CN203268315U - Protective device for airplane maintaining cockpit - Google Patents
Protective device for airplane maintaining cockpit Download PDFInfo
- Publication number
- CN203268315U CN203268315U CN2013201787689U CN201320178768U CN203268315U CN 203268315 U CN203268315 U CN 203268315U CN 2013201787689 U CN2013201787689 U CN 2013201787689U CN 201320178768 U CN201320178768 U CN 201320178768U CN 203268315 U CN203268315 U CN 203268315U
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- Prior art keywords
- cover plate
- driving compartment
- protecting equipment
- positive
- baffle plate
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Abstract
The utility model discloses a protective device for an airplane maintaining cockpit. The protective device comprises a cover plate, two side blocking plates, two supporting plates and a front blocking plate. The two side blocking plates are vertically connected with the two sides of the inner face of the cover plate. The two supporting plates are vertically connected on the inner face of the cover plate on the inner sides of the blocking plates. The heights of the supporting plates are smaller than the heights of the side blocking plates in the corresponding vertical direction. The front blocking plate is perpendicular to the side blocking plates and the cover plate and is connected with the same ends of the two side blocking plates to form a semi-encircling frame body with three sides. The protective device can effectively protect an instrument board.
Description
Technical field
The utility model relates to a kind of frock of the equipment such as driving compartment protection instrument when overhauling for aircraft.
Background technology
Aircraft revises greatly inspection and stops field interval, especially other fixed inspection of C inspection and higher level, and field time is longer owing to stopping, and when when driving compartment is worked, easily the Instrumentation and Control panel of driving compartment P8 plate is damaged, and causes unnecessary economic loss for company and client.
In recent years, those skilled in the art adopted various frocks with the protection instrument carrier panel, as driving compartment P8 plate when maintenance usually.Boeing-737 series aircraft driving compartment P8 plate has very important effect, not only should avoid the damage of macroscopic view, also should avoid dust, chip etc. to enter P8 plate gap.
The protection of P8 plate mainly is to provide cover protection in the past, and a little less than its protective capability is highly brittle, only can produces the barrier effect to foreign material such as dust, chips, can not produce effectively protection to the P8 plate.
Summary of the invention
In view of this, the utility model proposes a kind of special protecting equipment of aircraft maintenance driving compartment for the protection problem of current Boeing-737 series aircraft driving compartment P8 plate.
The utility model is by the following technical solutions:
A kind of aircraft maintenance driving compartment special protecting equipment comprises:
One cover plate;
Two side shields are vertically connected at cover plate inner face both sides;
Two stay bearing plates are vertically connected on the cover plate inner face of baffle plate inboard, and on corresponding vertical direction, the height of stay bearing plate is less than the height of side shield; And
Positive baffle plate, vertical with side shield and cover plate, and connect two side shields and construct the semi-surrounding framework with three frames with end.
According to said structure of the present utility model, cover plate and two side shields and bucket shape body of positive baffle plate formation, known, mostly be obliquely installed as the instrument carrier panel of P8 plate, rely on so gravity, the bucket shape body can cover on instrument carrier panel effectively.Simultaneously; form both sides according to said structure two side shields spacing, two stay bearing plates are just accurately located and are supported on the top surface edge of instrument carrier panel so, in the situation that instrument carrier panel is carried out effectively protection; fender guard depends on the edge of instrument carrier panel, and self can directly not contact instrument.Thereby, according to said structure, not only can carry out the set of fender guard by fast speed, and can effectively protect the instrument on instrument carrier panel.
Above-mentioned aircraft maintenance driving compartment special protecting equipment, the cover plate inner face of described positive baffle plate inboard is provided with one and stablizes bar.
Above-mentioned aircraft maintenance driving compartment special protecting equipment, described positive baffle plate has to get out of the way the groove that protected instrument carrier panel is positioned at the parts of positive baffle plate side.
Above-mentioned aircraft maintenance driving compartment special protecting equipment has inspection door on described positive baffle plate.
Above-mentioned aircraft maintenance driving compartment special protecting equipment, described inspection door is two, divides the both sides that occupy groove.
Above-mentioned aircraft maintenance driving compartment special protecting equipment also comprises the positive slope panel that is arranged on the outer human oriented side of described cover plate.
Above-mentioned aircraft maintenance driving compartment special protecting equipment mate described positive slope panel, also is provided with to have opposite domatic counter-slope panel positive and negative slope panel top joint.
It is 90 degree that above-mentioned aircraft maintenance driving compartment special protecting equipment, positive and negative slope panel top engage the drift angle that forms, and positive slope panel and cover plate angle are less than the angle of counter-slope panel and cover plate.
Above-mentioned aircraft maintenance driving compartment special protecting equipment, the cover plate side relative with positive baffle plate is provided with the auxiliary coverplate that extends to away from positive baffle plate direction.
Above-mentioned aircraft maintenance driving compartment special protecting equipment, auxiliary coverplate has one, and width connects on the cover board between two parties less than cover plate.
Description of drawings
Fig. 1 is the main TV structure schematic diagram according to a kind of aircraft maintenance driving compartment special protecting equipment of the utility model preferred embodiment.
Fig. 2 is the plan structure schematic diagram corresponding to Fig. 1.
Fig. 3 is the axle geodesic structure schematic diagram according to a kind of aircraft maintenance driving compartment special protecting equipment in the utility model preferred embodiment.
Fig. 4 is the axle geodesic structure schematic diagram of another direction.
In figure: 1, cover plate, 2, positive slope panel, 3, auxiliary coverplate, 4, stablize bar, 5, baffle plate just, 6, groove, 7, inspection door, 8, stay bearing plate, 9, side shield.
The specific embodiment
With reference to Figure of description 1, relational language once is described first:
For inner face and outside, based on the content that reaches described herein, it will be understood by those of skill in the art that for cover plate 1, protection face is inner face in the face of the face of capped article in other words, opposite face is the outside.
See positive baffle plate 5, take it as reference, the position of two side shield 9 correspondences shows as cover plate 1 side corresponding to both sides in positive baffle plate normal direction again.
As for the interior survey of side shield 9, for having as " bucket ", should be appreciated that " interior " should be able to be understood.
A kind of aircraft maintenance driving compartment special protecting equipment shown in structure as shown in Figures 1 to 4 comprises:
One cover plate 1 plays main covering effect;
Two side shields 2, as Fig. 1 the right and left, respectively there is one at cover plate 1 dual-side, is vertically connected at cover plate 1 inner face, namely on the protection face of cover plate 1, two side shield 2 spacings should be considered the width of instrument carrier panel such as P8 plate, thereby form the spacing of sway, under this structural condition, upper-lower position also should be spacing, prevent that cover plate 1 directly is pressed on instrument, thereby configure following stay bearing plate 8.
As shown in Fig. 1 the right and left, two stay bearing plates 8, be vertically connected on cover plate 1 inner face of baffle plate 2 inboards, and on this vertical direction, the length of stay bearing plate 8 is less than the length of side shield 9, form supporting bable tops, thereby form at described two side shields 2 support that the spacing situation lower supporting plate in left and right is formed on the instrument carrier panel edge, two side shields 2 also play the effect that forms the location to supporting simultaneously.
In above structure, in conjunction with above, instrument carrier panel is obliquely installed mostly; rely on gravity; according to said structure, fender guard has the trend of downward operation, for this reason; configure positive baffle plate 5; be used for providing downward operation partical gravity counter-force, vertical with side shield 9 and cover plate 1, consist of three vertical planes; the whole bucket type structure that forms namely connects two side shields and constructs the semi-surrounding framework with three frames with end.
Said structure facilitates set, places to get final product, and it is also convenient to carry, and the structure of taking off is relatively compact, easy to carry.
In structure as shown in Figure 1, the cover plate inner face of described positive baffle plate 5 inboards is provided with a rectangular template, be expressed as and stablize bar 4, its two ends engage with the stay bearing plate 8 of both sides, form and support, guarantee the assembly reliability of stay bearing plate 8, the outside is connected with the inboard of positive baffle plate 5, strengthens the connection reliability of positive baffle plate.For stabilization, show as in the horizontal direction, the stable bar 4 with certain altitude can rely on some article on instrument carrier panel and contact, and improves fender guard stability in the horizontal direction.
For instrument carrier panel and equipment on every side thereof, inevitably various features can appear, the coupling correlated characteristic, preferably the relevant correspondence structure of configuration, can not produce because of the existence of fender guard conflict.Side shield 9 for the left and right said conflict can not occur, as shown in Figure 1 in most cases; described positive baffle plate 5 has to get out of the way the groove 6 that protected instrument carrier panel is positioned at the parts of positive baffle plate side; thereby, when forming effective positioning action, the conflict that can not produce the squaring pusher side apparatus.Groove 6 shapes and size and distribute depends on that this side need to be got out of the way the position of the equipment of avoiding in other words, shape and size.
Should be appreciated that the setting for groove 6, should mate concrete application and select, but not imperative, after all protected instrument carrier panel around may not have the equipment that need to be avoided, therefore, it has the advantages that to arise at the historic moment.
Preferably, have inspection door 7 on described positive baffle plate 5, by inspection door, whether the maintainer can lead to the range estimation fender guard and be in place, with the positional accuracy that guarantees that fender guard is placed.
Further, as Fig. 1 and 4, described inspection door 7 is two, minute occupy the both sides of groove 6, more is close to the position of side shield, the position of more close stay bearing plate 8 in other words, the accuracy that can better observe placement location.
As shown in Figures 1 to 4; also comprise the positive slope panel 2 that is arranged on the outer human oriented side of described cover plate 1; the existence of positive slope panel 2 makes fender guard have larger gradient; the related personnel is usually when seeing such structure; above can not being sitting in; above also can not being placed on weight, thereby can prevent as damaging because personnel's mistake is sat the instrument that causes.
On the other hand, the space between positive slope panel 2 and cover plate can prevent some simple utensils, uses during convenient for maintaining.
