CN203172881U - Underwater airplane - Google Patents
Underwater airplane Download PDFInfo
- Publication number
- CN203172881U CN203172881U CN 201320024380 CN201320024380U CN203172881U CN 203172881 U CN203172881 U CN 203172881U CN 201320024380 CN201320024380 CN 201320024380 CN 201320024380 U CN201320024380 U CN 201320024380U CN 203172881 U CN203172881 U CN 203172881U
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- Prior art keywords
- airplane
- underwater
- sides
- body shell
- propeller
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Abstract
The utility model relates to an underwater airplane. The underwater airplane is characterized by comprising an airtight airplane body shell body, wherein two middle wings are arranged at two sides of the middle of the airplane body shell body, a propeller is arranged at the tail end of an airplane body, two tail vanes arranged at two sides of the propeller are arranged at the tail end of the airplane body, a motor is arranged inside the airplane body shell body and drives the propeller to rotate. According to the underwater airplane, the two middle wings are arranged at the two sides of the middle of the airplane body shell body, the propeller and the two tail vanes arranged at the two sides of the propeller are arranged at the tail end of the airplane body, the motor is arranged inside the airplane body shell body and drives the propeller to rotate, and therefore the underwater airplane is simple in structure, low in production cost and beneficial to reducing noise and improving the air quality inside a cabin.
Description
Technical field:
The utility model relates to a kind of underwater airplane.
Background technology:
Conveyer makes conveyer that bigger buoyancy be arranged owing to can discharge larger volume under water, can carry the greater weight goods, but when conveyer is equipped with diesel oil or engine petrol under water, structure all complicated, cost is also higher, and engine noise is big, the tail gas of discharge also can influence air in the cabin.
Summary of the invention:
The purpose of this utility model is to provide a kind of underwater airplane, and this underwater airplane is not only simple in structure, reasonable in design, and is conducive to reduce noise and improves air in the cabin.
The utility model underwater airplane, it is characterized in that: comprise airtight body shell, both sides, described body shell middle part are provided with two wing centre sections, and described fuselage tail end is provided with screw propeller and is located at two tail vanes of screw propeller both sides, are provided with in the described body shell and drive the electrical motor that screw propeller rotates.
Above-mentioned afterbody both sides are provided with two empennages.
Above-mentioned two wing centre section rear sides be provided with can upper and lower swing fin.
Above-mentioned two tail vanes are for vertically putting.
Above-mentioned two empennages be provided with can upper and lower swing back fin.
The utility model underwater airplane, be provided with two wing centre sections by both sides, closed fuselage housing middle part, the fuselage tail end is provided with screw propeller and is located at two tail vanes of screw propeller both sides, be provided with in the body shell and drive the electrical motor that screw propeller rotates, thereby screw propeller can drive this underwater airplane and carries out high speed and advance under the drive of electrical motor, therefore, underwater airplane of the present utility model not only simple in structure, productive costs is low, and be conducive to reduce noise and improve air quality in the cabin.
Description of drawings:
Fig. 1 is D structure scheme drawing of the present utility model;
Fig. 2 is D structure scheme drawing of the present utility model;
Fig. 3 is birds-eye view of the present utility model.
The specific embodiment:
The utility model underwater airplane, comprise airtight body shell 1, both sides, described body shell 1 middle part are provided with two wing centre sections 2, and described fuselage tail end is provided with screw propeller 3 and is located at two tail vanes 4 of screw propeller 3 both sides, are provided with in the described body shell 1 and drive the electrical motor 5 that screw propeller rotates.
More reliable for what the utility model underwater airplane was travelled, above-mentioned afterbody both sides are provided with two empennages 6.
In order to design needs, above-mentioned two wing centre sections, 2 rear sides be provided with can upper and lower swing fin 7.
In order to design needs, above-mentioned two tail vanes are for vertically putting.
More reliable for what the utility model underwater airplane was travelled, above-mentioned two empennages be provided with can upper and lower swing back fin 8.
The utility model underwater airplane, be provided with two wing centre sections by both sides, closed fuselage housing middle part, the fuselage tail end is provided with screw propeller and is located at two tail vanes of screw propeller both sides, be provided with in the body shell and drive the electrical motor that screw propeller rotates, thereby screw propeller can drive this underwater airplane and carries out high speed and advance under the drive of electrical motor, therefore, underwater airplane of the present utility model not only simple in structure, productive costs is low, and be conducive to reduce noise and improve air quality in the cabin.
The above only is preferred embodiment of the present utility model, and all equalizations of doing according to the utility model claim change and modify, and all should belong to covering scope of the present utility model.
Claims (5)
1. underwater airplane, it is characterized in that: comprise airtight body shell, both sides, described body shell middle part are provided with two wing centre sections, and described fuselage tail end is provided with screw propeller and is located at two tail vanes of screw propeller both sides, are provided with in the described body shell and drive the electrical motor that screw propeller rotates.
2. underwater airplane according to claim 1, it is characterized in that: described afterbody both sides are provided with two empennages.
3. underwater airplane according to claim 1 and 2 is characterized in that: described two wing centre section rear sides be provided with can upper and lower swing fin.
4. underwater airplane according to claim 3, it is characterized in that: described two tail vanes are for vertically putting.
5. underwater airplane according to claim 4 is characterized in that: described two empennages be provided with can upper and lower swing back fin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320024380 CN203172881U (en) | 2013-01-17 | 2013-01-17 | Underwater airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320024380 CN203172881U (en) | 2013-01-17 | 2013-01-17 | Underwater airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203172881U true CN203172881U (en) | 2013-09-04 |
Family
ID=49069623
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320024380 Expired - Fee Related CN203172881U (en) | 2013-01-17 | 2013-01-17 | Underwater airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203172881U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104589938A (en) * | 2014-03-20 | 2015-05-06 | 中国特种飞行器研究所 | Cross-medium aircraft with changeable shape like flying fish |
| CN109895939A (en) * | 2018-12-14 | 2019-06-18 | 上海海事大学 | Vault shell cabin self-saving manned underwater vehicle |
-
2013
- 2013-01-17 CN CN 201320024380 patent/CN203172881U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104589938A (en) * | 2014-03-20 | 2015-05-06 | 中国特种飞行器研究所 | Cross-medium aircraft with changeable shape like flying fish |
| CN104589938B (en) * | 2014-03-20 | 2016-07-13 | 中国特种飞行器研究所 | A kind of imitative flying fish variable configuration is across medium aircraft |
| CN109895939A (en) * | 2018-12-14 | 2019-06-18 | 上海海事大学 | Vault shell cabin self-saving manned underwater vehicle |
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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: 20130904 Termination date: 20190117 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |