CN204548092U - One hovers formula air cushion vehicle entirely - Google Patents
One hovers formula air cushion vehicle entirely Download PDFInfo
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- CN204548092U CN204548092U CN201520191069.7U CN201520191069U CN204548092U CN 204548092 U CN204548092 U CN 204548092U CN 201520191069 U CN201520191069 U CN 201520191069U CN 204548092 U CN204548092 U CN 204548092U
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- capsule
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- seat
- air bag
- entirely
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Abstract
The utility model relates to one and entirely to hover formula air cushion vehicle, comprise hull and be connected to the skirt structure below hull, described skirt structure comprises air bag and capsule refers to, described air bag is wrapped in planking and forms airtight air bag chamber with planking, described capsule refers to be connected to bottom described air bag, airport is provided with bottom air bag, air bag chamber refers to be communicated with by airport and capsule, described capsule refers to the zonary structure for being referred to be connected to form by multiple monomer capsule, described monomer capsule refers to that both sides are provided with capsule and refer to seat and refer to that seat is connected with air bag by capsule, described capsule refers to that a side is connected to gasbag ektexine, one end that opposite side refers to monomer capsule is connected by attaching parts, capsule of the present utility model refers to refer to that seat connects by capsule, and capsule refers to that seat is connected for detouchable attaching parts between referring to capsule, and maintainability is strong, convenient disassembly, without the need to making entirely to hover, the rise of formula air cushion vehicle and replaceable capsule refer to, actv. extends the service life of skirt structure, reduces cost.
Description
Technical field
The utility model relates to ship domain, particularly relates to one and entirely to hover formula air cushion vehicle.
Background technology
The skirt structure of air cushion vehicle is the vitals of air cushion vehicle, and skirt structure determines that air cushion vehicle whether can steady safe navigation.The formula that entirely hovers air cushion vehicle can on ground, ice face, sandy beach, the navigation of the bearing surface such as marsh.Ideally, only air dielectric is there is between bearing surface and skirt of hovercraft structure, but during real navigation, due to the high-speed cruising of ship, there will be the phenomenon tilting and teetertotter, cause skirt structure to contact with the direct of bearing surface, the damage such as very easily cause apron bottom abrasion, scratch, therefore apron part needs frequent replacing, not only brings great economic attrition, and exchonge step is loaded down with trivial details, cause the waste of human cost and time cost.
Existing skirt of hovercraft structure is integral type, and each parts adopt to glued joint and connect, and namely capsule needs the replacing of overall skirt structure after referring to breakage, its maintainability is poor, and the service life of skirt structure is short, and use cost is high.
Utility model content
Capsule of the present utility model refers to refer to that seat connects by capsule, and capsule refers to that seat is connected for detouchable attaching parts between referring to capsule, and maintainability is strong, convenient disassembly, without the need to making entirely to hover, the rise of formula air cushion vehicle and replaceable capsule refer to, actv. extends the service life of skirt structure, reduces cost.
For reaching this object, the utility model by the following technical solutions:
The utility model provides one entirely to hover formula air cushion vehicle, comprise hull and be connected to the skirt structure below hull, described skirt structure comprises air bag and capsule refers to, described air bag is wrapped in planking and forms airtight air bag chamber with planking, described capsule refers to be connected to described capsule bottom described air bag and refers to the zonary structure for being referred to be connected to form by multiple monomer capsule, each described monomer capsule refers to inside all by airport and described air bag chamber, described monomer capsule refers to that both sides are provided with capsule and refer to seat and refer to that seat is connected with air bag by capsule, described capsule refers to that a side is connected to gasbag ektexine, one end that opposite side refers to monomer capsule is connected by attaching parts.
Further technical scheme is, described capsule refers to that seat comprises the first capsule and refers to that seat and the second capsule refer to seat, described first capsule refers to that seat is that triangle capsule refers to seat, described second capsule refers to that seat is that banded capsule refers to seat, described first capsule refers to seat offer the first through hole referring to one end for lateral connection monomer capsule, and described second capsule refers to that on seat, array is provided with the second through hole referring to the other end for longitudinally connecting monomer capsule.
