CN102233949A - Main windshield assembly and method of installing same - Google Patents
Main windshield assembly and method of installing same Download PDFInfo
- Publication number
- CN102233949A CN102233949A CN2010101684306A CN201010168430A CN102233949A CN 102233949 A CN102233949 A CN 102233949A CN 2010101684306 A CN2010101684306 A CN 2010101684306A CN 201010168430 A CN201010168430 A CN 201010168430A CN 102233949 A CN102233949 A CN 102233949A
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- windscreen
- main air
- assembly set
- skeleton
- skylight
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- 238000000034 method Methods 0.000 title claims abstract description 8
- 238000003825 pressing Methods 0.000 claims abstract description 22
- 238000009434 installation Methods 0.000 claims description 9
- 238000007789 sealing Methods 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 3
- 238000012360 testing method Methods 0.000 claims description 3
- 239000003795 chemical substances by application Substances 0.000 claims description 2
- 239000011248 coating agent Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 claims description 2
- 238000009499 grossing Methods 0.000 claims description 2
- 238000007689 inspection Methods 0.000 claims description 2
- 239000000696 magnetic material Substances 0.000 claims description 2
- 230000002787 reinforcement Effects 0.000 claims description 2
- 230000000007 visual effect Effects 0.000 abstract description 3
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 239000011521 glass Substances 0.000 description 6
- 238000013461 design Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000010006 flight Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000008093 supporting effect Effects 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 210000001364 upper extremity Anatomy 0.000 description 1
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- Body Structure For Vehicles (AREA)
- Securing Of Glass Panes Or The Like (AREA)
Abstract
The invention relates to a main windshield assembly for an aircraft and a method of installing the same. The main windshield assembly comprises a windshield, a pressing plate, a skylight framework and a connecting piece, wherein the windshield is fixed between the pressing plate and the skylight framework through the connecting piece and is in a curved surface shape. The main windshield assembly has the advantages of good visual field, cockpit space and aerodynamic characteristics, good bird impact resistance, more open emergency evacuation channels for drivers, greatly prolonged fatigue life and capability of quickly assembling and maintaining the main windshield.
Description
Technical field
The present invention relates to be used for the main air retaining assembly set and the installation method thereof of aircraft.
Background technology
The aircraft windshield is a structural features important on the aircraft.As the part of fuselage, windshield wants to bear structural load and the impact under the various state of flights; Simultaneously, windshield will provide visual field and good optical performance clearly for chaufeur, also will possess the deicing demist, lets out static, anti-rainwater etc. is all multi-functional.Requirement on structure and function contradiction often concerning material, windshield technology are exactly to satisfy the specific (special) requirements of the performance such as various mechanics, optics, electricity, environment of aircraft by the research of aspects such as material selection, structure design, manufacturing process, test evaluation simultaneously.
Although the windscreen of aspect helps thickening thickness of glass, can strengthen the structural load of bearing under the various state of flights and the performance of impact, and the plane curvature tolerance is good, this kind windscreen has a strong impact on aviator's field range.
In the windscreen assembling unit structure that has proposed at present, publication number be US 2003/0062450A1 U.S. Patent Publication the one chip flange design of windshield annex, windscreen is clamped in the groove of window frame structure by the one chip flange.In the outside of one chip flange, the windscreen pressing plate is installed again.The mounting means of this windscreen, complex structure, the loading transfer of bearing on the windscreen is not direct to the route of peripheral window frame structure yet.
Publication number is that the Chinese patent application of CN 101473143 discloses a kind of being used for being inserted in the nut that two aircraft windshields between the holding element are fixed, and described holding element is assembled by at least one link that is made of bolt and described nut and remained to together; Described nut is made of two parts.When nut damages, especially when changing windshield, can change described nut easily.But it also is aspect that windshield is adopted in this patent application.
Summary of the invention
The objective of the invention is to overcome existing above-mentioned shortcoming in the existing design.
According to an exemplary embodiment of the present invention, main air retaining assembly set comprises windscreen, pressing plate, skylight skeleton and attaching parts, and wherein windscreen is fixed between pressing plate and the skylight skeleton by attaching parts, and windscreen adopts the curved-surface structure form.Be preferably the single-curvature surface shape.The for example monolateral transparent region area of main air retaining is approximately 0.5m
2Thereby, with respect to the plane windscreen visual field, driving compartment space and aerodynamic characteristic preferably being arranged, anti-preferably bird is hit performance, and driver emergency is withdrawn passage and is more opened wide.
