CN209382280U - The barrel configuration of sensing system is launched for high-altitude - Google Patents
The barrel configuration of sensing system is launched for high-altitude Download PDFInfo
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- CN209382280U CN209382280U CN201822272709.3U CN201822272709U CN209382280U CN 209382280 U CN209382280 U CN 209382280U CN 201822272709 U CN201822272709 U CN 201822272709U CN 209382280 U CN209382280 U CN 209382280U
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- main frame
- sensor
- altitude
- sensing system
- barrel configuration
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Abstract
The utility model relates to high-altitudes to launch sensor field, especially a kind of barrel configuration that sensing system is launched for high-altitude, comprising: main frame, attachment device is set on the main frame, the attachment device can make main frame that can be rotatably mounted on carrier around main frame own axes, and main frame is cylindrical shape；Sensor mount, the sensor mount is for installing sensor to be put, the sensor mount and main frame are configured as: several sensors to be put can be made circumferentially to be mounted on sensor mount in array centered on main frame axis, sensor to be put can be made to be detached from from columnar main frame one end, and the relatively described carrier of disengaging configuration is fixed, keep multiple sensors to be put stable under high dummy status the purpose of this utility model is to provide a kind of, the barrel configuration that sensing system is launched for high-altitude that hold mode consistently persistently exports.
Description
Technical field
The utility model relates to high-altitudes to launch sensor field, especially a kind of to launch turning for sensing system for high-altitude
Barrel structure.
Background technique
With the development of science and technology, the region that the mankind are explored on earth is increasing.
A certain range of high-altitude is monitored now, needs to carry out cooperating using several falling sensors.
Currently, generally using two ways when launching the sensor of monitoring high-altitude situation:
1, the frame body of multiple sensors is loaded using one, the frame body is placed in cabin and is located at tail position, flies
After machine reaches object height, tail portion hatch door is opened, is sequentially output several falling sensors from the frame body of airplane tail group.
2, on the bottom of airframe (or even wing bottom, but will affect the energy supply of wing, all not use generally)
The slot (since number of sensors is more, the quantity of required slot also can be more) of multiple installation sensors, each slot are set
It is inside respectively mounted sensor (generally one or a set of), after aircraft reaches object height, the sensing in the slot of the fuselage bottom
Device pops up in order.
Both schemes are respectively present following defect:
1, launch process is too cumbersome, and aircraft, which needs to open tail portion hatch door just, can carry out the dispensing of sensor, also increases peace
Full hidden danger is usually all that special plane carries out sensor secondly, influencing the normal use of airplane tail group hatch door and tail portion cabin
It launches, too waste of resource.
2, multiple slots are set in the external of fuselage, will affect the intensity of fuselage, while also will affect in aircraft flight
Air-flow caused by outer surface increases safe hidden danger.
Currently, devising a kind of high-altitude for being able to solve above-mentioned 2 defects launches sensing system, but it is internal wait throw
The lasting output for putting sensor is a problem, because sensor needs constantly to export, (and output state must be kept as far as possible
Unanimously), while sensing system is launched due to being to be directly installed on aircraft exterior in the high-altitude, so space is limited, how to have
Multiple sensors to be put are stored in the space of limit, while guaranteeing their with can stably keeping state consistency lasting outputs,
It is urgent problem.
Utility model content
In view of the problems of the existing technology, the purpose of this utility model is to provide one kind to make multiple sensors to be put
Can under high dummy status stable, hold mode consistently persistently export for high-altitude launch sensing system rotating cylinder knot
Structure.
To achieve the goals above, the technical solution adopted in the utility model are as follows:
A kind of barrel configuration for launching sensing system for high-altitude,
Comprising:
Main frame, is arranged attachment device on the main frame, the attachment device can make main frame can around main frame from
Body axis are rotatably mounted on carrier, and main frame is cylindrical shape；
Sensor mount, the sensor mount for installing sensor to be put, the sensor mount with
And main frame is configured as: several sensors to be put can be made circumferentially to be mounted on biography in array centered on main frame axis
On sensor mounting portion, sensor to be put can be made to be detached from from columnar main frame one end, and the relatively described carrier of disengaging configuration
It is fixed.
It is in circle centered on main frame axis to several sensors to be put by the way that sensor mount is set as meeting
Week installs in array, while can be detached from from the fixed position of opposite carrier, and main frame is arranged around main frame own axes
Rotation, can be continuously and uninterruptedly from load under sensor circumference array arrangement to be put after then matching sensor and mounting portion
Body output, while output state is stablized, while can efficiently use limited space, secondly, being detached from fixed position, can make
The output hold mode of several sensors to be put is consistent, and monitoring data is more acurrate when using convenient for later period sensor to be put.
As a preferred embodiment of the present invention, the chamber of multiple installation sensors to be put is provided in the main frame
Body, the cavity circumferentially array centered on main frame axis.
As a preferred embodiment of the present invention, the axis of the cavity and the axis of main frame are parallel, make biography to be put
Sensor can preferably carry out subsequent movement when fixed position is detached from.
As a preferred embodiment of the present invention, the one end being detached from the main frame for sensor to be put, is provided with
Block is provided with the notch passed through for the sensor to be put on block, and block is not rotated with main frame, lacking on block
The relatively described carrier positions of mouth are fixed, and make the sensor to be put of non-fixed position will not be from master in the rotary course of main frame
The end of body frame drops out.
As a preferred embodiment of the present invention, the width of the cavity is adapted to single sensor to be put, convenient for subsequent
Guiding when sensor to be put exports.
As a preferred embodiment of the present invention, the more than two biographies to be put from beginning to end of the length adaptation of the cavity
Sensor, multiple sensors to be put are compiled as one group, and convenient for the acquisition of follow-up data, this setting can be same group wait throw
It puts sensor to be mounted in a cavity, convenient for being constantly detached from (output).The beneficial effects of the utility model are:
It is in circle centered on main frame axis to several sensors to be put by the way that sensor mount is set as meeting
Week installs in array, while can be detached from from the fixed position of opposite carrier, and main frame is arranged around main frame own axes
Rotation, can be continuously and uninterruptedly from load under sensor circumference array arrangement to be put after then matching sensor and mounting portion
Body output, while output state is stablized, while can efficiently use limited space, secondly, being detached from fixed position, can make
The output hold mode of several sensors to be put is consistent, and monitoring data is more acurrate when using convenient for later period sensor to be put.
Detailed description of the invention
Fig. 1 is the structural schematic diagram (depicting a matched transfer member 6) of the utility model；
Fig. 2 is the cross-sectional view of a certain position in the utility model middle section；
Fig. 3 is that the arrangement schematic diagram of sensor to be put after installing sensor to be put on the utility model (conceals portion
Separation structure)
Marked in the figure: 1- main frame, 2- sensor to be put, 3- cavity, 4- inner ring opening, 5- block, 51- notch, 6-
Transfer member, 7- carrier.
Specific embodiment
The utility model is described in further detail below with reference to embodiment and specific embodiment.But it should not be by this
The range for being interpreted as the above-mentioned theme of the utility model is only limitted to embodiment below, in all utility models based on the utility model
Hold realized technology and belongs to the scope of the utility model.
Embodiment 1
Such as Fig. 1-3, a kind of barrel configuration for launching sensing system for high-altitude,
Comprising:
Attachment device is arranged on the main frame 1 in main frame 1, and the attachment device can make main frame 1 can be around main frame
1 own axes are rotatably mounted on carrier 7, and main frame 1 is cylindrical shape；
Sensor mount, the sensor mount for installing sensor 2 to be put, the sensor mount with
And main frame 1 is configured as: several sensors to be put 2 can be made circumferentially to install in array centered on 1 axis of main frame
On sensor mount, sensor 2 to be put can be made to be detached from from columnar 1 one end of main frame, and disengaging configuration is with respect to institute
It is fixed to state carrier 7.
The cavity 3 (the i.e. described sensor mount) of multiple installation sensors 2 to be put is provided in the main frame 1,
The cavity 3 circumferentially array centered on 1 axis of main frame, the axis of the cavity 3 (institute parallel with the axis of main frame 1
1 exterior contour of main frame is stated as cylindrical shape, central axis also has a columnar space, i.e. main frame 1 is actually one
Between inner ring and outer rings, the cavity 3 is arranged in circular structure, and cavity 3 is class trapezoidal shape, only top and under
While being arc, in the present embodiment, cavity 3 is six, and equiangularly arranged with the central axis of main frame 1, the bottom of inner ring is provided with
Inner ring opening 4, inner ring opening 4 is longer in the axial direction of main frame 1, and both ends are connected to the both ends of main frame 1, is used for transfer member 6
When being mounted in inner ring, on transfer member 6 for push sensor 2 to be put part can pass through inner ring opening 4 with wait throw
The matching of sensor 2 is put, and the part for pushing sensor 2 to be put can be moved along inner ring 4 length directions of opening, it is real
The promotion of existing sensor 2 to be put), the width of the cavity 3 is adapted to single sensor 2 to be put, and the length of the cavity 3 is suitable
With more than two sensors to be put 2 from beginning to end, (in the present embodiment, the length compensation of cavity 3 is set as four tops of adaptation
The connected sensor 2 to be put of tail), the one end being detached from the main frame 1 for sensor 2 to be put is provided with block 5, keeps off
The notch 51 passed through for the sensor 2 to be put is provided on block 5, and block 5 is not rotated with main frame 1, lacking on block 5
51 relatively described 7 positions of carrier of mouth are fixed.
Claims (6)
1. a kind of barrel configuration that sensing system is launched for high-altitude,
It is characterised by comprising:
Attachment device is arranged on the main frame in main frame, and the attachment device can make main frame can be around main frame itself axis
Line is rotatably mounted on carrier, and main frame is cylindrical shape；
Sensor mount, the sensor mount is for installing sensor to be put, the sensor mount and master
Body frame is configured as: several sensors to be put can be made circumferentially to be mounted on sensor in array centered on main frame axis
On mounting portion, sensor to be put can be made to be detached from from columnar main frame one end, and the relatively described carrier of disengaging configuration is fixed.
2. the barrel configuration according to claim 1 for launching sensing system for high-altitude, which is characterized in that the main body
It is provided with the cavitys of multiple installations sensors to be put in frame, the cavity circumferentially array centered on main frame axis.
3. the barrel configuration according to claim 2 for launching sensing system for high-altitude, which is characterized in that the cavity
Axis it is parallel with the axis of main frame.
4. the barrel configuration according to claim 3 for launching sensing system for high-altitude, which is characterized in that the main body
The one end being detached from frame for sensor to be put, is provided with block, is provided with what the confession sensor to be put passed through on block
Notch, and block is not rotated with main frame, the relatively described carrier positions of the notch on block are fixed.
5. the barrel configuration according to claim 4 for launching sensing system for high-altitude, which is characterized in that the cavity
Width be adapted to single sensor to be put.
6. the barrel configuration according to claim 5 for launching sensing system for high-altitude, which is characterized in that the cavity
The more than two sensors to be put from beginning to end of length adaptation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822272709.3U CN209382280U (en) | 2018-12-29 | 2018-12-29 | The barrel configuration of sensing system is launched for high-altitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822272709.3U CN209382280U (en) | 2018-12-29 | 2018-12-29 | The barrel configuration of sensing system is launched for high-altitude |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209382280U true CN209382280U (en) | 2019-09-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822272709.3U Active CN209382280U (en) | 2018-12-29 | 2018-12-29 | The barrel configuration of sensing system is launched for high-altitude |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113184191A (en) * | 2021-03-31 | 2021-07-30 | 成都飞机工业（集团）有限责任公司 | Mandrel operation mechanism for high-altitude release of meteorological sonde |
-
2018
- 2018-12-29 CN CN201822272709.3U patent/CN209382280U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113184191A (en) * | 2021-03-31 | 2021-07-30 | 成都飞机工业（集团）有限责任公司 | Mandrel operation mechanism for high-altitude release of meteorological sonde |
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