CN204587308U - Aircraft seeding mounting apparatus - Google Patents
Aircraft seeding mounting apparatus Download PDFInfo
- Publication number
- CN204587308U CN204587308U CN201520204636.8U CN201520204636U CN204587308U CN 204587308 U CN204587308 U CN 204587308U CN 201520204636 U CN201520204636 U CN 201520204636U CN 204587308 U CN204587308 U CN 204587308U
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- Prior art keywords
- clip
- bearing plate
- stay bearing
- aircraft
- mounting apparatus
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Abstract
The utility model relates to aircraft seeding mounting apparatus, comprise the stay bearing plate be arranged on aircraft, described stay bearing plate is at least set to two, described stay bearing plate is set up in parallel, stay bearing plate is symmetrical arranged two rafter bars, described rafter bar, in " ┗ " shape, rafter bar is at least provided with two bracket assemblies, support frame as described above assembly comprises bracing frame main body and is arranged at the first clip in bracing frame main body, and the first clip is provided with the second clip matched with it.Superior effect of the present utility model is: rational in infrastructure, firmly light and handy, under the prerequisite meeting operating load, at utmost reduce erection weight, effectively prevent Aircraft Load excessively increases.
Description
Technical field
The utility model relates to aircraft seeding equipment field engineering field, is specifically related to a kind of aircraft seeding mounting apparatus for rainmaking.
Background technology
Aircraft seeding equipment has been used for aircraft artificial precipitation enhancement operation, the erecting device that current aircraft seeding equipment manufacturer provides only is installed for ground, aircraft seeding equipment cannot be installed on aircraft, and the erecting device many employings box structure on aircraft, not only bad for the dynamic handling stability energy of aircraft, and weight is large.
Publication number is that the Chinese patent of CN2585813Y discloses the built-in spreading gear of a kind of Medium Helicopter, combined by dispenser and hopper, dispenser is contained on helicopter belly outer wall, hopper is contained in cabin, by the floor opening in cabin, seed inlet and the hopper of dispenser go out kind of a mouth and dock and connect firmly integral; Opening part is hung outside engine room floor central authorities, install additional and broadcast sowing platform, in this platform and cabin, floor slide rail is to connecting firmly, platform is provided with relative with hanging opening outside floor, the convenient opening installing hopper, hopper goes out kind of mouth and docks with platform seed inlet, dispenser seed inlet docks by up going out kind of a mouth through platform seed inlet with hopper under fuselage, and is connected with the lug of dispenser front portion by the screw rod of platform openings surrounding.The hopper of this spreading gear dispenser is arranged in cabin the space occupying cabin, and seed inlet and hopper go out kind of a mouth docks and connect firmly integral, installing/dismounting inconvenience, poor practicability.
Publication number is that the Chinese patent of CN1586993A discloses weather modification miniature robot aircraft, comprise fuselage, wing, power driven and control system, at belly, parachute storehouse is set, fix one before parachute storehouse and broadcast sowing frame, broadcast sowing frame to be made up of the snap ring at horizontal aluminium sheet and aluminium sheet two ends, snap ring lock ring in the stage casing of cylindrical shape catalytic system, the built-in transceiver cabin, wing root portion of left and right, wing outer end is built-in airborne sonde, and the wing tip portion of wing is provided with night flight lamp.The frame that broadcasts sowing of this robot airplane is fixed by means of only horizontal aluminium sheet and parachute storehouse, its poor rigidity, frangibility during flight.
Utility model content
The purpose of this utility model is to overcome deficiency of the prior art, provides a kind of rational in infrastructure, firmly light and handy aircraft seeding mounting apparatus.
The utility model is achieved through the following technical solutions:
Aircraft seeding mounting apparatus, comprise the stay bearing plate be arranged on aircraft, described stay bearing plate is at least set to two, described stay bearing plate is set up in parallel, stay bearing plate is symmetrical arranged two rafter bars, described rafter bar, in " ┗ " shape, rafter bar is at least provided with two bracket assemblies, support frame as described above assembly comprises bracing frame main body and is arranged at the first clip in bracing frame main body, and the first clip is provided with the second clip matched with it.
Described technical scheme is preferably, and support frame as described above main body is by welding manner and the first anulated connection.
Described technical scheme is preferably, and described stay bearing plate, rafter bar, bracing frame main body are connected by fix screw.
Described technical scheme is preferably, and described first clip and the second clip are bolted.
Described technical scheme is preferably, and described first clip and the second clip are semicircle shape.
Described technical scheme is preferably, and described first clip and the second clip are ∨ shape.
Described technical scheme is preferably, and the upper surface of described stay bearing plate is arranged with the hold down groove for limiting rafter bar position.
Described technical scheme is preferably, and described stay bearing plate is vertical with rafter bar to be arranged.
Described technical scheme is preferably, and support frame as described above assembly is vertical with rafter bar to be arranged.
Described technical scheme is preferably, and described stay bearing plate and bracket assembly are all set to two.
Compared with prior art, superior effect of the present utility model is: rational in infrastructure, firmly light and handy, under the prerequisite meeting operating load, at utmost reduce erection weight, effectively prevent Aircraft Load excessively increases.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model aircraft seeding mounting apparatus;
Fig. 2 is the structural representation of stay bearing plate described in Fig. 1;
Fig. 3 is the structural representation of rafter bar described in Fig. 1;
Fig. 4 is the structural representation of Fig. 1 support frame as described above assembly;
Fig. 5 is the structural representation of the second clip described in Fig. 1.
