CN106542069A - A kind of underwater aircraft - Google Patents
A kind of underwater aircraft Download PDFInfo
- Publication number
- CN106542069A CN106542069A CN201610932033.9A CN201610932033A CN106542069A CN 106542069 A CN106542069 A CN 106542069A CN 201610932033 A CN201610932033 A CN 201610932033A CN 106542069 A CN106542069 A CN 106542069A
- Authority
- CN
- China
- Prior art keywords
- section
- linkage section
- underwater aircraft
- underwater
- linkage
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/001—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B3/00—Hulls characterised by their structure or component parts
- B63B3/13—Hulls built to withstand hydrostatic pressure when fully submerged, e.g. submarine hulls
Abstract
The invention discloses a kind of underwater aircraft, it is characterised in that include：First section, control section, linkage section, power section and rear；The first section, control section, linkage section, power section and rear splice fixation successively, and are assembled together successively by securing member two-by-two.By the way, so that underwater vehicle hull is consisted of stagewise, and by adopting composite material casing, on the premise of submarine navigation device housing crushing resistance is met, greatly reduce the w/v of underwater aircraft, its inner space is effectively increased, so as to significantly improve the overall performance of underwater aircraft.
Description
Technical field
The present invention relates to a kind of underwater aircraft, specifically a kind of housing is by composite and traditional material segmentation spelling
The underwater aircraft for connecing.
Background technology
Submarine navigation device is military for deep water observation, salvage, Underwater Engineering maintenance, marine petroleum development, naval
The various underwater performances equipments such as construction.Submarine navigation device completes the various actions such as dive, floating, rotation, sidesway, advance, retrogressing
All propeller is driven to rotate and produce thrust to complete by motor.The housing crushing resistance of submarine navigation device, bulking value
It is the important indicator for judging submarine navigation device performance than, the internal useful space.
Submarine navigation device housing manufacture material is generally metal alloy, such as aluminium alloy.Using metal alloy compositions shell
Submarine navigation device, compared with the material shell submarine navigation device with identical casings crushing resistance, its w/v is often
Larger, its internal useful space is also relatively small in addition, i.e., can carry device inside which less.By composite and traditional material
The mode that material combines, and the form using splicing constitutes new stagewise submarine navigation device, is ensureing submarine navigation device housing
On the premise of crushing resistance, submarine navigation device case weight volume ratio can be not only substantially reduced, and more feature devices can be carried
Part, on the premise of its function is met, it will be apparent that improve the overall performance of submarine navigation device.
The content of the invention
In order to improve conventional subsea aircraft in one timing of housing crushing resistance, its case weight volume ratio and internal effectively sky
Between some shortcomings in problem, the present invention proposes a kind of underwater aircraft, the housing of aircraft improved.
To reach above-mentioned purpose, technical scheme is as follows：
A kind of underwater aircraft, including：First section, control section, linkage section, power section and rear；
The first section, control section, linkage section, power section and rear splice fixation successively, and by securing member two-by-two according to
It is secondary to be assembled together.
In a preferred embodiment of the invention, baffle plate is provided between the control section and linkage section, the baffle plate is used
In the control section and linkage section are isolated.
In a preferred embodiment of the invention, the linkage section is used for underwater aircraft signal transmission, wherein
GPS communication terminals be located at linkage section above, for the transmission of gps signal；Communication signal end is located at the side of linkage section, for interior
The derivation of portion's signal and the input of control signal.
In a preferred embodiment of the invention, the control section and power section are using the preparation of same composite
Into the linkage section is prepared from using metal alloy compositions, and the linkage section is used as the transition of two sections of composite material casings
Section.
In a preferred embodiment of the invention, the length of two sections of compositions of the control section and power section is about whole water
The 50% of lower aircraft length.
After using above-mentioned technical proposal, the invention has the advantages that：
By the way so that underwater vehicle hull is consisted of stagewise, and by adopting composite
Housing, on the premise of submarine navigation device housing crushing resistance is met, greatly reduces the w/v of underwater aircraft,
Its inner space is effectively increased, so as to significantly improve the overall performance of underwater aircraft.
