CN202499129U - Air cushion ship for rodeo - Google Patents
Air cushion ship for rodeo Download PDFInfo
- Publication number
- CN202499129U CN202499129U CN201220113947XU CN201220113947U CN202499129U CN 202499129 U CN202499129 U CN 202499129U CN 201220113947X U CN201220113947X U CN 201220113947XU CN 201220113947 U CN201220113947 U CN 201220113947U CN 202499129 U CN202499129 U CN 202499129U
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- CN
- China
- Prior art keywords
- air cushion
- thrust
- ship
- fan
- rudder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- ZEKANFGSDXODPD-UHFFFAOYSA-N glyphosate-isopropylammonium Chemical compound CC(C)N.OC(=O)CNCP(O)(O)=O ZEKANFGSDXODPD-UHFFFAOYSA-N 0.000 title abstract 2
- 230000000386 athletic effect Effects 0.000 claims description 6
- 230000003028 elevating effect Effects 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 abstract 3
- 239000003638 chemical reducing agent Substances 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 3
- 239000007921 spray Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 1
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model relates to an air cushion ship for a rodeo, mainly solving the technical problems of low thrust efficiency and small lift force in the conventional air cushion ship. The air cushion ship adopts the technical scheme as follows: the air cushion ship comprises a lift fan, a handle, a ship housing, an engine, a thrust fan, a lifting rudder, a rudder, an air cushion skirt and a thrust barrel as well as a transmission rod and a direction changer, wherein the lift fan is arranged on the top surface of the front end of the ship housing; the handle is arranged on the top surface of the front part of the ship housing; the engine is arranged in the back middle part in the ship housing; the thrust barrel is mounted on the top surface of the rear part of the ship housing; the thrust fan is mounted at the front part of the thrust barrel; the lifting rudder is horizontally arranged at the upper part of the rear end of the thrust barrel; the rudder is vertically arranged behind the thrust barrel and is connected with the handle; the air cushion skirt is mounted on the periphery of the ship housing; one end of the transmission rod is connected with a speed reducer of the engine; the other end of the transmission rod is connected with the input end of the direction changer; and the output end of the direction changer is connected with a rotary shaft of the lift fan.
Description
Technical field
The utility model relates to a kind of athletic competition and uses air cushion vehicle, and it belongs to a kind of air cushion vehicle that have direction control of navigation on the meadow and the water surface that can hover.
Background technology
Existing air cushion vehicle mostly is to be used as power with air screw, when air screw advances, on the water surface, evokes the very high spray; These sprays are to want the consumption of power energy, so the propulsion coefficient of boats and ships is low, on the other hand; The lift fan inlet and outlet of existing air cushion vehicle is the rear portion that is positioned at boats and ships mostly, and outlet is perpendicular to hull, because its living power is little; In high-speed travel, can't air cushion vehicle be raised to the little height of resistance, influence game tempo.
Summary of the invention
The purpose of the utility model is to solve the low and little technical matters of lift of propulsion coefficient that existing air cushion vehicle exists, and provides a kind of propulsion coefficient height and the big athletic competition of lift to use air cushion vehicle.
The utility model is to solve the problems of the technologies described above the technical scheme that adopts to be: air cushion vehicle is used in athletic competition, comprises lift fan, steering handle, shell, driving engine, fan propeller, elevating rudder, yaw rudder, caisson feed supple sirts and thrust tube, and wherein: it also comprises drive link and commutator; Lift fan is located on the end face of shell front end; Steering handle is located on the anterior end face of shell and is positioned at the back of lift fan, and driving engine is located at the postmedian in the shell, and the thrust wound packages is on the end face of hull back; Fan propeller is contained in the anterior of thrust tube and is connected with driving engine through retarder; The elevating rudder level is located at the top of thrust tube rear end, and yaw rudder vertically is located at the back of thrust tube and is positioned at the back of fan propeller, and yaw rudder is connected with steering handle through cable wire; Caisson feed supple sirts be contained in shell around; One end of drive link is connected with the retarder of driving engine, and the other end of drive link is connected with the input end of commutator, and the mouth of commutator is connected with the rotating shaft of lift fan.
Because the utility model has adopted technique scheme, solved the low and little technical matters of lift of propulsion coefficient that existing air cushion vehicle exists.Therefore, compare, the utlity model has the high and big advantage of lift of propulsion coefficient with background technology.
Description of drawings
Fig. 1 is the structural representation of the utility model;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the right elevation of Fig. 1.
