CN104386241A - Protective hood for organic glass transparent component of hatch cover of aircraft - Google Patents
Protective hood for organic glass transparent component of hatch cover of aircraft Download PDFInfo
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- CN104386241A CN104386241A CN201410609313.7A CN201410609313A CN104386241A CN 104386241 A CN104386241 A CN 104386241A CN 201410609313 A CN201410609313 A CN 201410609313A CN 104386241 A CN104386241 A CN 104386241A
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- aircraft
- protective case
- main body
- hatch cover
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Abstract
The invention relates to a protective hood for an organic glass transparent component of a hatch cover of an aircraft, and belongs to the technical field of manufacturing aircrafts. The protective hood comprises a aircraft protecting hood main body which is covered on the hatch cover of the aircraft, wherein a hanging device, an alignment directional line, product information signs on the hatch cover and a manually raising handle are arranged on the external surface of the aircraft protecting hood main body, and at least 3 rigidity reinforcing bands are distributed on the external surface of the aircraft protecting hood main body. Through the adoption of the protective hood for the hatch cover of the aircraft, the organic glass transparent component in a hatch cover component storing stage, an aircraft assembly manufacturing stage, an aircraft testing stage, an aircraft maintaining stage and a grounding stage can be effectively protected, damage from various outward materials to the organic glass transparent component can be effectively avoided, and the component information of the hatch cover is also convenient to identify. Compared with a traditional protection method, through the use of the protective hood, the work strength of manufacturing personnel, testing personnel, flight testing personnel and ground personnel is effectively reduced, and the work efficiency is improved.
Description
Technical field
The present invention relates to a kind of protective case of aircraft cabin lid perspex transparent part, belong to aircraft manufacturing technical field.
Background technology
The protection of conventional airplane hatchcover perspex transparent part adopts canvas, cotton, craft paper, spray protective film etc.These methods can not resist larger external force and hard objects is impacted, and some can not effectively waterproof, laying property and dismounting property be poor.
Summary of the invention
In order to overcome above-mentioned defect; the object of the invention is the protective case providing a kind of aircraft cabin lid perspex transparent part, solves perspex transparent part and deposits stage, transporation by plane fabrication phase, aircraft testing stage, aircraft maintenance stage in hatchcover components and treat that (stopping) flies the protection in stage.
To achieve these goals, the present invention adopts following technical scheme:
A kind of protective case of aircraft cabin lid perspex transparent part, it comprises the aircraft protective case main body that covers aircraft hatchcover, this aircraft protective case body outer surface is provided with erecting by overhang, aligning direction line, hatchcover product information mark, hand lift handle, aircraft protective case body outer surface is distributed with at least 3 rigidity stiffening bands;
Described erecting by overhang it comprise a hanging ring anchor fitting, have metal suspension ring in hanging ring anchor fitting inner sleeve;
Described aircraft protective case main body internal layer is flannelette napped fabric layer, and skin is glass fiber reinforced plastic protective cover body;
Hand is lifted handle and is connected and fixed by screw and glass fiber reinforced plastic protective cover body;
Outer protective paint layer is sprayed with at the outside face of glass fiber reinforced plastic protective cover body.
Described hand lifts the distance >=10mm of handle distance aircraft protective case body rim.
Thickness >=the 3mm of described flannelette napped fabric layer.
Beneficial effect of the present invention:
The present invention utilize this aircraft hatchcover protective case can effectively solve perspex transparent part hatchcover components deposit the stage, the transporation by plane fabrication phase, the aircraft testing stage, the aircraft maintenance stage and the grounding stage protection; various external substance effectively can be avoided the damage of perspex transparent part, be also convenient to hatchcover components message identification.This device compares traditional guard method, effectively lower manufacturer, testing crew, take a flight test and ground crew working strength and improve work efficiency.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is erecting by overhang of the present invention (2) installation site structural representation;
Fig. 3 is that hand of the present invention lifts handle (6) installation site structural representation;
Fig. 4 is the cross-sectional view of aircraft protective case main body (1) of the present invention.
Detailed description of the invention
Describe the present invention below in conjunction with accompanying drawing 1,2,3,4:
A kind of protective case of aircraft cabin lid perspex transparent part, it comprises the aircraft protective case main body 1 that covers aircraft hatchcover, this aircraft protective case main body 1 outside face is provided with erecting by overhang 2, aligning direction line 3, hatchcover product information mark 4, hand lift handle 6, aircraft protective case main body 1 outside face is distributed with at least 3 rigidity stiffening bands 5;
Described erecting by overhang 2 it comprise a hanging ring anchor fitting 7, have metal suspension ring 8 in hanging ring anchor fitting 7 inner sleeve;
Described aircraft protective case main body 1 internal layer is flannelette napped fabric layer 11, and skin is glass fiber reinforced plastic protective cover body 12;
Hand is lifted handle 6 and is connected and fixed by screw 13 and glass fiber reinforced plastic protective cover body 12;
Outer protective paint layer 14 is sprayed with at the outside face of glass fiber reinforced plastic protective cover body 12.
Described hand lifts the distance >=10mm of handle 6 apart from aircraft protective case main body 1 edge.
Thickness >=the 3mm of described flannelette napped fabric layer 11.
