CN201842259U - Quick integrated type heliport for emergency rescue - Google Patents
Quick integrated type heliport for emergency rescue Download PDFInfo
- Publication number
- CN201842259U CN201842259U CN2010205932777U CN201020593277U CN201842259U CN 201842259 U CN201842259 U CN 201842259U CN 2010205932777 U CN2010205932777 U CN 2010205932777U CN 201020593277 U CN201020593277 U CN 201020593277U CN 201842259 U CN201842259 U CN 201842259U
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- heliport
- emergency management
- pod apertures
- circuit board
- integration formula
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Abstract
The utility model discloses a quick integrated type heliport for emergency rescue, which is composed of a plurality of integrated plates assembled via quick connectors. Each integrated plate includes an upper panel, a lower panel and a core, the upper panel and the lower panel are respectively provided with an antistatic steel mesh in a laid manner, a plurality of guide holes having same structures and perpendicular to the integrated plate are embedded on the periphery of the integrated plate, cross through connecting holes are arranged on the periphery of the integrated plate corresponding to the guide holes, the cross through connecting holes are communicated with the guide holes correspondingly, and central reinforcing holes and auxiliary reinforcing holes are embedded into the integrated plate, while the auxiliary reinforcing holes are arranged outside the central reinforcing holes. The quick integrated type heliport has the advantages of simple integrated plate structure, reliable performance, quickness in assembly operation and reusability, and can meet requirements of landing, taking off, supplies parking, personnel loading and transfer and the like in case of emergency rescue and disaster relief for a helicopter with many fights and helicopter groups under field complex environments and difficult terrains during large-scale disaster relief and rescue operation.
Description
Technical field
The utility model relates to a kind of aviation field helicopter ground launching and recovering equipment, especially relates to a kind of fast integration formula heliport that is used for the emergency management and rescue purposes.
Background technology
Helicopter is applied to emergency management and rescue, have fast, efficient, be subjected to many advantages such as the geographical space restriction is few, can arrive the operation field that water, land route can not be led to fast, implementing a job such as searching rescue, goods and materials transport, airborne control operation, is the actv. emergency management and rescue means that many in the world countries generally adopt.
In recent years, China mainly focuses on the construction on civil airport construction or fixed type landing level ground, large-scale roof, and still, along with the frequent generation of various natural disaster disasters, urgent accident, helicopter participates in the more importance attached of emergency relief.Owing to limited by the complex situations of helicopter in hover technical merit, topographic condition and emergency relief place environment, helicopter has certain requirement to helicopter landing site when participating in rescue landing, and because condition restriction, often be difficult to search out at short notice suitable landing site, also very difficult building up rapidly is fit to open-air heliport extensive, the landing of many sorties helicopter, owing to there is this very serious problem during helicopter emergency relief at present, the effect of helicopter when participating in the emergency relief action caused very low efficient.
The patent No. is that the utility model patent of ZL200920106819.0 discloses a kind of helicopter combination moving type landing level ground, comprises mainly that cell block is assembled mutually by high strength bolt and cross terminal pad to be formed by connecting.Cell block has used high strength alumin ium alloy to be panel, and the suprduralumin honeycomb is an inner core, and the outside is coated by superduralumin section bar frame all around.Helicopter combination moving type landing level ground with said structure, any multinomial modes such as T shape, stack, solid of can carrying out are spliced into various landings level ground and are extended to interim urgent landing field, can satisfy the demand of the urgent landing of helicopter under rough topography.Terminal pad bolted connection speed is slow, the cell block material weight lays particular stress on, surface evenness is poor slightly, helicopter can not be slided the defective of running landing but exist simultaneously.
Summary of the invention
The purpose of this utility model overcomes deficiency of the prior art exactly, but provides that a kind of Fast Installation, structure are light firmly, dependable performance, planeness well also can slide the emergency management and rescue fast integration formula heliport that runs landing.
For solving the problems of the prior art, the utility model has adopted following technical scheme: it is assembled by quick connector by several circuit boards and forms, wherein, described circuit board comprises top panel, lower faceplate and be filled in described top panel and described lower faceplate between core, described top panel and described lower faceplate are laid with the electrostatic prevention steel mesh, it is identical and perpendicular to several pod apertures of described circuit board to be embedded with structure around the described circuit board, the position of corresponding pod apertures is provided with the logical heart connecting bore of criss-cross around the described circuit board, described criss-cross leads to the corresponding perforation with described pod apertures of heart connecting bore, described circuit board is embedded with center reinforced hole and auxiliary reinforced hole, and described auxiliary reinforced hole is positioned at the outside of center reinforced hole.
Further, described quick connector is provided with the anticreep self lock nut, is provided with spring shim in the described quick connector.
Further, described pod apertures is provided with quickly dismantled dust cover.
Further, the number of described pod apertures is 8.
Further, the number of described center reinforced hole is 3, and the number of described auxiliary reinforced hole is 18.
Further, described circuit board carries out parallel T shape and/or stack and/or three-dimensional mode by described pod apertures and described auxiliary reinforced hole and is connected.
Further, described center reinforced hole and described pod apertures are provided with the auxiliary telescopic supporting rod of wearing to its hole.
Further, be provided with the LED range light in described center reinforced hole and the described pod apertures.
Further, described emergency management and rescue fast integration formula heliport is provided with navigation landing sign.
The utility model emergency management and rescue fast integration formula heliport advantage is:
The utility model emergency management and rescue fast integration formula heliport, be repeatedly to take off for many helicopters, landing, park, maintenance, and the active platform of shipment noneffectives and relief goods, have dustproof, anti-falling into, anti-skidding, shockproof, multinomial comprehensive function such as positioning command, also have and to lay and to remove receipts fast, can singlely carry, helicopter-mounted hanging with car transported, multiple transportation mode such as shipping, circuit board has simple in structure, dependable performance, characteristics such as assembly operation fast, make many sorties helicopter can tackle landing under open-air complex environment and the rough topography simultaneously, take off and park goods and materials, problems such as personnel's loading and unloading transhipment, and can be repeatedly used.
Description of drawings
Fig. 1 is the front view of the circuit board of the utility model emergency management and rescue fast integration formula heliport.
Fig. 2 is the cutaway view of the circuit board of the utility model emergency management and rescue fast integration formula heliport.
Fig. 3 is the structural representation after the circuit board among Fig. 1 is installed LED range light and auxiliary telescopic supporting rod.
Fig. 4 is the utility model emergency management and rescue fast integration formula heliport plane connection structure scheme drawing.
Planar structure scheme drawing when Fig. 5 is used for many helicopter landings for the utility model emergency management and rescue fast integration formula heliport.
The specific embodiment
The utility model is described in more detail below in conjunction with accompanying drawing.
As shown in Figure 4, the utility model emergency management and rescue fast integration formula heliport is combined by quick connector 2 connections by several circuit boards 1.
In the present embodiment, described circuit board 1 is formed by epoxy resin equality of temperature one curing on the foamed core material preform.
As shown in Figure 2, circuit board 1 comprise top panel 11, lower faceplate 12 and be filled in top panel 11 and lower faceplate 12 between core 13.
As shown in Figure 1 and Figure 2, it is identical and perpendicular to 8 pod apertures 14 of circuit board 1 to be embedded with structure around the circuit board 1, the position of corresponding pod apertures 14 is provided with the logical heart connecting bore 15 of criss-cross around circuit board 1, logical heart connecting bore 15 of criss-cross and pod apertures 14 corresponding perforations, circuit board 1 is embedded with 3 center reinforced holes 16 and 18 auxiliary reinforced holes 17, and auxiliary reinforced hole 17 is positioned at the outside of center reinforced hole.
In the present embodiment, described top panel 11 and described lower faceplate 12 are laid with the electrostatic prevention steel mesh.Described core 13 adopts and strengthens the modified phenolic foam plate, use glass symmetry Z to strengthening the puncture sewing, top panel 11, lower faceplate 12 do not have the slit, interface owing to using equality of temperature to solidify respectively and between the core 13, avoid because of the weak cracking that comes unstuck that produces of core 13 and panel bonding interface performance, make circuit board 1 have higher loadintensity and tough, realized the material lightweight simultaneously.
In the present embodiment, in order to improve the stability and the bulk strength of the utility model emergency management and rescue fast integration formula heliport, what described quick connector 2 used is the quick connector that the anticreep self lock nut is set on it, is provided with spring shim in it, the vibration that is produced during landing on the landing field in the open air with the reply helicopter.
In the present embodiment, pod apertures 14 is made by composite material, is furnished with quickly dismantled dust cover, can snap to fast in the circuit board 1 when needs use, and quickly dismantled dust cover can be locked in use, can not come off after the distortion that is hit.Pod apertures 14 has the drain measure effect concurrently.
