with conformal Transparent Parts in the baffle plate of the conformal strut of three kinds of fixed types is pasted with rubber slab or flannelette（14）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611079946.7A CN106516156B (en) | 2016-11-30 | 2016-11-30 | A kind of conformal strut of aircraft transparencies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611079946.7A CN106516156B (en) | 2016-11-30 | 2016-11-30 | A kind of conformal strut of aircraft transparencies |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106516156A true CN106516156A (en) | 2017-03-22 |
| CN106516156B CN106516156B (en) | 2019-03-29 |
Family
ID=58353782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611079946.7A Active CN106516156B (en) | 2016-11-30 | 2016-11-30 | A kind of conformal strut of aircraft transparencies |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106516156B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201023652Y (en) * | 2007-04-24 | 2008-02-20 | 江西洪都航空工业集团有限责任公司 | Airplane integral movement canopy framework |
| CN101868382A (en) * | 2007-06-28 | 2010-10-20 | 法雷奥系统公司 | Windscreen wiper blade retention device |
| CN201847183U (en) * | 2010-10-20 | 2011-06-01 | 厦门市建潘卫厨有限公司 | Anti-deformation emptying table top |
| CN202863565U (en) * | 2012-10-16 | 2013-04-10 | 上海汽车集团股份有限公司 | Lower beam structure of windscreen |
-
2016
- 2016-11-30 CN CN201611079946.7A patent/CN106516156B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201023652Y (en) * | 2007-04-24 | 2008-02-20 | 江西洪都航空工业集团有限责任公司 | Airplane integral movement canopy framework |
| CN101868382A (en) * | 2007-06-28 | 2010-10-20 | 法雷奥系统公司 | Windscreen wiper blade retention device |
| CN201847183U (en) * | 2010-10-20 | 2011-06-01 | 厦门市建潘卫厨有限公司 | Anti-deformation emptying table top |
| CN202863565U (en) * | 2012-10-16 | 2013-04-10 | 上海汽车集团股份有限公司 | Lower beam structure of windscreen |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106516156B (en) | 2019-03-29 |
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