Windscreen is fixed between pressing plate and the skylight skeleton by attaching parts, and the presser type mounting means that adopts tripartite pressing plate, a side to insert can carry out the assembling and the maintenance of main air retaining fast.Because participation structure is not stressed for the windscreen of presser type mounting means, improve the fatigue life of windscreen greatly.In addition, the main air retaining adopts presser type to install with convenient outside dismounting and maintenance, and is convenient and swift.And the main air of presser type mounting means keeps off that participation structure is not stressed, and with respect to the Transparent Parts of the bonded assembly windscreen that directly is spirally connected, improve its fatigue life greatly.
The presser type of curved wind screen is installed, and makes the design of structure-skylight skeleton of windscreen periphery have more challenge.Main air retaining Transparent Parts bottom all has skeleton to support preferably, so the main air retaining is when bearing bird and hit impact load, and Transparent Parts can be delivered to load on the skeleton rapidly, thereby the anti-bird of improving Transparent Parts is hit ability.
Advantageously, skylight skeleton itself needs also to consider that bird hits factor, and skeleton each cross-sectional plane in skylight all has the higher bending resistance height and the interior edge strip of broad, in the time of bearing bird preferably and hit moment very big moment of flexure.
Advantageously, the skylight skeleton adopts dispersion to cross with canopy top plate, sidewall paneling, the isostructural connection of each associated frame, avoids too much rib to concentrate junction, to improve each part stress situation.The top of skylight skeleton is set up by the antitorque camber beam of glass frame upper limb and is added the keystone configuration form that the radial pattern skeleton is the master, the bottom is supported on each close frame by the many fulcrum hinge joints of window frame lower edge beam, formation is based on many point supportings structure of close frame, and downward, back kick increases progressively compressive load.
Advantageously, skylight skeleton area arrangements more reinforcement backing plate be connected with surrounding covering, can pass better and carry, improve the stand under load situation of whole regional structure greatly.
Advantageously, the material of skylight skeleton part itself, in-to-in attaching parts and with the attaching parts of pressing plate, all adopt non-magnetic material, therefore, guarantee the serviceability of equipment such as standby magnetic compass.
Such structure design has guaranteed that the presser type installation of large tracts of land curved surface main air retaining is achieved.
Figure of description
Fig. 1 is the erection plan according to main air retaining assembly set of the present invention;
Fig. 2 is the scheme drawing according to main air retaining assembly set of the present invention;
Fig. 3 keeps off the cutaway view of assembly set along the E-E line according to main air according to the present invention among Fig. 2;
Fig. 4 keeps off the cutaway view of assembly set along the F-F line according to main air according to the present invention among Fig. 2;
Fig. 5 keeps off the cutaway view of assembly set along the G-G line according to main air according to the present invention among Fig. 2;
Fig. 6 keeps off the cutaway view of assembly set along the H-H line according to main air according to the present invention among Fig. 2.
Description of reference numerals
1-windscreen 2-pressing plate 3-skylight skeleton 4-attaching parts 5-strengthens the interior edge strip of top 7-of backing plate 6-skylight skeleton
The specific embodiment
Below in conjunction with embodiment the present invention is described in further detail.
Fig. 1 is according to the scheme drawing of main air retaining assembly set of the present invention and adjacent component installation, and wherein, what Reference numeral 1 was represented is windshield, is furnished with near the zone of skylight skeleton 3 and strengthens backing plate 5.Being connected of the top 6 of skylight skeleton 1 and adjacent structure disperses to cross, and existing aircraft is that each skeleton all points to a point (a little zone), and is intersected in a plurality of points according to skylight of the present invention skeleton, promptly disperses to cross.Skeleton each cross-sectional plane in skylight all has the interior edge strip 7 (seeing Fig. 3-6) of broad.
Fig. 2 shows the scheme drawing according to main air retaining assembly set of the present invention, and Fig. 3,4,5,6 shows respectively among Fig. 2 and keeps off the cutaway view of assembly set along E-E line, F-F line, G-G line and H-H line according to main air according to the present invention.In these figure, main air retaining assembly set comprises windscreen 1, pressing plate 2, skylight skeleton 3 and attaching parts 4, and wherein windscreen 1 is fixed between pressing plate 2 and the skylight skeleton 3 by attaching parts 4, and the curved-surface structure form of windscreen is not shown in the drawings.
Below be the concrete installation steps of main air retaining assembly set:
1, fill up the gap of skylight skeleton 3 with aquaseal, and smoothing is so that the sealing of main air retaining has the surface of continuous formation;
2, check that skylight skeleton 3 supports the surface of windshields 1: press the process in the ZPS02700-01200 technological specification, the service test anchor clamps check that skylight skeleton 3 supports the surface of windshields 1, make its on request with theoretical profile 35 ± 0.15mm apart;
3, windscreen 1 preceding the inspection is installed: check between the skylight skeleton 3 whether the space is arranged,, then fill up these spaces fully with aquaseal ZMS2427 (for example producing) by PRC-Desoto.Inc. by the ZPS02590-00200 technological specification if having;
4, main air retaining glass location is adjusted outside the windshield and the gap on skylight skeleton 3 surfaces, remains in 1.5～3mm scope, makes main air retaining glass 1 be placed in reposefully on the attachment face of skylight skeleton 3;
5, main air block pressuring plate assembly is installed;
1), coating release agent (ZPM3494, #MS-122VDAVID H.SUTHERLAND ﹠amp on the binding face of pressing plate 2 and main air retaining glass 1; CO., INC produces), then pressing plate 2 is put on the main air retaining glass 1.
2), with the screw-down torque value all bolts are installed in a certain order.
3), tight a bolt after, check installation situation from the inside, determining whether bolt is screwed to the end, and guarantee that the length of thread that bolt protrudes plate nut meets ZPS03670-00000 technological specification related request fully.
6, the back is installed and checks, install main air block pressuring plate assembly after, whether the sealing member (not shown) of at first observing between windscreen edge and the skylight skeleton compacted fully.If sealing member can not be crowded with the gap fully, then press the ZPS02590-00200 technological specification with aquaseal ZMS2427 filling, it is gapped to use aquaseal ZMS2427 to fill up institute between each pressing plate, between windscreen sealing band and the pressing plate fully by the ZPS02590-00200 technological specification then.
Should be understood that embodiments of the invention just are used to illustrate the present invention rather than restriction the present invention, the details that the invention is not restricted to describe herein.As long as in connotation scope of the present invention, all will drop in claims scope of the present invention variation, the modification of the above embodiment.
Claims (8)
1. a main air retaining assembly set comprises windscreen, pressing plate, skylight skeleton and attaching parts, and wherein, windscreen is fixed between pressing plate and the skylight skeleton by attaching parts, it is characterized in that, described windscreen is a curve form.
2. main air retaining assembly set as claimed in claim 1 is characterized in that described windscreen is the single-curvature surface shape.
3. main air retaining assembly set as claimed in claim 1 or 2 is characterized in that each cross-sectional plane of described skylight skeleton has interior edge strip, the moment of flexure when hitting to bear bird.
4. the described main air of one of claim keeps off assembly set as described above, it is characterized in that, described skylight skeleton disperses to cross with the employing that is connected of the adjacent structure of windscreen assembly set.
5. the described main air of one of claim keeps off assembly set as described above, it is characterized in that, has arranged that in the zone of described skylight skeleton a plurality of reinforcement backing plates are connected with surrounding covering.
6. the described main air of one of claim keeps off assembly set as described above, it is characterized in that, described windscreen assembly set adopts magnetic material.
7. main air keeps off the installation method of assembly set, and described main air retaining assembly set comprises windscreen, pressing plate, skylight skeleton and attaching parts, and this method comprises the steps:
(1) fill up the gap of skylight skeleton with aquaseal, thereby and smoothing be the sealing surfaces that the windscreen of curve form forms continuous formation;
(2) press technological specification, the service test anchor clamps check that the skylight skeleton supports the surface of windscreen;
(3) the preceding inspection of windscreen is installed, checks between the skeleton structure of skylight whether the space is arranged,, then fill up these spaces with aquaseal by technological specification if having;
(4) windscreen location is adjusted outside the windscreen and the gap on skeleton surface, skylight, makes windscreen be placed in reposefully on the attachment face of skeleton;
(5) main air block pressuring plate assembly is installed;
(6) back being installed checks, after installing main air retaining assembly set, check whether the sealing member between windscreen edge and the skylight skeleton is compacted fully, if sealing member can not be crowded with the gap fully, then use the aquaseal filling, it is gapped to use aquaseal to fill up institute between each pressing plate, between windscreen sealing member and the pressing plate then.