Further technical scheme is, the shroud that described monomer capsule refers to comprise middle its central band and is arranged at middle its central band both sides, described in both sides, the described middle its central band of shroud parcel forms cavity, shroud described in both sides away from middle its central band position and the place of being interconnected is equipped with the first mounting hole, first mounting hole of the shroud that adjacent described monomer capsule refers to and the first through hole match, described middle its central band place is provided with the second mounting hole matched with the second through hole, refers to that bottom is provided with linear cuts at monomer capsule.
Further technical scheme is, described first capsule refers to that seat comprises two and to be symmetrical arranged and can the single page of folding, and described first through hole is positioned at the first capsule and refers on the dual-side of described single page of an opening part, and another side of single page described in both sides is bonded in gasbag ektexine; Described second through hole is arranged on the side that the second capsule refers to seat, and described second capsule refers to that the opposite side of seat is bonded in described gasbag ektexine.
Further technical scheme is, described first capsule refers to that seat is positioned near bottom plating side, and described second capsule refers to that seat is positioned at the first capsule and refers to outside seat.
Further technical scheme is, described attaching parts is nylon screw screw bolt and nut.
Further technical scheme is, described air bag dual-side is connected with planking by fixing press strip.
Further technical scheme is, described first capsule refers to that the dual-side of seat connection gasbag ektexine is provided with connecting band, and described first capsule refers to that seat is connected with air bag by connecting band.
Preferably, described second capsule refers to that seat and air bag glued joint or radio-frequency welding, and described connecting band and air bag glued joint or radio-frequency welding.
Preferably, described capsule refers to be made up of cotton synthetic fibre or polyurethane nylon or Hypalon material, and described air bag is made up of PVC material or elastomeric material.
The beneficial effects of the utility model are:
1, capsule of the present utility model refers to refer to that seat connects by capsule, and capsule refers to that seat is connected for detouchable attaching parts between referring to capsule, and maintainability is strong, convenient disassembly, without the need to making entirely to hover, the rise of formula air cushion vehicle and replaceable capsule refer to, actv. extends the service life of skirt structure, reduces cost.
2, air bag and capsule refer to adopt different materials, the capsule be positioned at bottom apron refers to adopt high wearable material as high-strength polyamide fibre or polyurethane nylon or wear-resisting Hypalon, air bag and gasbag seat adopt low, the lightweight PVC of cost or elastomeric material, decrease the cost of skirt structure, alleviate weight, the capsule of high-abrasive material refers to add its service life.
Accompanying drawing explanation
Fig. 1 is the front view of the formula that entirely the hovers air cushion vehicle that the utility model provides;
Fig. 2 is the birds-eye view of the formula that entirely the hovers air cushion vehicle that the utility model provides;
Fig. 3 is the section-drawing of A-A part in Fig. 2;
Fig. 4 is the annexation figure that the monomer capsule of the formula that entirely the hovers air cushion vehicle that the utility model provides refers to refer to capsule seat;
Fig. 5 is the structural representation that the first capsule of the formula that entirely the hovers air cushion vehicle that the utility model provides refers to seat;
Fig. 6 is the structural representation that the formula that entirely hovers air cushion vehicle monomer capsule that the utility model provides refers to;
Fig. 7 is the expansion drawing that the formula that entirely hovers air cushion vehicle monomer capsule that the utility model provides refers to;
Fig. 8 is the annexation figure that the formula that entirely hovers air cushion vehicle monomer capsule that the utility model provides refers to refer to the first capsule seat.
In figure:
1, air bag; 2, capsule refers to; 3, planking; 4, air bag chamber; 5, airport; 6, connecting band; 7, the first capsule refers to seat; 8, the second capsule refers to seat; 21, monomer capsule refers to; 71, the first through hole; 81, the second through hole; 211, the first mounting hole; 212, the second mounting hole; 213, middle its central band; 214, shroud.
Detailed description of the invention
The technical solution of the utility model is further illustrated by detailed description of the invention below in conjunction with accompanying drawing.
