CN214084763U - Investigation and attack integrated flying patrol device - Google Patents
Investigation and attack integrated flying patrol device Download PDFInfo
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- CN214084763U CN214084763U CN202022413065.2U CN202022413065U CN214084763U CN 214084763 U CN214084763 U CN 214084763U CN 202022413065 U CN202022413065 U CN 202022413065U CN 214084763 U CN214084763 U CN 214084763U
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Abstract
A reconnaissance and striking integrated flight inspection device comprises a power cabin, a flight control navigation cabin, a fuel oil cabin, a mission load cabin, wings and a tail wing; the power cabin, the flight control navigation cabin, the fuel oil cabin and the task load cabin are sequentially connected to form a fuselage structure, and the wings are arranged below the fuselage structure and connected with the fuselage structure through a folding mechanism; the empennage is connected to the side surface of the machine body structure through a folding mechanism. The utility model discloses patrol and fly the ware and carry optics investigation task load and great oil tank, can patrol and fly or spiral and carry out long-time investigation to the target area, simultaneously, should patrol and fly the ware and carry the load of warhead, can implement the strike to the target fast after the discovery target. Can realize simultaneously that the investigation and the attack to the target task carry a large amount of fuel, improve the flight time of patrolling the flight ware, and then can effectual increase radius of operation and investigation time.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, in particular to investigation and strike integration patrols and flies ware.
Background
Because rotor unmanned aerial vehicle flying speed is slow, can't implement reconnaissance and quick striking to maneuvering target, even if to the fixed target in ground, because its flying speed is slow, so also can give the longer preparation time of adversary to delay the wrong fighter. Simultaneously, rotor unmanned aerial vehicle can't carry the great task load of weight, so when attacking large-scale target, also be keenly powerless.
Missiles, while carrying a relatively heavy warhead and performing attack missions on moving and fixed targets, cannot perform reconnaissance missions. Therefore, if only the target is known to be present in a specific area, and the target is hidden and occasionally moves out, the missile cannot hover for a long time for detection and waits for the target to attack again.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a investigation and strike integration and patrol and fly ware to solve above-mentioned problem.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a reconnaissance and striking integrated flight inspection device comprises a power cabin, a flight control navigation cabin, a fuel oil cabin, a mission load cabin, wings and a tail wing; the power cabin, the flight control navigation cabin, the fuel oil cabin and the task load cabin are sequentially connected to form a fuselage structure, and the wings are arranged below the fuselage structure and connected with the fuselage structure through a folding mechanism; the empennage is connected to the side surface of the machine body structure through a folding mechanism.
Further, the power cabin comprises an engine and a battery, and the engine is connected with the fuel oil cabin.
Furthermore, the flight control navigation cabin comprises a flight control and a data link, wherein the flight control is used for flight control, and the data link is used for transmitting data.
Further, an oil tank is arranged in the fuel oil cabin; a battle loading part is arranged in the mission loading cabin.
Furthermore, the mission load cabin is the front part, the wings arranged below the fuselage structure are front and rear tandem wings, the extension length of the front wing is less than or equal to that of the rear wing, and the folding directions of the front wing and the rear wing are opposite.
Further, the rear wing can be folded forward by a folding mechanism.
Further, an optical detection camera is further arranged below the machine body structure and connected with the flight control navigation cabin.
Compared with the prior art, the utility model discloses there is following technological effect:
the utility model discloses patrol and fly the ware and carry optics investigation task load and great oil tank, can patrol and fly or spiral and carry out long-time investigation to the target area, simultaneously, should patrol and fly the ware and carry the load of warhead, can implement the strike to the target fast after the discovery target. Can realize simultaneously that the investigation and the attack to the target task carry a large amount of fuel, improve the flight time of patrolling the flight ware, and then can effectual increase radius of operation and investigation time.
Drawings
FIG. 1 is an overall structure diagram of the present invention;
fig. 2 is a perspective view of the present invention.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings:
referring to fig. 1 and 2, a reconnaissance and striking integrated flight inspection device comprises a power cabin 1, a flight control navigation cabin 2, a fuel oil cabin 3, a mission load cabin 4, wings and a tail wing; the power cabin 1, the flight control navigation cabin 2, the fuel oil cabin 3 and the task load cabin 4 are sequentially connected to form a fuselage structure, and the wings are arranged below the fuselage structure and connected with the fuselage structure through a folding mechanism; the empennage is connected to the side surface of the machine body structure through a folding mechanism.
The power compartment 1 comprises an engine 11 and a battery 10, the engine being connected to a fuel compartment.
The flight control navigation capsule 2 comprises a flight control 8 for flight control and a data link 9 for data transmission.
An oil tank 7 is arranged in the fuel oil cabin 3; a battle loading part 5 is arranged in the mission loading chamber 4.
