CN205872427U - Take photo by plane and seek thunder and use unmanned dirigible in sea - Google Patents
Take photo by plane and seek thunder and use unmanned dirigible in sea Download PDFInfo
- Publication number
- CN205872427U CN205872427U CN201620774272.1U CN201620774272U CN205872427U CN 205872427 U CN205872427 U CN 205872427U CN 201620774272 U CN201620774272 U CN 201620774272U CN 205872427 U CN205872427 U CN 205872427U
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- Prior art keywords
- dirigible
- motor
- thunder
- sea
- seek
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Abstract
The utility model provides a take photo by plane and seek thunder and use unmanned dirigible in sea, by installing at the anterior telecontrol antenna of dirigible, the metal hood, install the wind direction sensor of bottom before the dirigible, install at the left left propeller of dirigible, left side stand -by motor, install the right spiral oar on the dirigible right side, right side stand -by motor, install the channel screw at the dirigible middle part, the channel motor, install the high definition camera of lower part in the dirigible, the battery flat, electronic cabin, the balloon pressure sensor, install the antenna at the GPS of dirigible afterbody, the video transmission antenna, main motor, the principal screw oar, install the channel casing at middle part in the dirigible, the barometric height sensor group who installs lower part in the dirigible becomes, the gasbag by left ship wing gasbag, right ship wing gasbag, main gasbag, ballonet, port tailplane gasbag, right empennage gasbag, go up the fin gasbag and constitute. It can the reinforce to have the anti -wind, and be waterproof, and climatization can the reinforce, and hang time is long, the convenience of taking off and land, the low and risk of use cost advantage such as little.
Description
Technical field
This utility model relates to unmanned airship technical field, is specifically related to a kind of sea and takes photo by plane and seek thunder unmanned airship.
Background technology
During sea trial, troops' action image data is abnormal precious, to the strongest demand of taking photo by plane, meanwhile, and test behaviour's thunder
After floating, torpedo recovery boat is difficult to determine behaviour thunder position fast and accurately, needs to rely on air power to carry out seeking thunder.Test period is usual
Up to a few hours, this requires that the aircraft being used for taking photo by plane and seek thunder has longer flying power；It is big that sea climate has wind, empty
The feature of gas high humidity, and rainy weather may be met with, it is stronger that this just requires that the aircraft performing to take photo by plane and seek thunder has
Wind loading rating, and preferably water resistance.Unmanned plane flying power, wind loading rating and the water resistance sold in the market
It is difficult to meet the requirement taken photo by plane and seek thunder in sea, is the most all to use helicopter to carry out taking photo by plane and seek thunder, but helicopter navigates by water into
This is high.Unmanned airship, relative to helicopter, has the hang time long, takes off and lands conveniently, and use cost is low and risk is little
Etc. advantage.Utilize unmanned airship to carry high-definition camera system, utilize Radio Transmission Technology, design preferable control system and power
System, it is possible to satisfied sea is taken photo by plane, sought the mission requirements such as thunder.
Summary of the invention
This utility model provides a kind of sea and takes photo by plane and seek thunder unmanned airship, is conducive to overcoming on market on sale unmanned
Aircraft cruising time is short, wind loading rating and the shortcoming of water resistance difference, is simultaneously also beneficial to overcome use helicopter cost high
High shortcoming.Disclosure satisfy that taking photo by plane and seeking thunder demand during sea trial.