Description of the drawings
Fig. 1 is composite material submarine navigation device structure chart
Fig. 2 is composite material submarine navigation device linkage section profile
Fig. 3 composite material submarine navigation device linkage section bolt installations diagram-as shown in Figure 2, it is proposed that in Fig. 3 enterprising
The title of step sign all parts
In figure, 1- first sections, 2- control sections, 3-GPS communication terminals, 4- linkage sections, 5- power sections, 6- rears, 7- fin rudders, 8- spiral shells
Rotation oar, 9- motor shafts, 10- fin rudder bolts, 11- rear bolts, 12- control section bolts, 13- communication signals end, 14- communication signals
Bolt, 15- switches, 16- cock bolts, 17- first section bolts, 18- baffle plate bolts, 19- baffle plates, 20- linkage section bolts, 21-O types
Sealing ring, 22-O type sealing rings, 23- communication ports.
Specific embodiment
The present embodiment is a kind of stagewise composite material submarine navigation device, mainly includes first section 1, control section 2, connection
Section 4, power section 5, rear 6, fin rudder 7, propeller 8.
Conventional metal alloys shell submarine navigation device is carried out into sectionally smooth join.Underwater aircraft is divided into first section, control
Section, linkage section, power section, five part of rear, and each several part is manufactured respectively, finally spliced, constituted underwater
Aircraft.
To ensure the line style and its fluid property of submarine navigation device, underwater aircraft first section case material and conventional water
Lower aircraft material is identical, is metal alloy compositions, so as to ensure that the fluid line style of underwater aircraft front end；
The control section and power piece housing of underwater aircraft is fabricated by by composite, and its shell length is about whole
The 50% of individual submarine navigation device length, by the use to composite, not only greatly improves underwater aircraft
Crushing resistance, and considerably reduce the overall weight volume ratio of submarine navigation device；
The connection piece housing of underwater aircraft is metal alloy shell, for underwater aircraft signal transmission,
And as the changeover portion of two sections of composite material casings；
Due to submarine navigation device rear complex structure, be not suitable for manufacturing using composite, therefore underwater aircraft tail
Piece housing material is identical with conventional subsea aircraft material, is metal alloy compositions.
First section 1 be underwater aircraft head, be joined directly together with control section 2, using eight first section bolts 17 by its
Closely connect.
Control section 2 is underwater aircraft control cabinet, and its front end is connected with first section by eight first section bolts 17, thereafter
End is closely connected with linkage section 4 by eight linkage section bolts 20；
Baffle plate 19 is used for the isolation of control section 2 and linkage section 4, and is fixed by two baffle plate bolts 18；O-ring seal
21,22 for the process of junction watertight；Communication port 23 is used for the signal communication of control section 2.
Linkage section 4 is used for underwater aircraft signal transmission, and its front end passes through eight linkage section bolts 20 with control section 2
Closely connect, and be isolated by baffle plate 19, its rear end is connected with power section 5, and closely connected by eight control section bolts 12；
GPS communication terminals 3 are located above linkage section 4, for the transmission of gps signal；Communication signal end 13 is located on the left of linkage section 4, is used for
The derivation of its internal signal and the input of control signal, and be fixed on linkage section 4 by a communication signal bolt 14；Switch
15 are located on the right side of linkage section 4, and are fixed on linkage section 4 by four cock bolts 16.
Power section 5 is powered for underwater aircraft, and its front end is tight by eight control section bolts 12 with linkage section 4
Connection, its rear end are connected with rear 6, and are closely connected by rear bolt 11.
Rear 6 is submarine navigation device drive part, and propeller 8 is installed in its afterbody and is set on motor shaft 9；Four fins
, respectively on rear 6, for underwater aircraft gesture stability, and it is tight with rear 6 to pass through four fin rudder bolts 10 for rudder 7
Close connection；6 front end of rear is closely connected with power section 5 by eight rear bolts 11.
By the way so that underwater vehicle hull is consisted of stagewise, and by adopting composite
Housing, on the premise of submarine navigation device housing crushing resistance is met, greatly reduces the w/v of underwater aircraft,
Its inner space is effectively increased, so as to significantly improve the overall performance of underwater aircraft.
Claims (5)
1. a kind of underwater aircraft, it is characterised in that include：First section, control section, linkage section, power section and rear；
The first section, control section, linkage section, power section and rear splice fixation successively, and are filled successively by securing member two-by-two
With together.
2. a kind of underwater aircraft according to claim 1, it is characterised in that between the control section and linkage section
Baffle plate is provided with, the baffle plate is for the control section and linkage section are isolated.