Accompanying drawing mark is as follows:
1-stay bearing plate, 11-hold down groove, 2-rafter bar, 3-bracket assembly, 31-bracing frame main body, 32-first clip, 4-second clip.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model detailed description of the invention is described in further detail.
Embodiment 1
As shown in accompanying drawing 1-5, aircraft seeding mounting apparatus described in the utility model, comprises the stay bearing plate 1 be arranged on aircraft (not shown), and described stay bearing plate 1 is set to two, described stay bearing plate 1 is set up in parallel, and described stay bearing plate 1 is symmetrical arranged two rafter bars 2.Described rafter bar 2 is in " ┗ " shape, and rafter bar 2 is provided with two bracket assemblies 3, and support frame as described above assembly 3 comprises bracing frame main body 31 and the first clip 32, first clip 32 be arranged in bracing frame main body 31 is provided with the second clip 4 matched with it.
Support frame as described above main body 31 is connected with the first clip 32 by welding manner, improves the stability of stay bearing plate assembly 3; Described stay bearing plate 1, rafter bar 2, bracing frame main body 31 are connected by fix screw; Described first clip 32 and the second clip 4 are bolted, and make described aircraft broadcast sowing mounting apparatus convenient and swift when installing and dismantle.
Described first clip 32 and the second clip 4 are in semicircle shape, and described first clip 32 and the second clip 4 broadcast sowing equipment for fastening aircraft, and prevent aircraft from broadcasting sowing equipment and loosen, the equipment that broadcasts sowing is as rain maker.
The upper surface of described stay bearing plate 1 is arranged with the hold down groove 11 for limiting rafter bar 2 position, and the design of described hold down groove 11 further defines the degree of freedom of rafter bar 2 at the length direction of stay bearing plate 1, improves the stability of stay bearing plate 1 and rafter bar 2.
Described stay bearing plate 1 is vertical with rafter bar 2 to be arranged and support frame as described above assembly 3 is vertical with rafter bar 2 arranges, rational in infrastructure, safe and reliable, make aircraft described in the utility model broadcast sowing mounting apparatus and at utmost reduce erection weight under the prerequisite meeting operating load, effectively prevent Aircraft Load excessively increases.
Embodiment 2
The utility model provides another embodiment 2, is with the distinguishing characteristics of embodiment 1, and described first clip 32 and the second clip 4 are in ∨ shape; Determine the shape of described first clip 32 and the second clip 4 when practical operation according to actual conditions, improve its stability.
The utility model is not limited to above-mentioned embodiment, and when not deviating from flesh and blood of the present utility model, any distortion that it may occur to persons skilled in the art that, improvement, replacement all fall into scope of the present utility model.
Claims (10)
1. aircraft seeding mounting apparatus, it is characterized in that, comprise the stay bearing plate be arranged on aircraft, described stay bearing plate is at least set to two, and described stay bearing plate is set up in parallel, and stay bearing plate is symmetrical arranged two rafter bars, described rafter bar is in " ┗ " shape, rafter bar is at least provided with two bracket assemblies, support frame as described above assembly comprises bracing frame main body and is arranged at the first clip in bracing frame main body, and the first clip is provided with the second clip matched with it.
2. aircraft seeding mounting apparatus according to claim 1, is characterized in that, support frame as described above main body is by welding manner and the first anulated connection.
3. aircraft seeding mounting apparatus according to claim 1, is characterized in that, described stay bearing plate, rafter bar, bracing frame main body are connected by fix screw.
4. aircraft seeding mounting apparatus according to claim 1, is characterized in that, described first clip and the second clip are bolted.
5. the aircraft seeding mounting apparatus according to claim 1 or 4, is characterized in that, described first clip and the second clip are semicircle shape.
6. the aircraft seeding mounting apparatus according to claim 1 or 4, is characterized in that, described first clip and the second clip are ∨ shape.
7. the aircraft seeding mounting apparatus according to claim 1 or 3, is characterized in that, the upper surface of described stay bearing plate is arranged with the hold down groove for limiting rafter bar position.
8. the aircraft seeding mounting apparatus according to claim 1 or 3, is characterized in that, described stay bearing plate is vertical with rafter bar to be arranged.
9. aircraft seeding mounting apparatus according to claim 1, is characterized in that, support frame as described above assembly is vertical with rafter bar to be arranged.
10. aircraft seeding mounting apparatus according to claim 1, is characterized in that, described stay bearing plate and bracket assembly are all set to two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520204636.8U CN204587308U (en) | 2015-04-07 | 2015-04-07 | Aircraft seeding mounting apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520204636.8U CN204587308U (en) | 2015-04-07 | 2015-04-07 | Aircraft seeding mounting apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204587308U true CN204587308U (en) | 2015-08-26 |
Family
ID=53923489
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520204636.8U Active CN204587308U (en) | 2015-04-07 | 2015-04-07 | Aircraft seeding mounting apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204587308U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106800092A (en) * | 2017-03-30 | 2017-06-06 | 广州宏诚通用飞机维修服务有限公司 | Helicopter spray appliance attachment means |
| CN111288275A (en) * | 2018-12-07 | 2020-06-16 | 中航贵州飞机有限责任公司 | Adjustable aircraft task equipment stores pylon |
-
2015
- 2015-04-07 CN CN201520204636.8U patent/CN204587308U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106800092A (en) * | 2017-03-30 | 2017-06-06 | 广州宏诚通用飞机维修服务有限公司 | Helicopter spray appliance attachment means |
| CN111288275A (en) * | 2018-12-07 | 2020-06-16 | 中航贵州飞机有限责任公司 | Adjustable aircraft task equipment stores pylon |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |