CN203482690U - Artificial influence weather onboard dispenser - Google Patents
Artificial influence weather onboard dispenser Download PDFInfo
- Publication number
- CN203482690U CN203482690U CN201320543250.0U CN201320543250U CN203482690U CN 203482690 U CN203482690 U CN 203482690U CN 201320543250 U CN201320543250 U CN 201320543250U CN 203482690 U CN203482690 U CN 203482690U
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- flame bullet
- fixed mount
- flame
- horizontal
- gear
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Abstract
The utility model discloses an artificial influence weather onboard dispenser. The artificial influence weather onboard dispenser comprises a fixing supporting framework, a flame bomb rotating module and a driving unit, wherein the flame bomb rotating module is relatively rotatably installed in the fixing supporting framework, and the driving unit is used for driving the flame bomb rotating module to rotate relative to the fixing supporting framework. The artificial influence weather onboard dispenser can cooperate with an artificial precipitation plane operation business system to finish cold and warm catalytic operations, the flame bomb module of the dispenser can be rotated to a proper direction as required to send a flame bomb, and rapid and mass dispensing operations can be achieved.
Description
Technical field
The utility model relates to a kind of aircraft operation operation system of increasing rain artificially, and relates in particular to weather modification Airborne Dispenser.
Background technology
The aircraft operation operation system of increasing rain artificially is the working equipment of increasing rain artificially that integrates the functions such as the detection of sexual intercourse structure and acquisition of information, Application in Potential Prediction, operation command, Catalysis work, recruitment evaluation and informix demonstration, it can be, and enforcement is cold, warm cloud Catalysis work provides aerial platform, can be aerial work and effectively implement to provide ground monitoring and forecast supporting platform, can be operation effectiveness check Evaluation Platform is provided, being the emphasis equipment that the construction of the emergent professional contingent of weather modification is badly in need of, is effectively the carry out important support means of diversified task of professional contingent.
Cold, warm cloud Catalysis work function that dispensing device is used for realizing just, is transmitted and is communicated by letter by Air-Ground data, and comprehensive much information carries out orchestration, chooses effective job position and suitable activity duration, carries out the device of changes in temperature cloud seeding operation.
Utility model content
The purpose of this utility model is to be used to provide a kind of being arranged on aircraft drop in beam for carrying out the external hanging type dispensing device of artificial artificial rain operation.
The technical solution adopted in the utility model is: a kind of weather modification Airborne Dispenser, comprises fixed support framework, is installed on flame bullet rotating module in fixed support framework and driver element for driving flame bullet rotating module to rotate relative to fixed support framework rotatably;
Described fixed support framework is included in three horizontal large baffles and the horizontal small baffle of arranging in turn in the first horizontal direction, and for fixing the longitudinal beam extending along the first horizontal direction of all horizontal large baffles and horizontal small baffle, three horizontal large baffles are divided into two ends and the centre position of longitudinal beam, become front end, rear end and intermediate lateral large baffle, front installing zone between front end and intermediate lateral large baffle has at least one described horizontal small baffle, rear installing zone between centre and the horizontal large baffle in rear end has at least one described horizontal small baffle, on the outer surface of described longitudinal beam, be fixed with two and for the water chestnut with aircraft bottom, fall the water chestnut gripper shoe offseting, a hanger for being connected with aircraft drop in beam is set in each water chestnut gripper shoe,
Described flame bullet rotating module comprises the third and fourth flame bullet fixed mount that is positioned at the first and second flame bullet fixed mounts of front installing zone and is positioned at rear installing zone, in each flame bullet fixed mount, be provided with at least one flame bullet module, the two ends of the first and second flame bullet fixed mounts are installed on front end and intermediate lateral large baffle rotatably, in the middle of the two ends of the third and fourth flame bullet fixed mount are installed on rotatably and on the horizontal large baffle in rear end, the first and the 3rd flame bullet fixed mount is fixed together by a shaft coupling at intermediate lateral large baffle place, the second and the 4th flame bullet fixed mount is fixed together by another shaft coupling at intermediate lateral large baffle place, on the base plate of each flame bullet fixed mount, be provided with launch hole.
Preferably, on the outer surface of described fixed support framework, be covered with covering, described driver element is arranged in the radome fairing being fixedly connected with fixed support framework.
Preferably, described driver element comprise the motor that is installed in front installing zone, by the first gear of motor direct-drive, with the second gear of the first gear engagement and idle pulley, with the 3rd gear of idle pulley engagement, the first to the 3rd gear and idle pulley are all installed on the outer face of the horizontal large baffle of front end rotatably, it is connected described the first flame bullet fixed mount and the second gear limits in relative rotation, and it is connected the second flame bullet fixed mount and the 3rd gear limits in relative rotation.
Preferably, described the first flame bullet fixed mount and the second gear, and the second flame bullet fixed mount all limits it by key syndeton with the 3rd gear and is connected in relative rotation.
Preferably, in each flame bullet fixed mount, be provided with two flame bullet modules along the first horizontal direction parallel arranged.
Preferably, described longitudinal beam comprises that the cross section in the middle of being positioned at is the L-type beam that a T-shaped T-shaped beam and each two cross sections that minute are located at T-shaped beam both sides are L-type, and T-shaped beam and each L-type beam surround a curved surfaces.
The beneficial effects of the utility model are: dispensing device of the present utility model can coordinate the aircraft operation operation system of increasing rain artificially to complete cold, warm Catalysis work, the flame bullet module of this dispensing device can turn to suitable orientation as required launches, and can realize quick, heavy dose of operation that dispenses.Meanwhile, the utility model adopts modularization flame bullet modular structure, can realize quick-detachment and installation.
Accompanying drawing explanation
Fig. 1 is the overall appearance schematic diagram according to a kind of embodiment of weather modification Airborne Dispenser described in the utility model;
Fig. 2 is the front view of dispensing device shown in Fig. 1;
Fig. 3 is the vertical view of dispensing device shown in Fig. 1;
Fig. 4 is a kind of schematic perspective view of implementing structure of the fixed support framework of dispensing device shown in Fig. 1;
Fig. 5 shows a kind of interior schematic diagram of implementing structure of dispensing device shown in Fig. 1;
Fig. 6 shows the flame bullet rotating module of dispensing device shown in Fig. 1;
Fig. 7 shows the flame bullet module of the bullet of flame shown in Fig. 6 rotating module.
Embodiment
As shown in Fig. 1 to 7, weather modification Airborne Dispenser of the present utility model comprises fixed support framework 1, is installed on flame bullet rotating module 3 in fixed support framework 1 and driver element 2 for driving flame bullet rotating module 3 to rotate relative to fixed support framework 1 rotatably.On the outer surface of this fixed support framework 1, be covered with covering 4, driver element 2 can be installed in the radome fairing 5 being fixedly connected with fixed support framework 1.
As shown in Figures 4 and 5, this fixed support framework 1 can be included in horizontal large baffle and the horizontal small baffle 13 of arranging in turn in the first horizontal direction, and for fixing the longitudinal beam extending along the first horizontal direction of all horizontal large baffles and horizontal small baffle 13, three horizontal large baffles are divided into two ends and the centre position of longitudinal beam, become front end, rear end and intermediate lateral large baffle 11a, 11c and 11b, rear installing zone between front installing zone between the horizontal large baffle 11a of front end and intermediate lateral large baffle 11b and intermediate lateral large baffle 11b and the horizontal large baffle 11c in rear end respectively has two horizontal small baffles 13 in the present embodiment, on the outer surface of longitudinal beam, be fixed with two and for the water chestnut with aircraft bottom, fall the water chestnut gripper shoe 16 offseting, to prevent that dispensing device from rocking, a hanger 14 for being connected with aircraft drop in beam is set in each water chestnut gripper shoe 16, this hanger 14 exposes by covering 4.
Above longitudinal beam can comprise that the cross section in the middle of being positioned at is the L-type beam 15 that a T-shaped T-shaped beam 12 and each two cross sections that minute are located at T-shaped beam 12 both sides are L-type, and T-shaped beam 12 surrounds a curved surfaces with each L-type beam 15, to reduce air drag.
As Fig. 5, shown in 6 and 7, flame bullet rotating module 3 is installed on the below of horizontal small baffle 13, it comprises the first and second flame bullet fixed mount 31a that are positioned at front installing zone, 31b and be positioned at the third and fourth flame bullet fixed mount 31c of rear installing zone, 31d, in each flame bullet fixed mount 31, be provided with at least one flame bullet module 32, the first and second flame bullet fixed mount 31a, the two ends of 31b are installed on front end and intermediate lateral large baffle 11a rotatably, on 11b, the third and fourth flame bullet fixed mount 31c, the two ends of 31d are installed on middle and the horizontal large baffle 11b in rear end rotatably, on 11c, the first and the 3rd flame bullet fixed mount 31a, 31c is fixed together by a shaft coupling at intermediate lateral large baffle 11b place, the second and the 4th flame bullet fixed mount 31b, 31d is fixed together by another shaft coupling at intermediate lateral large baffle 11b place, make the first and the 3rd flame bullet fixed mount 31a, 31c can synchronously rotate, the second and the 4th flame bullet fixed mount can synchronously rotate, on the base plate of each flame bullet fixed mount 31, be provided with the launch hole 311 for flame is launched out, by horizontal small baffle 13, can limit the slewing area of flame bullet fixed mount 31, and then the emission angle of restriction flame bullet.
The first and the 3rd flame bullet fixed mount rotates along contrary direction with the second and the 4th flame bullet fixed mount in the present embodiment, therefore, as shown in Figure 5, driver element 2 can comprise the motor 21 being installed in front installing zone, the first gear 22 directly being driven by motor 21, the second gear 24 and idle pulley 23 with the first gear 22 engagements, the 3rd gear 25 with idle pulley 23 engagements, the first to the 3rd gear and idle pulley are all installed on the outer face of the horizontal large baffle 11a of front end rotatably, the first flame bullet fixed mount 31a is for example by key syndeton, to limit it to be connected in relative rotation with the second gear 24, the second flame bullet fixed mount 31b is for example also by key syndeton, to limit it to be connected in relative rotation with the 3rd gear 25.
In the present embodiment, be provided with two flame bullet modules 32 along the first horizontal direction parallel arranged in each flame bullet fixed mount 31, each flame bullet module 32 can comprise it being for example 50 flame bullets, flame cartridge box body, wiring board and baffle.
The foregoing is only preferably embodiment of the utility model, be not used for limiting practical range of the present utility model, the equivalence of in every case doing in protection domain of the present utility model changes and modifies, and all should think and fall in protection domain of the present utility model.
Claims (6)
1. a weather modification Airborne Dispenser, is characterized in that: comprise fixed support framework, be installed on flame bullet rotating module in fixed support framework and driver element for driving flame bullet rotating module to rotate relative to fixed support framework rotatably;
Described fixed support framework is included in three horizontal large baffles and the horizontal small baffle of arranging in turn in the first horizontal direction, and for fixing the longitudinal beam extending along the first horizontal direction of all horizontal large baffles and horizontal small baffle, three horizontal large baffles are divided into two ends and the centre position of longitudinal beam, become front end, rear end and intermediate lateral large baffle, front installing zone between front end and intermediate lateral large baffle has at least one described horizontal small baffle, rear installing zone between centre and the horizontal large baffle in rear end has at least one described horizontal small baffle, on the outer surface of described longitudinal beam, be fixed with two and for the water chestnut with aircraft bottom, fall the water chestnut gripper shoe offseting, a hanger for being connected with aircraft drop in beam is set in each water chestnut gripper shoe,
Described flame bullet rotating module is installed on the below of horizontal small baffle, described flame bullet rotating module comprises the third and fourth flame bullet fixed mount that is positioned at the first and second flame bullet fixed mounts of front installing zone and is positioned at rear installing zone, in each flame bullet fixed mount, be provided with at least one flame bullet module, the two ends of the first and second flame bullet fixed mounts are installed on front end and intermediate lateral large baffle rotatably, in the middle of the two ends of the third and fourth flame bullet fixed mount are installed on rotatably and on the horizontal large baffle in rear end, the first and the 3rd flame bullet fixed mount is fixed together by a shaft coupling at intermediate lateral large baffle place, the second and the 4th flame bullet fixed mount is fixed together by another shaft coupling at intermediate lateral large baffle place, on the base plate of each flame bullet fixed mount, be provided with launch hole.
2. weather modification Airborne Dispenser according to claim 1, is characterized in that: on the outer surface of described fixed support framework, be covered with covering, described driver element is arranged in the radome fairing being fixedly connected with fixed support framework.
3. weather modification Airborne Dispenser according to claim 1, it is characterized in that: described driver element comprise the motor that is installed in front installing zone, by the first gear of motor direct-drive, with the second gear of the first gear engagement and idle pulley, with the 3rd gear of idle pulley engagement, the first to the 3rd gear and idle pulley are all installed on the outer face of the horizontal large baffle of front end rotatably, it is connected described the first flame bullet fixed mount and the second gear limits in relative rotation, and it is connected the second flame bullet fixed mount and the 3rd gear limits in relative rotation.
4. weather modification Airborne Dispenser according to claim 3, is characterized in that: described the first flame bullet fixed mount and the second gear, and the second flame bullet fixed mount all limits it by key syndeton with the 3rd gear and is connected in relative rotation.
5. according to the weather modification Airborne Dispenser described in any one in claim 1 to 4, it is characterized in that: in each flame bullet fixed mount, be provided with two flame bullet modules along the first horizontal direction parallel arranged.
6. according to the weather modification Airborne Dispenser described in any one in claim 1 to 4, it is characterized in that: described longitudinal beam comprises that the cross section in the middle of being positioned at is the L-type beam that a T-shaped T-shaped beam and each two cross sections that minute are located at T-shaped beam both sides are L-type, and T-shaped beam and each L-type beam surround a curved surfaces.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320543250.0U CN203482690U (en) | 2013-09-03 | 2013-09-03 | Artificial influence weather onboard dispenser |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320543250.0U CN203482690U (en) | 2013-09-03 | 2013-09-03 | Artificial influence weather onboard dispenser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203482690U true CN203482690U (en) | 2014-03-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320543250.0U Expired - Fee Related CN203482690U (en) | 2013-09-03 | 2013-09-03 | Artificial influence weather onboard dispenser |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203482690U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105423815A (en) * | 2015-11-28 | 2016-03-23 | 内蒙古北方保安民爆器材有限公司 | Onboard flame cannonball launcher |
| CN106043700A (en) * | 2016-06-24 | 2016-10-26 | 河南沃野智能科技有限公司 | Artificial rainfall aircraft and method |
-
2013
- 2013-09-03 CN CN201320543250.0U patent/CN203482690U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105423815A (en) * | 2015-11-28 | 2016-03-23 | 内蒙古北方保安民爆器材有限公司 | Onboard flame cannonball launcher |
| CN105423815B (en) * | 2015-11-28 | 2017-03-22 | 内蒙古北方保安民爆器材有限公司 | Onboard flame cannonball launcher |
| CN106043700A (en) * | 2016-06-24 | 2016-10-26 | 河南沃野智能科技有限公司 | Artificial rainfall aircraft and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20140319 Termination date: 20160903 |