CN116588371A - Patrol aircraft separation guiding device and patrol aircraft assembly - Google Patents
Patrol aircraft separation guiding device and patrol aircraft assembly Download PDFInfo
- Publication number
- CN116588371A CN116588371A CN202310845395.4A CN202310845395A CN116588371A CN 116588371 A CN116588371 A CN 116588371A CN 202310845395 A CN202310845395 A CN 202310845395A CN 116588371 A CN116588371 A CN 116588371A
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- cabin
- patrol
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- aircraft
- parachute
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- 238000000926 separation method Methods 0.000 title claims abstract description 26
- 238000004880 explosion Methods 0.000 claims abstract description 36
- 239000002360 explosive Substances 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims 1
- 230000009471 action Effects 0.000 abstract description 9
- 230000007246 mechanism Effects 0.000 abstract description 7
- 230000009467 reduction Effects 0.000 abstract description 4
- 229910000831 Steel Inorganic materials 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 239000012634 fragment Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000000739 chaotic effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/20—Launching, take-off or landing arrangements for releasing or capturing UAVs in flight by another aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model relates to a patrol device separation guide device and a patrol device assembly, which belong to the technical field of unmanned aerial vehicles and comprise a base, wherein an explosion bolt is fixedly connected to the base, the explosion bolt is fixedly connected with an parachute cabin connector, and a speed reduction parachute cabin is fixedly arranged on the parachute cabin connector; the two sides of the base are connected with the toothed lock through the sliding mechanism, the outer side of the toothed lock is provided with external teeth, the two sides of the parachute cabin connector are provided with connecting rods, the connecting rods are rotationally connected with the parachute cabin connector, and the connecting rods are rotationally connected with the toothed lock; the outer side of the tooth-shaped lock is connected with a dowel bar through an elastic ejection mechanism; an aircraft patrol assembly includes an aircraft patrol, a carrier bay, and an aircraft patrol separation guide. When the explosion bolt is successfully exploded and disconnected, the parachute can be released from the parachute cabin, so that the parachute cabin connector, the connecting rod and the tooth-shaped lock are sequentially driven to move, and meanwhile, the whole separation guide device moves towards the tail under the action of the parachute cabin, so that the patrol aircraft is released, and meanwhile, the patrol aircraft is successfully separated from the carrying cabin.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and mainly relates to a patrol aircraft separation guide device and a patrol aircraft assembly.
Background
The launching method of the patrol aircraft (unmanned aerial vehicle) is various, and the patrol aircraft has the advantages of hand throwing, vertical takeoff, aerial launching, rocket boosting, runway running, vehicle-mounted takeoff and catapult-assisted takeoff. When the patrol device is carried and put in through a conveyor, a large unmanned aerial vehicle and other platforms, the patrol device is required to be safely separated from the carrying and transporting platform, and then fly by itself.
In order to realize throwing of the patrol aircraft, the Chinese patent with the authorized bulletin number of CN212448104U discloses an air-drop throwing cylinder of the folding wing patrol aircraft, which comprises a cylinder body, a mounting assembly, a battery pack, an umbrella opening control assembly, an umbrella cabin box, a guiding umbrella, a main umbrella, an umbrella cabin cover and an umbrella opening steering engine; the control signal output end of the umbrella opening control component is connected with the control signal input end of the umbrella opening steering engine; the umbrella opening steering engine is arranged on the cylinder body and is used for controlling the locking of the umbrella cabin cover and the cylinder body. But has the following problems: in the prior art, the air drop can be realized after the umbrella cabin cover is opened, and the air drop is easy to trigger by mistake in actual use, so that the patrol aircraft is released.
Disclosure of Invention
The utility model provides a separating and guiding device for a patrol aircraft, which aims to solve the problem of separating the patrol aircraft from a carrying cabin in the prior art. The utility model also provides an aircraft patrol assembly, which is used for solving the problem of separation of the aircraft patrol and the carrier cabin in the prior art.
In order to solve the problems, the separating and guiding device of the patrol aircraft adopts the following technical scheme:
the separating and guiding device for the cruise ship comprises a base and an explosion bolt, wherein one end of the explosion bolt is fixedly arranged on one side of the base, an umbrella cabin connector is fixedly arranged at the other end of the explosion bolt, and the umbrella cabin connector is fixedly connected with a speed reduction umbrella cabin;
the two opposite ends of the base are slidably provided with tooth-shaped locks, the two tooth-shaped locks can move relatively, external teeth are arranged on the tooth-shaped locks and are used for being inserted with internal teeth on the inner wall of the carrying cabin so as to prevent the base from being separated from the carrying cabin; a connecting rod is arranged between the parachute cabin connector and each tooth-shaped lock, one end of the connecting rod is hinged to the parachute cabin connector, the other end of the connecting rod is hinged to the tooth-shaped lock, and after explosion and separation of explosion bolts, the speed-reducing parachute cabin is enabled to pull the tooth-shaped locks on two sides of the base to move oppositely through the parachute cabin connector and separate from corresponding inner teeth; a dowel bar is arranged on one side of the base or the tooth-shaped lock, which is away from the parachute cabin connector, and the base or the tooth-shaped lock is used for pulling the patrol aircraft out of the carrying cabin through the dowel bar.
Has the following beneficial effects: in the utility model, after the explosion bolt is successfully exploded and disconnected, the parachute can be released from the speed reducing parachute cabin, so that the parachute cabin connector, the connecting rod and the tooth-shaped lock are sequentially driven to move, even if the speed reducing parachute cabin is mistakenly touched, the patrol device is not released, and meanwhile, the whole separation guide device moves towards the tail under the action of the speed reducing parachute cabin, so that the patrol device is released, and meanwhile, the patrol device is successfully separated from the carrier cabin.
Furthermore, each tooth-shaped lock is provided with the dowel bars, the two dowel bars are used for clamping the patrol device together, and the two dowel bars are used for sliding on the inner wall of the carrying cabin; the tooth-shaped lock is provided with a cylindrical pin, the dowel bar is provided with a U-shaped groove, the U-shaped groove is inserted and sleeved outside the cylindrical pin along the interval direction of the two dowel bars, a spring is arranged between the tooth-shaped lock and the dowel bar in a pressing mode, and the spring is used for pushing the U-shaped groove of the dowel bar away from the cylindrical pin after the dowel bar is separated from the carrying cabin, so that the two dowel bars are separated in opposite directions, and the patrol aircraft is released.
Furthermore, the tooth-shaped lock is provided with a spring hole, the spring is embedded into the spring hole, a thimble is also slidably arranged in the spring hole, and the spring drives the thimble to be propped against the dowel bar.
Has the following beneficial effects: when the patrol device is not separated from the carrying cabin, the U-shaped groove on the dowel bar is clamped on the cylindrical pin, and after the patrol device is released, the tooth-shaped lock moves, and the thimble pushes the dowel bar under the action of the spring, and drives the U-shaped groove to be far away from the cylindrical pin, so that the dowel bar is separated from the tooth-shaped lock.
Further, the outside of dowel steel sets up the leading wheel, and the leading wheel is used for with the inner wall sliding fit of carrying the cabin.
Has the following beneficial effects: the separation guide device is convenient to move in the carrying cabin.
Further, the parachute cabin connector is of a sleeve structure, the explosion bolts penetrate into the parachute cabin connector, and the corresponding ends of the explosion bolts are connected with the parachute cabin connector.
Has the following beneficial effects: the explosion bolt penetrates into the umbrella cabin connector of the sleeve structure, and after the explosion bolt explodes, surrounding components can be protected from being influenced by explosion fragments or shock waves, so that the separation effect is prevented from being influenced.
In order to solve the problems, the patrol aircraft assembly adopts the following technical scheme:
the utility model provides an patrol and flyer subassembly, includes patrol and flyer, delivery cabin with patrol and flyer separation guider, the internal tooth has set firmly on the inner wall of delivery cabin, and the internal tooth is equipped with two and relative arrangement, external tooth and internal tooth meshing in order to realize patrol and flyer and delivery cabin between fixed and separation.
Has the following beneficial effects: the meshing of internal tooth and external tooth has guaranteed that the aircraft separation guider that patrols can be stable fix in the carrying cabin, and the aircraft that patrols that release that simultaneously can be smooth through the subassembly, release effectually.
Further, the inner wall of the carrying cabin is provided with a guide groove, and the guide groove is matched with the guide wheel.
Further, the carrying cabin is provided with a plurality of cabins, and each cabin is internally provided with a patrol aircraft.
Drawings
The above, as well as additional purposes, features, and advantages of exemplary embodiments of the present utility model will become readily apparent from the following detailed description when read in conjunction with the accompanying drawings. In the drawings, embodiments of the utility model are illustrated by way of example and not by way of limitation, and like reference numerals refer to similar or corresponding parts and in which:
FIG. 1 is a schematic view of the structure of the present utility model (without a parachute cabin);
FIG. 2 is an enlarged view of a portion of FIG. 1 at A;
FIG. 3 is a view of a base;
FIG. 4 is a right side view of FIG. 2;
FIG. 5 is a cross-sectional view at B in FIG. 4;
FIG. 6 is a top view of FIG. 2;
FIG. 7 is a cross-sectional view at C in FIG. 6;
FIG. 8 is a schematic diagram of the structure of the present utility model;
fig. 9 is a partial enlarged view at D in fig. 8.
Reference numerals illustrate: 1. tooth-shaped lock; 2. an umbrella pod connector; 3. an explosive bolt; 4. a base; 5. a connecting rod; 6. a dowel bar; 7. a guide wheel; 8. a fixed flange; 9. a guide pin; 10. a slide hole; 11. external teeth; 12. a connecting rod; 13. a rotation pin; 14. a cylindrical pin; 15. a thimble; 16. a spring; 17. a speed reducing parachute cabin; 18. and (5) carrying the cabin.
Detailed Description
The following description of the embodiments of the present utility model will be made more complete and clear to those skilled in the art by reference to the figures of the embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Various non-limiting embodiments of the utility model are described in detail below. Any number of elements in the figures are for illustration and not limitation, and any naming is used for distinction only and not for any limiting sense.
Referring to fig. 1, a cruise control assembly is shown positioned within the vehicle bay 18 and the cruise control assembly is mounted therein to provide a secure connection between the cruise control assembly and the vehicle bay 18. The device comprises a base 4, wherein the base 4 is in threaded connection with one end of an explosion bolt 3, the other end of the explosion bolt 3 is in threaded connection with an parachute cabin connector 2, the parachute cabin connector 2 is fixedly connected with a speed reduction parachute cabin 17, and the speed reduction parachute cabin 17 can be a device described in an authorized bulletin No. CN 218113003U. The explosive bolt 3 is used for multipoint connection of the separating surfaces. Each explosion bolt 3 is shaped like a common bolt, and is internally provided with an explosive and an igniter. During separation, the explosive is detonated, so that the shear lock is sheared or broken along the bolt weakening groove, and two separated unlocking is realized. The explosion bolts are of various types and mainly comprise slotted type, shearing pin type, steel ball type explosion bolts, pollution-free explosion bolts and the like. The device has the advantages of large bearing capacity, simple structure, reliable work and convenient use. In addition, the broken bolts are ensured not to hurt surrounding structures and equipment, so that a protection structure is correspondingly arranged if necessary. After the explosion bolts 3 are exploded, the parachute cabin 17 can release the parachute to form a pulling force to drive the parachute cabin connector 2 to move.
The opposite sides of the base 4 are connected with the tooth-shaped lock 1 through a sliding mechanism, external teeth 11 are arranged on the outer side of the tooth-shaped lock 1, internal teeth meshed with the external teeth 11 are arranged on the inner wall of the carrying cabin 18, and the separation guide device is ensured to be fixed in the carrying cabin 18 through the meshing of the internal teeth and the external teeth 11. The opposite sides of the canopy connector 2 are provided with links 5, and the opposite sides of the canopy connector 2 are perpendicular to the opposite sides of the base 4. One end of a connecting rod 5 is rotationally connected with the parachute cabin connector 2, and the other end of the connecting rod 5 is rotationally connected with the tooth-shaped lock 1; or, the opposite sides of the parachute cabin connector 2 are provided with the rotating pins 13, one end of the connecting rod 5 is rotationally connected with the rotating pins 13, the opposite sides of the tooth lock 1 are provided with the connecting rods 12, and the other end of the connecting rod 5 is rotationally connected with the connecting rods 12.