The utility model provides one entirely to hover formula air cushion vehicle, as shown in Figure 1-Figure 3, comprise hull and be connected to the skirt structure below hull, described skirt structure comprises air bag 1 and capsule refers to 2, described air bag 1 is wrapped in planking 3 and forms airtight air bag chamber 4 with planking 3, described capsule refers to that 2 are connected to bottom described air bag 1, and described capsule refers to that 1 for refer to 21 zonary structures be connected to form by multiple monomer capsule, and each described monomer capsule refers to that 21 are communicated with by airport 5 with described air bag chamber 4 for inner.The formula that entirely hovers air cushion vehicle is also known as full-floating air cushion vehicle, and be the formula air cushion vehicle that entirely hovers in the present embodiment, the lift fan work on ship, produces pressurized air, enter air bag chamber 4, then enter capsule via airport 5 and refer to 2 by air flue.Pressurized air refers to the bottom ejection of 21 by monomer capsule, compressed air is at a high speed by running surface-limited, just from top to bottom curvedly along table towards outer loss, thus form air curtain to maintain air cushion support hull in surrounding, and make hull all leave bearing surface.
As shown in Figure 3, described monomer capsule refers to that 21 both sides are provided with capsule and refer to seat and refer to that seat is connected with air bag 1 by capsule, and described capsule refers to that a side is connected to air bag 1 outer wall, and opposite side and monomer capsule refer to that one end of 21 is connected by attaching parts.Described attaching parts is nylon bolt and nut, be convenient to contact with bearing surface and the capsule easily worn and torn refer to 2 dismounting, maintainability is strong.When capsule refer to 2 be worn after, can realize repeatedly changing, without the need to making air cushion vehicle float during replacing, easy to operate.This structure design can extend the service life of air bag 1 by more than 10 years, avoids traditional overall skirt structure frequently to change problem.
Described capsule refer to 2 by high strength and wear-resisting cotton synthetic fibre or polyurethane nylon or Hypalon high-abrasive material make, described air bag 1 and capsule refer to that seat is low by cost and the PVC material that quality is light or elastomeric material are made.Described capsule refer to 2 and air bag 1 adopt different materials, and carry out material arrangements according to its different environment for use, not only increase the service life of skirt structure, and actv. decrease cost, alleviate quality.
For surface effect vehicle, skirt structure expense accounts for 20% of total price, and air bag 1 expense accounts for 12 ~ 15% of total price, and capsule refers to that 2 account for about 5 ~ 8% of total price.Change 1 time by annual, reduce expenses every year and account for 12% ~ 15% of total price.Air bag 1 life-span can reach 10 years, within 10 years, saves 1.2 ~ 1.5 times of total price expenses altogether.
As shown in Figure 6 and Figure 7, described monomer capsule refers to that 21 comprise middle its central band 213 and are arranged at the shroud 214 of middle its central band 213 both sides, and shroud 214 described in both sides wraps up described middle its central band 213 and forms cavity, and described middle its central band 213 and described shroud 214 are structure as a whole.Shroud 214 described in both sides away from middle its central band position and the place of being interconnected is equipped with the first mounting hole 211, described middle its central band 213 one end is provided with the second mounting hole 21.Described monomer capsule refers to that 21 deployed configurations are trapezoidal, and its trapezoidal minor face place arranges the second mounting hole 212, two base angle place and arranges the first mounting hole 211, and folding dual-side, can form curved cavity, and first mounting hole 211 at two places is corresponding.After folding forming, at monomer capsule, the two side that monomer capsule refers to 21 substantially structure triangular in shape refers to that bottom is provided with linear cuts, refer to that bottom is flowed out for air-flow from monomer capsule, the direction of arrow is as shown in Figure 3 the flow direction of air-flow.Skirt structure afterbody is set up and is prevented that bailing capsule refers to, to avoid making water resistance sharply increase because afterbody bails reason.