3. a kind of underwater aircraft according to claim 1, it is characterised in that the linkage section is used for underwater
Aircraft signal transmission, GPS communication terminals therein are located above linkage section, for the transmission of gps signal；Communication signal end is located at
The side of linkage section, the input of derivation and control signal for internal signal.
4. a kind of underwater aircraft according to one of claim 1-3, it is characterised in that the control section and power
The same composites of Duan Caiyong are prepared from, and the linkage section is prepared from using metal alloy compositions, and the linkage section is made
For the changeover portion of two sections of composite material casings.
5. a kind of underwater aircraft according to claim 4, it is characterised in that two sections of the control section and power section
The length of composition is about the 50% of whole submarine navigation device length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610932033.9A CN106542069A (en) | 2016-10-25 | 2016-10-25 | A kind of underwater aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610932033.9A CN106542069A (en) | 2016-10-25 | 2016-10-25 | A kind of underwater aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106542069A true CN106542069A (en) | 2017-03-29 |
Family
ID=58392747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610932033.9A Pending CN106542069A (en) | 2016-10-25 | 2016-10-25 | A kind of underwater aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106542069A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108313243A (en) * | 2018-04-03 | 2018-07-24 | 河北科技大学 | A kind of underwater submariner rapid propulsion device and processing method |
| CN108321598A (en) * | 2017-12-27 | 2018-07-24 | 中国船舶重工集团公司第七0研究所 | Autonomous aircraft under a kind of modular water |
| CN111634394A (en) * | 2020-06-09 | 2020-09-08 | 长沙金信诺防务技术有限公司 | Underwater vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1531569A1 (en) * | 1967-12-21 | 1969-12-18 | Herbert Evans | Process for the manufacture of submersible boats |
| US6483865B1 (en) * | 2000-04-13 | 2002-11-19 | The Boeing Company | Wireless interface for electronic devices located in enclosed spaces |
| CN1666925A (en) * | 2005-01-07 | 2005-09-14 | 天津大学 | Underwater self-navigating platform mechanical system |
| CN102862667A (en) * | 2012-09-26 | 2013-01-09 | 浙江大学 | Mixed type underwater navigation detector |
| CN105620693A (en) * | 2016-01-28 | 2016-06-01 | 安阳市腾飞高分子复合材料有限公司 | Novel pressure-resistant cabin body made from carbon fiber macromolecular composite materials and manufacturing technology of novel pressure-resistant cabin body |
| CN105711777A (en) * | 2016-01-26 | 2016-06-29 | 河北工业大学 | Micro-miniature modularized AUV (autonomous underwater vehicle) |
-
2016
- 2016-10-25 CN CN201610932033.9A patent/CN106542069A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1531569A1 (en) * | 1967-12-21 | 1969-12-18 | Herbert Evans | Process for the manufacture of submersible boats |
| US6483865B1 (en) * | 2000-04-13 | 2002-11-19 | The Boeing Company | Wireless interface for electronic devices located in enclosed spaces |
| CN1666925A (en) * | 2005-01-07 | 2005-09-14 | 天津大学 | Underwater self-navigating platform mechanical system |
| CN102862667A (en) * | 2012-09-26 | 2013-01-09 | 浙江大学 | Mixed type underwater navigation detector |
| CN105711777A (en) * | 2016-01-26 | 2016-06-29 | 河北工业大学 | Micro-miniature modularized AUV (autonomous underwater vehicle) |
| CN105620693A (en) * | 2016-01-28 | 2016-06-01 | 安阳市腾飞高分子复合材料有限公司 | Novel pressure-resistant cabin body made from carbon fiber macromolecular composite materials and manufacturing technology of novel pressure-resistant cabin body |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108321598A (en) * | 2017-12-27 | 2018-07-24 | 中国船舶重工集团公司第七0研究所 | Autonomous aircraft under a kind of modular water |
| CN108321598B (en) * | 2017-12-27 | 2019-06-11 | 中国船舶重工集团公司第七一0研究所 | Autonomous aircraft under a kind of modular water |
| CN108313243A (en) * | 2018-04-03 | 2018-07-24 | 河北科技大学 | A kind of underwater submariner rapid propulsion device and processing method |
| CN111634394A (en) * | 2020-06-09 | 2020-09-08 | 长沙金信诺防务技术有限公司 | Underwater vehicle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170329 |
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| RJ01 | Rejection of invention patent application after publication |