One, protective case cover body manufactures:
First by aircraft cabin lid perspex transparent part fixed position (for two-crew cockpit, it is involutory fixing to press hatchcover profile, and opposite joint seals), spray mold release on its outer surface or lay release cloth and form mould.Then hand is stuck with paste or on paving glass fabric/epoxy prepreg and mould, thickness >=2mm, is cured by its resin solidification parameter, solidifies aft-loaded airfoil and cuts unnecessary rim charge.Then on drip molding, place the hawser of more than 3 diameter >=40mm; spacing controls evenly, and then its surperficial paving glass fibre/epoxy resin forms stiffening band; the unnecessary hawser of clip double end after solidification is also worked into distance protection shroud rim 10mm, seals with epoxide-resin glue.Ready-made half-blank protective case sprays paint, and easily distinguishes color paint with other and spray aligning direction line 3 in Fig. 1, and for the hatchcover product information mark 4 of sticky note hatchcover components or Transparent Parts load card.
Two, protective case remaining parts is installed
Install erecting by overhang by Fig. 1 in protective case surrounding (rectangle end points) level, in Fig. 2, hanging ring anchor fitting 7 is the anchor fitting of metal suspension ring 8, is connected with protective case with screw.The type of attachment that handle distance edge >=10mm, Fig. 3 hand lifts handle 9 is lifted at protective case surrounding (rectangle end points) level installation hand in the position of lifting handle 6 by hand in Fig. 1, is connected with protective case with screw.All attaching partss must not affect protective case inside face.The glue that finally can be used for sticky note flannelette and glass fiber reinforced plastic surface at protective case inside face epoxy glue or other glues note a layer thickness >=3mm flannelette 13 and protective case inside face, sees Fig. 4.
Claims (3)
1. the protective case of an aircraft cabin lid perspex transparent part, it is characterized in that: it comprises the aircraft protective case main body (1) that covers aircraft hatchcover, this aircraft protective case main body (1) outside face is provided with erecting by overhang (2), aligning direction line (3), hatchcover product information mark (4), hand lift handle (6), aircraft protective case main body (1) outside face is distributed with at least 3 rigidity stiffening bands (5);
Described erecting by overhang (2) it comprise a hanging ring anchor fitting (7), have metal suspension ring (8) in hanging ring anchor fitting (7) inner sleeve;
Described aircraft protective case main body (1) internal layer is flannelette napped fabric layer (11), and skin is glass fiber reinforced plastic protective cover body (12);
Hand is lifted handle (6) and is connected and fixed by screw (13) and glass fiber reinforced plastic protective cover body (12);
Outer protective paint layer (14) is sprayed with at the outside face of glass fiber reinforced plastic protective cover body (12).
2. the protective case of aircraft cabin lid perspex transparent part according to claim 1, is characterized in that: described hand lifts the distance >=10mm at handle (6) distance aircraft protective case main body (1) edge.
3. the protective case of aircraft cabin lid perspex transparent part according to claim 1, is characterized in that: the thickness >=3mm of described flannelette napped fabric layer (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410609313.7A CN104386241B (en) | 2014-11-04 | 2014-11-04 | A kind of protective cover of aircraft cabin lid perspex transparent part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410609313.7A CN104386241B (en) | 2014-11-04 | 2014-11-04 | A kind of protective cover of aircraft cabin lid perspex transparent part |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104386241A true CN104386241A (en) | 2015-03-04 |
| CN104386241B CN104386241B (en) | 2016-08-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410609313.7A Active CN104386241B (en) | 2014-11-04 | 2014-11-04 | A kind of protective cover of aircraft cabin lid perspex transparent part |
Country Status (1)
| Country | Link |
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| CN (1) | CN104386241B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292302A (en) * | 2015-11-10 | 2016-02-03 | 德文能源股份有限公司 | Automobile part protective cover |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5318251A (en) * | 1991-12-05 | 1994-06-07 | Minnesota Mining And Manufacturing Company | Protective flexible boot |
| US5622336A (en) * | 1994-04-18 | 1997-04-22 | Aerospatiale Societe Nationale Industrielle | Device for the protection of a control surface hinge particularly for an aircraft |
| CN102458839A (en) * | 2009-04-14 | 2012-05-16 | 克莱博格橡胶股份有限公司 | Composite components and heat-curing resins and elastomers |
| CN103658475A (en) * | 2013-11-28 | 2014-03-26 | 江西洪都航空工业集团有限责任公司 | Airplane two-seater canopy framework integral-forging method |
| CN204250358U (en) * | 2014-11-04 | 2015-04-08 | 江西洪都航空工业集团有限责任公司 | A kind of protective case of aircraft cabin lid perspex transparent part |
-
2014
- 2014-11-04 CN CN201410609313.7A patent/CN104386241B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5318251A (en) * | 1991-12-05 | 1994-06-07 | Minnesota Mining And Manufacturing Company | Protective flexible boot |
| US5622336A (en) * | 1994-04-18 | 1997-04-22 | Aerospatiale Societe Nationale Industrielle | Device for the protection of a control surface hinge particularly for an aircraft |
| CN102458839A (en) * | 2009-04-14 | 2012-05-16 | 克莱博格橡胶股份有限公司 | Composite components and heat-curing resins and elastomers |
| CN103658475A (en) * | 2013-11-28 | 2014-03-26 | 江西洪都航空工业集团有限责任公司 | Airplane two-seater canopy framework integral-forging method |
| CN204250358U (en) * | 2014-11-04 | 2015-04-08 | 江西洪都航空工业集团有限责任公司 | A kind of protective case of aircraft cabin lid perspex transparent part |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292302A (en) * | 2015-11-10 | 2016-02-03 | 德文能源股份有限公司 | Automobile part protective cover |
| CN105292302B (en) * | 2015-11-10 | 2018-01-19 | 宣城市东科电器有限公司 | A kind of automobile component protective cover |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104386241B (en) | 2016-08-17 |
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