For solving above-mentioned technical problem, the application be the technical scheme is that take photo by plane and seek thunder with unmanned in a kind of sea
Dirigible, is made up of with information system inner frame and assembly, air bag and control, and inner frame and assembly are anterior by being arranged on dirigible
Telecontrol antenna, metal head-shield, be arranged on the wind transducer of bottom before dirigible, be arranged on the left-hand airscrew on the left of dirigible, left
Stand-by motor, is arranged on the right-hand screw oar on the right side of dirigible, right redundant motor, is arranged on the conduit propeller in the middle part of dirigible, conduit
Motor, is arranged on the high-definition camera of dirigible middle and lower part, battery flat, electronic compartment, gasbag pressure sensor, is arranged on dirigible afterbody
Gps antenna, transmission of video antenna, mair motor, main screw, be arranged in dirigible the conduit housing at middle part, be arranged on dirigible
The pressure-altitude sensor composition of middle and lower part；Described air bag is by left ship wing air bag, right ship wing air bag, main gasbag, balloonet, a left side
Empennage air bag, starboard tailplane air bag, upper empennage air bag form；Control with information system by control system, communication module and storage mould
Block forms.
As a preferred technical scheme of the present utility model, described left redundant motor and right redundant motor are
Waterproof machine.
As a preferred technical scheme of the present utility model, described conduit motor is waterproof machine, conduit motor
Drive connection conduit propeller, the propeller installation direction of conduit propeller is vertical with left-hand airscrew and right-hand screw oar.
As a preferred technical scheme of the present utility model, described mair motor uses waterproof machine, and mair motor drives
Be dynamically connected main screw.
As a preferred technical scheme of the present utility model, described battery flat uses sealing cabin, its internal dress
Dynamic battery and instrument battery, electrokinetic cell electrical connection left redundant motor, right redundant motor, mair motor, conduit motor, instrument
Battery electrical connection controls and information system, gps antenna, high-definition camera.
As a preferred technical scheme of the present utility model, described electronic compartment uses seal casinghousing, controls and letter
Breath system is arranged on inside.
As a preferred technical scheme of the present utility model, described gasbag pressure sensor is installed on balloonet
On, balloonet top is provided with gas vent, and gas vent is controlled switch by control system.
As a preferred technical scheme of the present utility model, described main gasbag, balloonet all fill helium, main gas
The maximum volume of capsule and balloonet is than for 17:3.
As a preferred technical scheme of the present utility model, described wind transducer, high-definition camera are the most waterproof.
The beneficial effects of the utility model are:
Having wind loading rating strong, waterproof, climatic adaptation ability is strong, and the hang time is long, takes off and land conveniently, use cost
The advantages such as low and risk is little.Can preferably meet below strong gale sea to take photo by plane, seek the mission requirements such as thunder.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, the accompanying drawing in describing below is only
Embodiments more of the present utility model, for those of ordinary skill in the art, in the premise not paying creative work
Under, it is also possible to other accompanying drawing is obtained according to these accompanying drawings.
Take photo by plane and seek thunder unmanned airship inner frame and assembly plan view in Fig. 1 this utility model sea；
Take photo by plane and seek thunder unmanned airship inner frame and components side view in Fig. 2 this utility model sea；
Take photo by plane and seek thunder unmanned airship outside side view in Fig. 3 this utility model sea；
Take photo by plane and seek thunder unmanned airship outward appearance top view in Fig. 4 this utility model sea.
Detailed description of the invention
This utility model provides a kind of sea and takes photo by plane and seek thunder unmanned airship, is conducive to overcoming on market on sale unmanned
Aircraft cruising time is short, wind loading rating and the shortcoming of water resistance difference, is simultaneously also beneficial to overcome use helicopter cost high
High shortcoming.Disclosure satisfy that taking photo by plane and seeking thunder demand during sea trial.
In order to be better understood from technique scheme, below in conjunction with Figure of description and specific embodiment to upper
State technical scheme to be described in detail.