8. the installation method of main air retaining assembly set as claimed in claim 7 is characterized in that, the step that main air block pressuring plate assembly is installed comprises:
(1) coating release agent on the binding face of pressing plate and windscreen is put into pressing plate on the windscreen then;
(2) with the screw-down torque value all bolts are installed in a certain order;
(3) tight a bolt after, check installation situation from the inside, determining whether bolt is screwed to the position, and guarantee that the length of thread that bolt protrudes plate nut meets the requirements fully.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010168430.6A CN102233949B (en) | 2010-05-06 | 2010-05-06 | Main windshield assembly and method of installing same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010168430.6A CN102233949B (en) | 2010-05-06 | 2010-05-06 | Main windshield assembly and method of installing same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102233949A true CN102233949A (en) | 2011-11-09 |
| CN102233949B CN102233949B (en) | 2014-05-21 |
Family
ID=44885164
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201010168430.6A Active CN102233949B (en) | 2010-05-06 | 2010-05-06 | Main windshield assembly and method of installing same |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102233949B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104816838A (en) * | 2015-05-07 | 2015-08-05 | 哈尔滨飞机工业集团有限责任公司 | Installing method for preventing helicopter glass from leakage of rain |
| CN105386547A (en) * | 2012-08-28 | 2016-03-09 | 一禾科技发展（上海）有限公司 | Compressing assembly for fastening system |
| CN106882357A (en) * | 2015-12-15 | 2017-06-23 | 空中客车运营简化股份公司 | Windshield with support bar |
| CN111731504A (en) * | 2020-06-12 | 2020-10-02 | 陕西飞机工业（集团）有限公司 | Positioning method of cockpit glass framework |
| CN112758300A (en) * | 2021-01-21 | 2021-05-07 | 中电科芜湖钻石飞机制造有限公司 | Installation positioning device and method for aircraft sun visor |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3382630A (en) * | 1965-01-06 | 1968-05-14 | British Aircraft Corp Ltd | Mountings for aircraft windscreens |
| US3953630A (en) * | 1972-03-13 | 1976-04-27 | Triplex Safety Glass Company Limited | Laminated transparent assemblies |
| US20030062450A1 (en) * | 2001-10-02 | 2003-04-03 | Francis Dazet | Aircraft windshield attachment device |
| CN2898990Y (en) * | 2006-04-28 | 2007-05-09 | 江西洪都航空工业集团有限责任公司 | Cloth curtain type aircraft dark cabin flight cover |
| CN101473143A (en) * | 2006-03-31 | 2009-07-01 | 法国空中巴士公司 | Nut for securing an aircraft windscreen and device for securing an aircraft windscreen incorporating the said nut |
| US20100020381A1 (en) * | 2006-12-15 | 2010-01-28 | Saint-Gobain Glass France | Functionalized glazing |
-
2010
- 2010-05-06 CN CN201010168430.6A patent/CN102233949B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3382630A (en) * | 1965-01-06 | 1968-05-14 | British Aircraft Corp Ltd | Mountings for aircraft windscreens |
| US3953630A (en) * | 1972-03-13 | 1976-04-27 | Triplex Safety Glass Company Limited | Laminated transparent assemblies |
| US20030062450A1 (en) * | 2001-10-02 | 2003-04-03 | Francis Dazet | Aircraft windshield attachment device |
| CN101473143A (en) * | 2006-03-31 | 2009-07-01 | 法国空中巴士公司 | Nut for securing an aircraft windscreen and device for securing an aircraft windscreen incorporating the said nut |
| CN2898990Y (en) * | 2006-04-28 | 2007-05-09 | 江西洪都航空工业集团有限责任公司 | Cloth curtain type aircraft dark cabin flight cover |
| US20100020381A1 (en) * | 2006-12-15 | 2010-01-28 | Saint-Gobain Glass France | Functionalized glazing |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105386547A (en) * | 2012-08-28 | 2016-03-09 | 一禾科技发展（上海）有限公司 | Compressing assembly for fastening system |
| CN104816838A (en) * | 2015-05-07 | 2015-08-05 | 哈尔滨飞机工业集团有限责任公司 | Installing method for preventing helicopter glass from leakage of rain |
| CN106882357A (en) * | 2015-12-15 | 2017-06-23 | 空中客车运营简化股份公司 | Windshield with support bar |
| CN106882357B (en) * | 2015-12-15 | 2022-03-29 | 空中客车运营简化股份公司 | Windshield with support rod |
| CN111731504A (en) * | 2020-06-12 | 2020-10-02 | 陕西飞机工业（集团）有限公司 | Positioning method of cockpit glass framework |
| CN112758300A (en) * | 2021-01-21 | 2021-05-07 | 中电科芜湖钻石飞机制造有限公司 | Installation positioning device and method for aircraft sun visor |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102233949B (en) | 2014-05-21 |
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