As shown in Figure 4 and Figure 5, described capsule refers to that seat comprises the first capsule and refers to that seat 7 and the second capsule refer to seat 8.Described first capsule refers to that seat 7 refers to seat for triangle capsule, and comprise two and to be symmetrical arranged and can the single page of folding, be positioned at the first capsule and refer to that the dual-side of the described single page of seat 7 opening part is provided with connecting band 6, described first capsule refers to that seat 7 is connected with air bag 1 outer wall by connecting band 6.Preferably, with described first capsule, described connecting band 6 refers to that seat 7 is one-body molded.Another side edge of described single page be provided with to refer to adjacent monomer capsule 21 the first through hole 71 of matching of the first mounting hole 211 of respective side shroud 214, described first capsule refers to that seat 7 refers to 21 lateral connection by the first through hole 71 with monomer capsule.Described first capsule refers to that the quantity of seat 7 and monomer capsule refer to that the quantity of 21 is identical; As shown in Figure 8, described first capsule refers to that seat 7 and monomer capsule refer to that 21 are staggeredly arranged.Two connected monomer capsules refer to that 21 have four shrouds 214, and wherein, with first capsule, adjacent two shrouds 214 refer to that seat is connected, and the monomer capsule that the shroud on both sides is adjacent respectively refers to by two other first capsule, the shroud 214 of 21 refers to that seat connects.Namely adjacent two described monomer capsules refer to by the first capsule, 21 one end arranging the first mounting hole 211 refer to that the single page of seat 7 closes up, and the first mounting hole 211-first through hole 71 that the first mounting hole 211-adjacent monomer capsule that described attaching parts refers to through the first through hole 71-monomer capsule successively refers to is to carry out the locking that monomer capsule refers to 21 one end.
Described second capsule refers to that seat 8 refers to seat for banded capsule, and its side is connected to air bag 1 outer wall, and opposite side array is provided with and refers to monomer capsule the second through hole 81 that 21 second mounting holes 212 match.Described second capsule refers to by the second through hole 81 and monomer capsule, seat 8 refers to that 21 are longitudinally connected.Described first capsule refers to that seat 7 is positioned at the inner side near bottom plating side namely near ship, and described second capsule refers to that seat 8 is positioned at the first capsule and refers to outside seat 7, i.e. the outside of ship.
Preferably, described air bag 1 dual-side realizes being connected with planking with the cooperation of thread-forming screw by fixing press strip, the preferred aluminum alloy materials of described fixation clip.
Preferably, described second capsule refers to that the connection mode of one end that seat 8 is connected with air bag 1 is for glued joint or radio-frequency welding, and the connection mode of described connecting band 6 and air bag 1 is for glued joint or radio-frequency welding.
Below know-why of the present utility model is described in conjunction with specific embodiments.These describe just in order to explain principle of the present utility model, and can not be interpreted as the restriction to the utility model protection domain by any way.Based on explanation herein, those skilled in the art does not need to pay performing creative labour can associate other detailed description of the invention of the present utility model, and these modes all will fall within protection domain of the present utility model.
Claims (10)
1. the formula air cushion vehicle that entirely hovers, it is characterized in that: comprise hull and be connected to the skirt structure below hull, described skirt structure comprises air bag (1) and capsule refers to (2), described air bag (1) is wrapped in planking (3) and forms airtight air bag chamber (4) with planking (3), described capsule refers to that (2) are connected to described air bag (1) bottom, described capsule refers to that (2) inside is connected with described air bag chamber (4) by airport (5), described capsule refers to that (2) are for refer to by multiple monomer capsule the zonary structure that (21) are connected to form, described monomer capsule refers to that (21) both sides are provided with capsule and refer to seat and refer to that seat is connected with air bag (1) by capsule, described capsule refers to that a side is connected to air bag (1) outer wall, opposite side refers to that with monomer capsule the one end of (21) is connected by attaching parts.
2. the formula air cushion vehicle that entirely hovers according to claim 1, it is characterized in that: described capsule refers to that seat comprises the first capsule and refers to that seat (7) and the second capsule refer to seat (8), described first capsule refers to that seat (7) refers to seat for triangle capsule, described second capsule refers to that seat (8) refers to seat for banded capsule, described first capsule refers to seat (7) offer the first through hole (71) referring to (21) one end for lateral connection monomer capsule, and described second capsule refers to that the upper array of seat (8) is provided with the second through hole (81) referring to (21) other end for longitudinally connecting monomer capsule.
3. the formula air cushion vehicle that entirely hovers according to claim 2, it is characterized in that: described monomer capsule refers to that (21) comprise middle its central band (213) and are arranged at the shroud (214) of middle its central band (213) both sides, shroud described in both sides (214) wraps up described middle its central band (213) and forms cavity, shroud described in both sides (214) away from middle its central band position and the place of being interconnected is equipped with the first mounting hole (211), adjacent described monomer capsule refers to that first mounting hole (211) of the shroud (214) of (21) and the first through hole (71) match, described middle its central band (213) place is provided with the second mounting hole (212) matched with the second through hole (81), refer to that bottom is provided with linear cuts at monomer capsule.
4. the formula air cushion vehicle that entirely hovers according to claim 3, it is characterized in that: described first capsule refers to that seat (7) comprises two and to be symmetrical arranged and can the single page of folding, described first through hole (71) is positioned at the first capsule and refers to that, on the dual-side of the described single page of seat (7) opening part, another side of single page described in both sides is bonded in air bag (1) outer wall; Described second through hole (81) is arranged on the side that the second capsule refers to seat (8), and described second capsule refers to that the opposite side of seat (8) is bonded in described air bag (1) outer wall.
5. the formula air cushion vehicle that entirely hovers according to claim 2, is characterized in that: described first capsule refers to that seat (7) is positioned near bottom plating side, and described second capsule refers to that seat (8) is positioned at the first capsule and refers to seat (7) outside.
6. the formula air cushion vehicle that entirely hovers according to claim 1, is characterized in that: described attaching parts is nylon bolt and nut.
7. the formula air cushion vehicle that entirely hovers according to claim 1, is characterized in that: described air bag (1) dual-side is connected with planking by fixing press strip.
8. the formula air cushion vehicle that entirely hovers according to claim 2, it is characterized in that: described first capsule refers to that the dual-side of seat (7) connection air bag (1) outer wall is provided with connecting band (6), and described first capsule refers to that seat (7) is connected with air bag (1) by connecting band (6).
9. the formula air cushion vehicle that entirely hovers according to claim 8, it is characterized in that: described second capsule refers to that seat (8) and air bag (1) glued joint or radio-frequency welding, and described connecting band (6) and air bag (1) glued joint or radio-frequency welding.
10. the formula air cushion vehicle that entirely hovers according to claim 1, it is characterized in that: described capsule refers to that (2) are made up of cotton synthetic fibre or polyurethane nylon or Hypalon material, and described air bag (1) and capsule refer to that seat is made up of PVC material or elastomeric material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520191069.7U CN204548092U (en) | 2015-03-31 | 2015-03-31 | One hovers formula air cushion vehicle entirely |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520191069.7U CN204548092U (en) | 2015-03-31 | 2015-03-31 | One hovers formula air cushion vehicle entirely |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204548092U true CN204548092U (en) | 2015-08-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520191069.7U Withdrawn - After Issue CN204548092U (en) | 2015-03-31 | 2015-03-31 | One hovers formula air cushion vehicle entirely |
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| Country | Link |
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| CN (1) | CN204548092U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104760589A (en) * | 2015-03-31 | 2015-07-08 | 广州广船国际股份有限公司 | Floating hovership |
| CN105235677A (en) * | 2015-10-14 | 2016-01-13 | 江门飞鲸科技实业有限公司 | Hovercraft using distributed duct fans |
-
2015
- 2015-03-31 CN CN201520191069.7U patent/CN204548092U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104760589A (en) * | 2015-03-31 | 2015-07-08 | 广州广船国际股份有限公司 | Floating hovership |
| CN105235677A (en) * | 2015-10-14 | 2016-01-13 | 江门飞鲸科技实业有限公司 | Hovercraft using distributed duct fans |
| CN105235677B (en) * | 2015-10-14 | 2018-05-01 | 佛山夸克兄弟科技有限公司 | A kind of aircushion vehicle of application distribution formula ducted-fan blower |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 510382 Fangcun Road, Guangdong, Liwan District Province, south of No. 40, No. Patentee after: CSSC OFFSHORE & MARINE ENGINEERING (GROUP) COMPANY LIMITED Address before: 510382 Fangcun Road, Guangdong, Liwan District Province, south of No. 40, No. Patentee before: Guangzhou Shipyard International Co., Ltd. |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20151224 Address after: 511462 Nansha District, Guangzhou, Pearl River Management District, West Road, No., the first floor of the layer on the ground floor, No. 68 Patentee after: GUANGZHOU SHIPYARD INTERNATIONAL COMPANY LIMITED Address before: 510382 Fangcun Road, Guangdong, Liwan District Province, south of No. 40, No. Patentee before: CSSC OFFSHORE & MARINE ENGINEERING (GROUP) COMPANY LIMITED |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20150812 Effective date of abandoning: 20170405 |
|
| AV01 | Patent right actively abandoned |