Embodiment one
Take photo by plane and seek thunder unmanned airship in a kind of sea described in the present embodiment, by inner frame and assembly, air bag and control
System forms with information system, and inner frame and assembly, by being arranged on the anterior telecontrol antenna 1 of dirigible, metal head-shield 2, are arranged on and fly
The wind transducer 3 of bottom before ship, wind transducer measures wind direction, and when needing hovering, control system controls left and right auxiliary propulsion
Device adjustment of rotational speed dirigible course, just to wind direction, controls main thruster rotating speed and realizes dirigible hovering, be arranged on the left spiral shell on the left of dirigible
Rotation oar 4, left redundant motor 5, it is arranged on the right-hand screw oar 6 on the right side of dirigible, right redundant motor 7, is arranged on the conduit in the middle part of dirigible
Propeller 8, conduit motor 9, be arranged on the high-definition camera 10 of dirigible middle and lower part, battery flat 11, electronic compartment 12, and gasbag pressure passes
Sensor 13, is arranged on the gps antenna 14 of dirigible afterbody, transmission of video antenna 15, mair motor 16, main screw 17, is arranged on and flies
The conduit housing 18 at middle part in ship, the pressure-altitude sensor 19 being arranged on dirigible middle and lower part forms；Described air bag is by left ship
Wing air bag 20, right ship wing air bag 21, main gasbag 22, balloonet 23, port tailplane air bag 24, starboard tailplane air bag 25, upper empennage air bag
26 compositions；Control to be made up of with memory module control system, communication module with information system.
Wherein, in the present embodiment, described left redundant motor 5 and right redundant motor 7 are waterproof machine, left redundant
Motor 5 and right redundant motor 7 and propeller are mainly used in controlling dirigible course.
Wherein, in the present embodiment, described conduit motor 9 is waterproof machine, conduit motor 9 drive connection conduit spiral
Oar 8, the propeller installation direction of conduit propeller 8 is vertical with left-hand airscrew 4 and right-hand screw oar 6, conduit motor 9 and conduit spiral shell
Rotation oar 8 is mainly used in the Altitude control of dirigible.
Wherein, in the present embodiment, described mair motor 16 uses waterproof machine, mair motor 16 drive connection main screw
17, the maximum output power that itself and main screw 17 provide is resistant to strong gale, mair motor 16 and main screw 17 and mainly carries dirigible
For longitudinal thrust.
Wherein, in the present embodiment, described battery flat 11 uses sealing cabin, equipped with electrokinetic cell and instrument inside it
Battery, electrokinetic cell electrical connection left redundant motor 5, right redundant motor 7, mair motor 16, conduit motor 9, instrument battery electrically connects
Control and information system, gps antenna 14, high-definition camera 10.
Wherein, in the present embodiment, described electronic compartment 12 uses seal casinghousing, in controlling to be arranged on information system
Portion.
Wherein, in the present embodiment, described gasbag pressure sensor 13 is installed on balloonet 23, balloonet 23 top
Being provided with gas vent, gas vent is controlled switch by control system, and pressure-altitude sensor is measured dirigible height and reached to set maximum height
During angle value, under conduit motor not working condition, if dirigible still becomes ascendant trend i.e. buoyancy for just, then control system controls balloonet
Venting is until this height buoyancy is 0.
Wherein, in the present embodiment, described main gasbag 22, balloonet 23 all fill helium, main gasbag 22 and balloonet
The maximum volume of 23 is than for 17:3.
Wherein, in the present embodiment, described wind transducer 3, high-definition camera 10 are the most waterproof.
Speed, course, the adjustment of height can be realized by ground remote control terminal, and be provided with landing mode.Open landing
Pattern, balloonet release part helium, make balloonet pressure arrive landing setting value.
The above, be only preferred embodiment of the present utility model, not this utility model is made any in form
Restriction, although this utility model is disclosed above with preferred embodiment, but is not limited to this utility model, any ripe
Know professional and technical personnel, in the range of without departing from technical solutions of the utility model, when in the technology of available the disclosure above
Hold and make a little change or be modified to the Equivalent embodiments of equivalent variations, as long as without departing from technical solutions of the utility model
Hold, any simple modification, equivalent variations and modification above example made according to technical spirit of the present utility model, the most still
Belong in the range of technical solutions of the utility model.
Claims (9)
1. take photo by plane and seek thunder unmanned airship in a sea, it is characterised in that by inner frame and assembly, air bag and control and letter
Breath system forms, and inner frame and assembly, by being arranged on the anterior telecontrol antenna (1) of dirigible, metal head-shield (2), are arranged on dirigible
The wind transducer (3) of front bottom, is arranged on the left-hand airscrew (4) on the left of dirigible, left redundant motor (5), is arranged on dirigible right
The right-hand screw oar (6) of side, right redundant motor (7), be arranged on the conduit propeller (8) in the middle part of dirigible, conduit motor (9), installs
High-definition camera (10) in dirigible middle and lower part, battery flat (11), electronic compartment (12), gasbag pressure sensor (13), it is arranged on
The gps antenna (14) of dirigible afterbody, transmission of video antenna (15), mair motor (16), main screw (17), it is arranged in dirigible
The conduit housing (18) in portion, is arranged on pressure-altitude sensor (19) composition of dirigible middle and lower part；Described air bag is by the left ship wing
Air bag (20), right ship wing air bag (21), main gasbag (22), balloonet (23), port tailplane air bag (24), starboard tailplane air bag (25),
Upper empennage air bag (26) forms；Control to be made up of with memory module control system, communication module with information system.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described left redundant
Motor (5) and right redundant motor (7) are waterproof machine.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described conduit electricity
Machine (9) is waterproof machine, conduit motor (9) drive connection conduit propeller (8), the propeller installation side of conduit propeller (8)
To vertical with left-hand airscrew (4) and right-hand screw oar (6).
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described mair motor
(16) waterproof machine, mair motor (16) drive connection main screw (17) are used.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described battery flat
(11) using sealing cabin, equipped with electrokinetic cell and instrument battery inside it, electrokinetic cell connects left redundant motor (5), inside right forward
Helping motor (7), mair motor (16), conduit motor (9), the electrical connection of instrument battery controls and information system, gps antenna (14), height
Clear video camera (10).
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described electronic compartment
(12) use seal casinghousing, control to be arranged on inside with information system.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described air bag pressure
Force transducer (13) is installed on balloonet (23), and balloonet (23) top is provided with gas vent, and gas vent is by control system control
Switch.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described main gasbag
(22), balloonet (23) all fill helium, the maximum volume of main gasbag (22) and balloonet (23) ratio is for 17:3.
Take photo by plane and seek thunder unmanned airship in a kind of sea the most according to claim 1, it is characterised in that described wind direction passes
Sensor (3), high-definition camera (10) are the most waterproof.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620774272.1U CN205872427U (en) | 2016-07-22 | 2016-07-22 | Take photo by plane and seek thunder and use unmanned dirigible in sea |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620774272.1U CN205872427U (en) | 2016-07-22 | 2016-07-22 | Take photo by plane and seek thunder and use unmanned dirigible in sea |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872427U true CN205872427U (en) | 2017-01-11 |
Family
ID=57697322
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620774272.1U Expired - Fee Related CN205872427U (en) | 2016-07-22 | 2016-07-22 | Take photo by plane and seek thunder and use unmanned dirigible in sea |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872427U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109592035A (en) * | 2018-12-04 | 2019-04-09 | 北京空天技术研究所 | High speed information platform and its application method can be suspended |
| CN110450936A (en) * | 2019-07-30 | 2019-11-15 | 福建工程学院 | A kind of unmanned airship delivery formula high foaming rate fixed froth installation |
| CN114339154A (en) * | 2021-12-29 | 2022-04-12 | 福州大学 | Floating type mobile camera device |
-
2016
- 2016-07-22 CN CN201620774272.1U patent/CN205872427U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109592035A (en) * | 2018-12-04 | 2019-04-09 | 北京空天技术研究所 | High speed information platform and its application method can be suspended |
| CN110450936A (en) * | 2019-07-30 | 2019-11-15 | 福建工程学院 | A kind of unmanned airship delivery formula high foaming rate fixed froth installation |
| CN114339154A (en) * | 2021-12-29 | 2022-04-12 | 福州大学 | Floating type mobile camera device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20170722 |