In the present embodiment, center reinforced hole 16 and auxiliary reinforced hole 17 are multi-functional connecting through hole, can strengthen the support strength and the cushioning ability of circuit board 1, circuit board 1 can also carry out parallel T shape with pod apertures 14 and/or multiple mode such as stack and/or solid is connected by auxiliary reinforced hole 17, form helicopter and hang the storehouse, can set up interim emergency management and rescue facilities such as the open-air hangar of interim helicopter, barracks, material depot, shallow water bridge, road panel, to satisfy each model helicopter at the needs of carrying out various different rescue tasks.
As shown in Figure 3, the center reinforced hole 16 of circuit board 1 and pod apertures 14 can be equipped with auxiliary telescopic supporting rod 3, can use in rough landform, also can assemble LED range light 4, to satisfy landing requirement under helicopter night and the low visibility meteorological conditions.
As shown in Figure 4, circuit board 1 uses quick connector 2 to assemble heliport mutually fast by the logical heart connecting bore 15 of pod apertures 14 pairing criss-crosss, and heliport is provided with navigation landing sign 5.
As shown in Figure 5, circuit board 1 and adaptor union 2 also can be combined into heliport unit 6 earlier according to mode shown in Figure 5, the heliport unit 6 of different directions is after laying interface channel 7, the composition scale is gone straight up to a group of planes, form the emergency management and rescue fast integration formula heliport that many sorties use, also can carry out polymorphic heliport according to different terrain.
The utility model emergency management and rescue fast integration formula heliport also is furnished with portable navigation command platform, portable weather prognosis system, aviation fuel supply vehicle and flight engineering maintenance equipment cart.
The utility model is not limited to above-mentioned embodiment, no matter do any variation on its shape or structure, everyly utilizes heliport that circuit board carries out Rapid Combination all within the utility model protection.
Claims (9)
1. emergency management and rescue fast integration formula heliport, assemble by quick connector by several circuit boards and to form, it is characterized in that, described circuit board comprises top panel, lower faceplate and be filled in described top panel and described lower faceplate between core, described top panel and described lower faceplate are laid with the electrostatic prevention steel mesh, it is identical and perpendicular to several pod apertures of described circuit board to be embedded with structure around the described circuit board, the position of corresponding pod apertures is provided with the logical heart connecting bore of criss-cross around the described circuit board, described criss-cross leads to the corresponding perforation with described pod apertures of heart connecting bore, described circuit board is embedded with center reinforced hole and auxiliary reinforced hole, and described auxiliary reinforced hole is positioned at the outside of described center reinforced hole.
2. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that described quick connector is provided with the anticreep self lock nut, is provided with spring shim in the described quick connector.
3. emergency management and rescue fast integration formula heliport according to claim 1 and 2 is characterized in that described pod apertures is provided with quickly dismantled dust cover.
4. emergency management and rescue fast integration formula heliport according to claim 3 is characterized in that the number of described pod apertures is 8.
5. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that the number of described center reinforced hole is 3, and the number of described auxiliary reinforced hole is 18.
6. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that, described circuit board carries out parallel T shape and/or stack and/or three-dimensional mode by described pod apertures and described auxiliary reinforced hole and is connected.
7. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that described center reinforced hole and described pod apertures are provided with the auxiliary telescopic supporting rod of wearing to its hole.
8. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that, is provided with the LED range light in described center reinforced hole and the described pod apertures.
9. emergency management and rescue fast integration formula heliport according to claim 1 is characterized in that, described emergency management and rescue fast integration formula heliport is provided with navigation landing sign.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010205932777U CN201842259U (en) | 2010-11-05 | 2010-11-05 | Quick integrated type heliport for emergency rescue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010205932777U CN201842259U (en) | 2010-11-05 | 2010-11-05 | Quick integrated type heliport for emergency rescue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201842259U true CN201842259U (en) | 2011-05-25 |
Family
ID=44037158
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010205932777U Expired - Fee Related CN201842259U (en) | 2010-11-05 | 2010-11-05 | Quick integrated type heliport for emergency rescue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201842259U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572802A (en) * | 2020-04-15 | 2020-08-25 | 武汉理工大学 | Emergency temporary helicopter airport light and shadow navigation system in alpine region and working method thereof |
-
2010
- 2010-11-05 CN CN2010205932777U patent/CN201842259U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572802A (en) * | 2020-04-15 | 2020-08-25 | 武汉理工大学 | Emergency temporary helicopter airport light and shadow navigation system in alpine region and working method thereof |
| CN111572802B (en) * | 2020-04-15 | 2022-11-08 | 武汉理工大学 | Emergency temporary helicopter airport light and shadow navigation system in alpine region and working method thereof |
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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 |
Granted publication date: 20110525 Termination date: 20191105 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |