CN210000589U - pod type airborne dropsonde throwing device - Google Patents
pod type airborne dropsonde throwing device Download PDFInfo
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- CN210000589U CN210000589U CN201920760236.3U CN201920760236U CN210000589U CN 210000589 U CN210000589 U CN 210000589U CN 201920760236 U CN201920760236 U CN 201920760236U CN 210000589 U CN210000589 U CN 210000589U
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- sonde
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Abstract
The utility model discloses a hanging cabin formula machine carries and drops sonde input device relates to meteorological technical field, including the nacelle, cabin has been seted up to nacelle back end bottom, the nacelle outside is equipped with the sounding receiving antenna, be equipped with the machine in the nacelle and carry the receiver, the nacelle controller, sonde transport mechanism and sonde push mechanism, the machine carries the receiver and gives the nacelle controller with signal transmission after receiving the signal of sonde, signal controller control sonde transport mechanism, the work of sonde push mechanism, thereby with sonde propelling movement cabin , thereby realize the input of sonde.
Description
Technical Field
The utility model relates to a meteorological technical field specifically is kinds of pod formula machine carries and throws sonde and put in device down.
Background
At present, the common launching mode of the sonde is mainly a ground ball-borne launching mode, and the sounding method cannot be used for sounding observation of special observation targets (areas) such as typhoons, disaster areas and the like in areas such as oceans (open sea), mountain areas and the like.
The airborne downward-throwing sounding uses a manned airplane (or unmanned aerial vehicle) with high maneuverability as a platform, when the flying platform arrives at a target observation area, the downward-throwing sounding instruments are sequentially ejected out of a cabin from high altitude, and sounding data transmitted back by the downward-throwing sounding instruments in a wireless mode are received to obtain meteorological element data such as temperature, humidity, air pressure, wind direction, wind speed and the like in the process of the sounding instruments from the flying height to the ground (sea surface), which is the most important of the most important and most effective airborne direct observation load.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide kinds of pod formula machine carries and drops sonde input device to current dropsonde input exists the operation degree of difficulty great under the solution machine carries the environment, and is high to staff's operation technical requirement, and the precision is lower, receives the great technical problem of weather effect.
In order to solve the technical problem, the utility model provides an kind of nacelle formula machine carries and throws sonde input device down, including the nacelle, cabin has been seted up to nacelle back end bottom, the nacelle outside is equipped with the receiving antenna that visits, be equipped with in the nacelle:
the airborne receiver is arranged at the front section in the nacelle and is in signal connection with the sounding receiving antenna;
the nacelle controller is arranged at the rear section in the nacelle and is in signal connection with the airborne receiver;
the sonde transmission mechanism is arranged at the middle section in the nacelle and is in signal connection with the nacelle controller;
and the sonde pushing mechanisms are arranged at the middle section and the rear section of the bottom in the nacelle, the outlets of the sonde pushing mechanisms are positioned at the cabin , and the sonde pushing mechanisms are in signal connection with the nacelle controller.
Preferably, the sonde push mechanism comprises a throwing channel, an electromagnet, a push rod and a spring, wherein the electromagnet, the push rod and the spring are arranged in the throwing channel, the push rod penetrates through the electromagnet, the spring is sleeved outside the push rod behind the electromagnet, and the push rod moves towards the cabin when the electromagnet is electrified and stretches the spring.
Preferably, a nacelle lifting lug is arranged at the top of the outer side of the nacelle and is positioned in the middle section of the nacelle.
Preferably, the nacelle outer top is also provided with a nacelle electrical interface which is positioned at the rear section of the nacelle and is electrically connected with the nacelle controller.
Preferably, the outer side of the nacelle is fully paved with layers of heat insulation.
Preferably, the pod controller comprises an electric heating control part, a motor control part and a temperature monitoring part, the electric heating control part is electrically connected with the heat insulation layer, the motor control part is electrically connected with the sonde conveying mechanism and the sonde pushing mechanism, and the temperature monitoring part is electrically connected with the heat insulation layer and the temperature sensor.
Preferably, the sounding receiving antenna is located at the rear section outside the nacelle.
Preferably, the front half section of the sonde pushing mechanism is located at the middle section of the nacelle, and the rear half section of the sonde pushing mechanism is located at the rear section of the nacelle.
Compared with the prior art, the utility model discloses a characteristics and beneficial effect do, the utility model discloses a set up machine-carried receiver, nacelle controller, sonde transport mechanism, sonde push mechanism in the nacelle among the nacelle formula machine-carried lower drop sonde jettison device, sonde transport mechanism is used for storing the sonde, and sonde push mechanism is used for going out the cabin with the sonde propelling movement, machine-carried receiver sends the signal to the nacelle controller after receiving the signal of sonde, and signal controller control sonde transport mechanism, the work of sonde push mechanism to with sonde propelling movement out cabin , thereby realize the input of sonde.
Drawings
Fig. 1 is a schematic structural diagram of a pod type airborne dropsonde launching device.
Fig. 2 is a schematic structural diagram of a sonde pushing mechanism.
Fig. 3 is a working principle diagram of the pod type airborne dropsonde launching device.
The attached drawing labels are 1-pod, 2-pod lifting lug, 4-sonde receiving antenna, 5-airborne receiver, 6-pod controller, 8-sonde, 9-sonde transmission mechanism, 10-sonde pushing mechanism, 101-throwing channel, 102-electromagnet, 103-push rod, 104-spring, 11-cabin , 12-heat insulation layer and 13-pod electrical interface.
Detailed Description
In order to make the technical means, innovative features, objectives and functions realized by the present invention easily understood, the present invention will be described in .
The embodiments described herein are specific embodiments of the present invention, and are intended to be illustrative of the concepts of the present invention, which are intended to be illustrative and exemplary, and should not be construed as limiting the scope of the embodiments of the present invention. In addition to the embodiments described herein, those skilled in the art will be able to employ other technical solutions which are obvious based on the disclosure of the claims and the specification of the present application, and these technical solutions include technical solutions which make any obvious replacement or modification for the embodiments described herein.
As shown in fig. 1 for kinds of pod type airborne dropsonde putting devices, including nacelle 1. the utility model discloses a pod type airborne dropsonde putting device contains two nacelles 1, can carry a plurality of pieces of sondes 8, can put into quantity to different aircraft platform load capacity adjustment sondes 8 for different aircraft platforms throw out sondes 8 as much as possible in target putting observation region, optimize the flight observation task, save flight resources.
The nacelle 1 is divided into a front section, a middle section and a rear section, the middle section of the nacelle is cylindrical, cowlings of the front section and the rear section of the nacelle 1 are of a shape-preserving structure so as to reduce the influence on the flight performance of an airplane, a cabin 11 is arranged at the bottom of the rear section of the nacelle 1, an aerial sounding receiving antenna 4 is arranged on the outer side of the nacelle 1, the aerial sounding receiving antenna 4 is located at the rear section of the outer side of the nacelle 1, the aerial sounding receiving antenna 4 receives wireless signals sent by an aerial sonde 8, in order to ensure a sufficient reflection area, a whip antenna insensitive to a reflection surface is selected as the aerial sounding receiving antenna 4, and layers of heat preservation layers 12 are fully paved on the outer side of the nacelle 1 so as to provide a heat preservation environment for normal work.
The top of the outer side of the nacelle 1 is provided with a nacelle lifting lug 2, and the nacelle lifting lug 2 is positioned in the middle section of the nacelle 1. The nacelle lifting lugs 2 are two, and the nacelle lifting lugs 2 are located on two sides of the gravity center of the nacelle 1 and connected with a nacelle hanging rack mounted on the lower surface of the wing, so that the nacelle type airborne dropsonde launching device can be suitable for various airplane platforms using standard wing nacelle hanging racks.
The outer top of the nacelle 1 is also provided with a nacelle electrical interface 13, the nacelle electrical interface 13 is positioned at the rear section of the nacelle 1, and the nacelle electrical interface 13 is electrically connected with the nacelle controller 6. The nacelle electrical interface 13 is connected to terminals on the underside of the aircraft wing for connecting the aircraft platform to nacelle data and command communication electrical signals, as well as for powering the nacelle 1.
An airborne receiver 5, a pod controller 6, a sonde transmission mechanism 9 and a sonde pushing mechanism 10 are arranged in the pod 1.
An airborne receiver 5 is arranged at the front section in the nacelle 1, and the airborne receiver 5 is in signal connection with a sonde 8 and a sonde receiving antenna 4. The airborne receiver 5 is a main communication node of the pod type airborne dropsonde launching device, and mainly has the functions of receiving and demodulating wireless signals sent by the launched sondes 8 and transmitting decoded data to an aircraft platform.
The nacelle controller 6 is arranged at the rear section in the nacelle 1, the nacelle controller 6 is in signal connection with the onboard receiver 5, the nacelle controller 6 is connected with the onboard receiver 5 through a serial communication cable and a power supply cable, the nacelle controller 6 is connected with a nacelle electrical interface 13, power supply inside the nacelle is distributed by a nacelle controller 6 system , and a system is in data and command communication with an aircraft platform, the nacelle 1 is connected with terminals below the wings of the aircraft through the nacelle electrical interface 13, the connection content comprises a nacelle power supply source and data and command communication links of the nacelle and the aircraft platform, and the nacelle controller 6 receives commands of launching a sonde sent by the aircraft platform, reporting the state of the nacelle and the like and is responsible for controlling the internal work of the whole nacelle.
The pod controller 6 comprises an electric heating control part, a motor control part and a temperature monitoring part, the electric heating control part is electrically connected with the heat insulation layer 12, the motor control part is electrically connected with the sonde conveying mechanism 9 and the sonde pushing mechanism 10, and the temperature monitoring part is electrically connected with the heat insulation layer 12 and the temperature sensor. The pod controller 6 controls the heat-insulating layer 12 to heat, controls the sonde conveying mechanism 9 and the sonde pushing mechanism 10 to work, monitors whether faults occur or not and uploads results to the airplane platform.
The sonde conveying mechanism 9 is arranged in the middle section in the nacelle 1, the sonde 8 is stored in the sonde conveying mechanism 9, and the sonde conveying mechanism 9 is in signal connection with the nacelle controller 6. The sonde conveying mechanism 9 is used for storing the sondes 8 and sequentially conveying the sondes 8 to the sonde pushing mechanism 10 in a mechanical transmission mode. The sonde delivery mechanism 9 is controlled by a servo motor, and an encoder is used as feedback, so that the sonde delivery mechanism can accurately act mechanically and can accurately send the sonde 8 into a launching position.
The sonde pushing mechanism 10 is arranged in the middle section and the rear section of the bottom in the nacelle 1, the outlet of the sonde pushing mechanism 10 is located in the cabin 11, the sonde pushing mechanism 10 is in signal connection with the nacelle controller 6, the first half section of the sonde pushing mechanism 10 is located in the middle section of the nacelle 1, and the rear half section of the sonde pushing mechanism 10 is located in the rear section of the nacelle 1.
As shown in fig. 2, the sonde push mechanism 10 includes a throwing channel 101, and an electromagnet 102, a push rod 103 and a spring 104 which are arranged in the throwing channel 101, wherein the push rod 103 passes through the electromagnet 102, the spring 104 is sleeved outside the push rod 103 behind the electromagnet 102, the push rod 103 moves towards the cabin 11 when the electromagnet 102 is powered on, and the spring 104 is stretched.
As shown in fig. 3, when the pod type airborne sonde launching device works, an unmanned aerial vehicle flies to a predetermined airspace, an aircraft platform sends a launching command to a pod controller 6 when the aircraft reaches a launching point of a launching observation area according to a preset program, after the pod controller 6 receives the launching command, a sonde transmission mechanism 9 transports an internally stored sonde 8 to a sonde pushing mechanism 10, after the airborne receiver 5 confirms the state of the launch sonde, the pod controller 6 sends the launching command to the sonde pushing mechanism 10, after the sonde pushing mechanism 10 receives the launching command, the sonde 8 to be launched is launched into the air at a fixed initial speed of , after the sonde 8 is separated from the pod, an umbrella carried by the aircraft is opened, slowly descends at a stable posture until reaching the sea ground, and in the descending process, the sonde 8 detects atmospheric falling temperature, humidity, air pressure, wind direction, wind speed and other elements in the atmosphere, returns detection data to the pod 5 in a wireless mode, receives the airborne antenna 5, sends the detection data to the airborne receiver 4, and decodes the airborne data, and sends the detection data to the airborne receiver 8, and decodes the airborne data.
The above embodiments are merely illustrative of the preferred embodiments of the present invention, and are not intended to limit the scope of the present invention, and various modifications and improvements made by those skilled in the art without departing from the spirit of the present invention should fall within the protection scope defined by the claims.
Claims (8)
1, kind of pod formula machine carries and throws sonde jettison device down, includes nacelle (1), cabin (11) have been seted up to nacelle (1) back end bottom, the nacelle (1) outside is equipped with and visits sky receiving antenna (4), its characterized in that is equipped with in nacelle (1):
the airborne receiver (5) is arranged at the front section in the nacelle (1), and the airborne receiver (5) is in signal connection with the sounding receiving antenna (4);
the nacelle controller (6) is arranged at the rear section in the nacelle (1), and the nacelle controller (6) is in signal connection with the airborne receiver (5);
the sonde transmission mechanism (9) is arranged in the middle section in the nacelle (1), and the sonde transmission mechanism (9) is in signal connection with the nacelle controller (6);
the sonde pushing mechanism (10) is arranged at the middle section and the rear section of the bottom in the nacelle (1), the outlet of the sonde pushing mechanism (10) is located at the cabin (11), and the sonde pushing mechanism (10) is in signal connection with the nacelle controller (6).
2. The pod type airborne sonde launch apparatus according to claim 1 wherein the sonde propelling mechanism (10) includes a launch path (101) and an electromagnet (102), a push rod (103) and a spring (104) disposed in the launch path (101), the push rod (103) passes through the electromagnet (102), the spring (104) is sleeved outside the push rod (103) behind the electromagnet (102), the push rod (103) moves in the direction of the (11) when the electromagnet (102) is energized, and the spring (104) stretches.
3. The kind of pod type airborne sonde launch apparatus according to claim 1, characterized in that a pod lifting lug (2) is provided on the top of the outer side of the pod (1), and the pod lifting lug (2) is located in the middle section of the pod (1).
4. The kind of pod type airborne sonde launch apparatus according to claim 1, characterized in that a pod electrical interface (13) is further provided on the top outside the pod (1), the pod electrical interface (13) is located on the rear section of the pod (1), and the pod electrical interface (13) is electrically connected with the pod controller (6).
5. The launch device of kinds of pod type airborne dropsondes according to claim 1, characterized in that layers of insulating layer (12) are laid outside the pod (1).
6. The pod type airborne sonde launch apparatus according to claim 5, wherein the pod controller (6) includes an electrical heating control section, a motor control section and a temperature monitoring section, the electrical heating control section is electrically connected to the heat insulating layer (12), the motor control section is electrically connected to both the sonde transfer mechanism (9) and the sonde push mechanism (10), and the temperature monitoring section is electrically connected to both the heat insulating layer (12) and the temperature sensor.
7. The launch device of kinds of pod-type airborne downlroking sondes according to claim 1, wherein the sonde receiving antenna (4) is located at the rear section of the outer side of the pod (1).
8. The kinds of nacelle type airborne sonde launch apparatus according to claim 1, wherein the front half of the sonde propelling mechanism (10) is located at the middle section of the nacelle (1), and the rear half of the sonde propelling mechanism (10) is located at the rear section of the nacelle (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920760236.3U CN210000589U (en) | 2019-05-24 | 2019-05-24 | pod type airborne dropsonde throwing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920760236.3U CN210000589U (en) | 2019-05-24 | 2019-05-24 | pod type airborne dropsonde throwing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210000589U true CN210000589U (en) | 2020-01-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920760236.3U Active CN210000589U (en) | 2019-05-24 | 2019-05-24 | pod type airborne dropsonde throwing device |
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| Country | Link |
|---|---|
| CN (1) | CN210000589U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824426A (en) * | 2020-06-15 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Pod appearance structure for launching dropsonde |
| CN115675869A (en) * | 2023-01-03 | 2023-02-03 | 中国人民解放军海军工程大学 | Marine hydrology detection instrument launching device and launching and detection method |
-
2019
- 2019-05-24 CN CN201920760236.3U patent/CN210000589U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824426A (en) * | 2020-06-15 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Pod appearance structure for launching dropsonde |
| CN115675869A (en) * | 2023-01-03 | 2023-02-03 | 中国人民解放军海军工程大学 | Marine hydrology detection instrument launching device and launching and detection method |
| CN115675869B (en) * | 2023-01-03 | 2023-04-07 | 中国人民解放军海军工程大学 | Marine hydrology detection instrument launching device and launching and detection method |
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