The specific embodiment
Like Fig. 1, Fig. 2 and shown in Figure 3; Air cushion vehicle is used in athletic competition in the present embodiment, comprises lift fan 1, steering handle 2, shell 3, driving engine 4, fan propeller 5, elevating rudder 6, yaw rudder 7, caisson feed supple sirts 8 and thrust tube 11, and wherein: it also comprises drive link 9 and commutator 10; Lift fan 1 is located on the end face of shell 3 front ends; Steering handle 2 is located on the shell 3 anterior end faces and is positioned at the back of lift fan 1, and driving engine 4 is located at the postmedian in the shell 3, and thrust tube 11 is contained on the end face at shell 3 rear portions; Fan propeller 5 is contained in the anterior of thrust tube 11 and is connected with driving engine 4 through retarder; Elevating rudder 6 levels are located at the top of thrust tube 11 rear ends, and yaw rudder 7 vertically is located at the back of thrust tube 11 and is positioned at the back of fan propeller 5, and yaw rudder 7 is connected with steering handle 2 through cable wire; Caisson feed supple sirts 8 be contained in shell 3 around; One end of drive link 9 is connected with the retarder of driving engine 4, and the other end of drive link 9 is connected with the input end of commutator 10, and the mouth of commutator 10 is connected with the rotating shaft of lift fan 1.
Claims (1)
1. air cushion vehicle is used in an athletic competition, comprises lift fan, steering handle, shell, driving engine, fan propeller, elevating rudder, yaw rudder, caisson feed supple sirts and thrust tube, it is characterized in that: further comprising drive link and commutator; Lift fan is located on the end face of shell front end; Steering handle is located on the anterior end face of shell and is positioned at the back of lift fan, and driving engine is located at the postmedian in the shell, and the thrust wound packages is on the end face of hull back; Fan propeller is contained in the anterior of thrust tube and is connected with driving engine through retarder; The elevating rudder level is located at the top of thrust tube rear end, and yaw rudder vertically is located at the back of thrust tube and is positioned at the back of fan propeller, and yaw rudder is connected with steering handle through cable wire; Caisson feed supple sirts be contained in shell around; One end of drive link is connected with the retarder of driving engine, and the other end of drive link is connected with the input end of commutator, and the mouth of commutator is connected with the rotating shaft of lift fan.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201220113947XU CN202499129U (en) | 2012-03-23 | 2012-03-23 | Air cushion ship for rodeo |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201220113947XU CN202499129U (en) | 2012-03-23 | 2012-03-23 | Air cushion ship for rodeo |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202499129U true CN202499129U (en) | 2012-10-24 |
Family
ID=47035754
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201220113947XU Expired - Fee Related CN202499129U (en) | 2012-03-23 | 2012-03-23 | Air cushion ship for rodeo |
Country Status (1)
Country | Link |
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CN (1) | CN202499129U (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2592754C1 (en) * | 2015-01-19 | 2016-07-27 | Александр Юрьевич Тенищев | Propulsor with cargo platform on air cushion |
CN106364639A (en) * | 2016-08-31 | 2017-02-01 | 何洪波 | Full cushion lifting hovercraft |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US10875658B2 (en) | 2015-09-02 | 2020-12-29 | Jetoptera, Inc. | Ejector and airfoil configurations |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US11148801B2 (en) | 2017-06-27 | 2021-10-19 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US20220242385A1 (en) * | 2021-02-04 | 2022-08-04 | Rui Ma | An electric hovercraft for sports competitions |
-
2012
- 2012-03-23 CN CN201220113947XU patent/CN202499129U/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2592754C1 (en) * | 2015-01-19 | 2016-07-27 | Александр Юрьевич Тенищев | Propulsor with cargo platform on air cushion |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US10875658B2 (en) | 2015-09-02 | 2020-12-29 | Jetoptera, Inc. | Ejector and airfoil configurations |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
CN106364639A (en) * | 2016-08-31 | 2017-02-01 | 何洪波 | Full cushion lifting hovercraft |
US11148801B2 (en) | 2017-06-27 | 2021-10-19 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US20220242385A1 (en) * | 2021-02-04 | 2022-08-04 | Rui Ma | An electric hovercraft for sports competitions |
US11465603B2 (en) * | 2021-02-04 | 2022-10-11 | Rui Ma | Electric hovercraft for sports competitions |
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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: 20121024 Termination date: 20150323 |
|
EXPY | Termination of patent right or utility model |