In above-mentioned structure, positive slope panel is vertical with positive baffle plate, and acutangulates with cover plate, and this structure configuration mode makes the space between positive slope panel 2 and cover plate 1 can prevent some simple utensils because of the relation of installation site.These simple utensils are not enough to affect the protective effect of cover plate.
In some applications, preferably to Shaozheng slope panel 2, alert layer being set, such as coating bright yellow color, the personnel that can more effectively prevent sit back and wait problem by mistake.
In structure as shown in Figure 1, mate described positive slope panel, also be provided with and have opposite domatic counter-slope panel, positive and negative slope panel top engages.This structure all can have under various application conditions two domatic, all can produce warning function on which direction.On the other hand, two domatic combinations can improve the intensity of mounting structure, better reliability effectively.In such structure, also can form must container cavity, can place some small articles.
Preferably, it is 90 degree that positive and negative slope panel top engages the drift angle that forms, and aesthetic property is relatively good, and positive slope panel and cover plate angle are less than the angle of counter-slope panel and cover plate.Can effectively distinguish pros and cons, can determine mounting means by fast speed in use.
In some applications; mate claimed equipment; the cover plate side relative with positive baffle plate is provided with the auxiliary coverplate 3 that extends to away from positive baffle plate direction; this structure has under the condition of reasonable support and positioning action at cover plate 1; the configuration of auxiliary coverplate 3 will be simplified relatively; in theory, can form in the situation of larger area protection, integral structure can be compact.
Further, auxiliary coverplate 3 has one, and width is mainly used in the miniature instrument plate on supplementary protection central instrument panel side less than cover plate 1, is connected between two parties on cover plate 1, makes as much as possible the center of gravity of fender guard placed in the middle, improves stability.
Claims (10)
1. an aircraft maintenance driving compartment special protecting equipment, is characterized in that, comprising:
One cover plate (1);
Two side shields (2) are vertically connected at cover plate (1) inner face both sides;
Two stay bearing plates (8) be vertically connected on the inboard cover plate inner face of baffle plate (2), and on corresponding vertical direction, the height of stay bearing plate (8) are less than the height of side shield (2); And
Positive baffle plate (5), vertical with side shield and cover plate, and connect two side shields and construct the semi-surrounding framework with three frames with end.
2. aircraft maintenance driving compartment special protecting equipment according to claim 1, is characterized in that, the inboard cover plate inner face of described positive baffle plate (5) is provided with one and stablizes bar (4).
3. aircraft maintenance driving compartment special protecting equipment according to claim 1 and 2, is characterized in that, described positive baffle plate (5) has to get out of the way the groove (6) that protected instrument carrier panel is positioned at the parts of positive baffle plate side.
4. aircraft maintenance driving compartment special protecting equipment according to claim 1 and 2, is characterized in that, has inspection door (7) on described positive baffle plate (5).
5. aircraft maintenance driving compartment special protecting equipment according to claim 4, is characterized in that, described inspection door (7) is two, divides the both sides that occupy groove (6).
6. aircraft maintenance driving compartment special protecting equipment according to claim 1, is characterized in that, also comprises the positive slope panel that is arranged on the outer human oriented side of described cover plate (1).
7. aircraft according to claim 6 maintenance driving compartment special protecting equipment, is characterized in that, mate described positive slope panel, also is provided with to have opposite domatic counter-slope panel positive and negative slope panel top joint.
8. aircraft according to claim 7 maintenance driving compartment special protecting equipment, is characterized in that, it is 90 degree that positive and negative slope panel top engages the drift angle that forms, and positive slope panel and cover plate angle are less than the angle of counter-slope panel and cover plate.
9. aircraft maintenance driving compartment special protecting equipment according to claim 1, is characterized in that, the cover plate side relative with positive baffle plate is provided with the auxiliary coverplate (3) that extends to away from positive baffle plate direction.
10. aircraft maintenance driving compartment special protecting equipment according to claim 9, is characterized in that, auxiliary coverplate (3) has one, and width is connected on cover plate (1) between two parties less than cover plate (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013201787689U CN203268315U (en) | 2013-04-11 | 2013-04-11 | Protective device for airplane maintaining cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013201787689U CN203268315U (en) | 2013-04-11 | 2013-04-11 | Protective device for airplane maintaining cockpit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203268315U true CN203268315U (en) | 2013-11-06 |
Family
ID=49498773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013201787689U Expired - Fee Related CN203268315U (en) | 2013-04-11 | 2013-04-11 | Protective device for airplane maintaining cockpit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203268315U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103204250A (en) * | 2013-04-11 | 2013-07-17 | 山东太古飞机工程有限公司 | Protecting device special for airplane cockpit maintenance |
-
2013
- 2013-04-11 CN CN2013201787689U patent/CN203268315U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103204250A (en) * | 2013-04-11 | 2013-07-17 | 山东太古飞机工程有限公司 | Protecting device special for airplane cockpit maintenance |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131106 Termination date: 20160411 |