The mission load cabin 4 is the front part, the wings arranged below the fuselage structure are front and rear tandem wings, the extension length of the front wing is less than or equal to that of the rear wing, and the folding directions of the front wing and the rear wing are opposite.
The tail wing can be folded forwards through a folding mechanism.
An optical investigation camera 6 is further arranged below the machine body structure and connected with the flight control navigation cabin 2.
The flight patrol device consists of a body structure, a power system, a flight control navigation system and a task load system, and can carry out investigation and attack on a target when cruising and flying to a target area after being launched. The aircraft body mechanism of the flight patrol device comprises an aircraft body, wings and a tail wing. The fuselage is divided into a mission load cabin, a fuel oil cabin, a navigation control cabin and a power cabin along the longitudinal direction, and the bulkhead sections are separated by a baffle plate inside the fuselage. The wings are connected with the fuselage through a folding mechanism, the wings are front and rear tandem wings and are arranged on the lower part of the fuselage, the extension length of the front wings is less than or equal to that of the rear wings, when the front wings are stored or transported, the front wings are folded backwards to be parallel to the fuselage, the rear wings are folded forwards to be parallel to the fuselage, and after the cruise device is launched, the front wings and the rear wings are unfolded to be perpendicular to the fuselage. The empennage is connected with the fuselage through a folding mechanism, mainly comprises vertical tails on two sides of the fuselage, and is folded forwards on two sides of the fuselage during storage or transportation and unfolded during flight. The power system mainly comprises an engine, an oil tank and a battery, which are respectively fixed on a baffle plate inside the machine body. The flight control navigation system consists of flight control and a data link which are respectively fixed on a baffle inside the airplane body. The mission load comprises an optical investigation load and a warhead load, the optical investigation load is arranged at the lower part of the machine body and mainly used for carrying out investigation and monitoring missions, and the warhead is arranged in the mission load cabin and is fixed on a baffle plate in the machine body through screws and mainly used for carrying out attack missions.
Claims (7)
1. A reconnaissance and striking integrated flight inspection device is characterized by comprising a power cabin (1), a flight control navigation cabin (2), a fuel oil cabin (3), a mission load cabin (4), wings and a tail wing; the power cabin (1), the flight control navigation cabin (2), the fuel oil cabin (3) and the task load cabin (4) are sequentially connected to form a fuselage structure, and the wings are arranged below the fuselage structure and connected with the fuselage structure through a folding mechanism; the empennage is connected to the side surface of the machine body structure through a folding mechanism.
2. A reconnaissance and percussion integrated cruise device according to claim 1, wherein the power compartment (1) comprises an engine (11) and a battery (10), and the engine is connected with the fuel compartment.
3. A reconnaissance and percussion integrated patrol aircraft according to claim 1, wherein the flight control navigation cabin (2) comprises a flight control (8) and a data link (9), the flight control is used for flight control, and the data link is used for data transmission.
4. The investigation and striking integrated patrol aircraft according to claim 1, wherein an oil tank (7) is arranged in the fuel oil cabin (3); a battle loading part (5) is arranged in the mission loading cabin (4).
5. The investigation and striking integrated patrol aircraft according to claim 1, wherein the mission load cabin (4) is a front part, the wings arranged below the fuselage structure are front and rear tandem wings, the extension length of the front wing is less than or equal to that of the rear wing, and the folding directions of the front and rear wings are opposite.
6. The integrated reconnaissance and percussion patrolling device according to claim 5, wherein the tail wing can be folded forwards by a folding mechanism.
7. The investigation and striking integrated patrol aircraft according to claim 1, wherein an optical investigation camera (6) is further arranged below the aircraft body structure, and is connected with the flight control navigation cabin (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022413065.2U CN214084763U (en) | 2020-10-26 | 2020-10-26 | Investigation and attack integrated flying patrol device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022413065.2U CN214084763U (en) | 2020-10-26 | 2020-10-26 | Investigation and attack integrated flying patrol device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214084763U true CN214084763U (en) | 2021-08-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022413065.2U Active CN214084763U (en) | 2020-10-26 | 2020-10-26 | Investigation and attack integrated flying patrol device |
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| Country | Link |
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| CN (1) | CN214084763U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113602499A (en) * | 2021-09-15 | 2021-11-05 | 尚之灏 | Multipurpose attack and transportation integrated aircraft |
-
2020
- 2020-10-26 CN CN202022413065.2U patent/CN214084763U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113602499A (en) * | 2021-09-15 | 2021-11-05 | 尚之灏 | Multipurpose attack and transportation integrated aircraft |
| CN113602499B (en) * | 2021-09-15 | 2023-09-19 | 尚之灏 | Multipurpose attack transportation integrated aircraft |
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