The outside of the tooth-shaped lock 1 is connected with the dowel bars 6 through an elastic ejection mechanism, the dowel bars 6 can be separated from the tooth-shaped lock 1 through the elastic ejection mechanism, and the patrol device is arranged between the dowel bars 6. The dowel bar 6 is used for installing the patrol device, and can also be in sliding fit with a guide groove arranged on the inner wall of the carrying cabin 18 to play a role in guiding. In the utility model, after the explosion bolt 3 is successfully exploded and disconnected, the parachute can be released from the speed reducing parachute cabin 17, so that the parachute cabin connector 2, the connecting rod 5 and the tooth-shaped lock 1 are sequentially driven to move, even if the speed reducing parachute cabin is mistakenly touched, the patrol aircraft can not be released, and meanwhile, the whole separation guide device moves towards the tail under the action of the speed reducing parachute cabin 17, so that the patrol aircraft is released, and meanwhile, the patrol aircraft is successfully separated from the carrier cabin 18.
The elastic ejection mechanism comprises a spring 16 and a thimble 15 positioned at the top end of the spring 16, wherein the thimble 15 contacts the dowel bar 6, and when the aircraft is not released, the spring 16 is in a compressed state; after the patrol device is released, the spring 16 rebounds, and the ejector pin 15 pushes the dowel bar 6 open. The outside of tooth form lock 1 sets up the spring hole, and spring 16 and thimble 15 all are located the spring hole, and dowel steel 6 root inboard sets up the U type groove, tooth form lock 1 rear side set up with U type groove complex cylindric lock 14, cylindric lock 14 can block dowel steel 6 like this, prevents dowel steel 6 and tooth form lock 1 separation. When the patrol device is not separated from the carrier cabin 18, the U-shaped groove on the dowel bar 6 is clamped on the cylindrical pin 14, and after the patrol device is released, the tooth lock 1 moves, and the ejector pin 15 pushes away the dowel bar 6 under the action of the spring 16, and drives the U-shaped groove to be far away from the cylindrical pin 14, wherein the ejector pin 15 is long enough to completely drive the dowel bar 6 to be far away from the cylindrical pin 14, so that the restriction of the cylindrical pin 14 on the dowel bar 6 is eliminated, and the dowel bar 6 is separated from the tooth lock 1.
The sliding mechanism comprises a guide pin 9, the guide pin 9 is fixedly connected with the tooth-shaped lock 1, a sliding hole 10 matched with the guide pin 9 is formed in the side face of the base 4, and the guide pin 9 can slide in the sliding hole 10 under the condition that the tooth-shaped lock 1 is driven, so that the tooth-shaped lock has a guiding function. The guide pin 9 slides in the sliding hole 10 to guide the movement of the tooth-shaped lock 1, so that the tooth-shaped lock 1 is prevented from moving in a chaotic manner, and the stability of separating the patrol from the carrier cabin 18 is improved.
The outside of dowel bar 6 sets up leading wheel 7, and leading wheel 7 and the inside guide way sliding fit of setting up in carrying cabin 18 play the guide effect, and the separation guider of being convenient for simultaneously removes in carrying cabin 18.
The appearance of the parachute cabin connector 2 is of a sleeve structure, the explosion bolts 3 penetrate into the parachute cabin connector 2 of the sleeve structure, and the corresponding ends of the explosion bolts 3 are connected with the parachute cabin connector 2. The umbrella cabin connector 2 with the sleeve structure can protect surrounding parts from the influence of explosion fragments or shock waves after the explosion of the explosion bolt 3, plays a role in protection, and avoids influencing the separation effect.
The explosion bolt 3 is fixedly connected with the base 4 through the fixing flange 8, the base 4 is fixedly connected with the fixing flange 8, and the fixing flange 8 is in threaded connection with the explosion bolt 3.
Referring to fig. 8-9, a cruise control assembly includes, in addition to the cruise control separation guide described above, a cruise control and a vehicle 18, with other vehicles (cars or planes) moving on the outside of the vehicle 18, and when the vehicle arrives at a predetermined location, the cruise control is released from the vehicle 18 to perform a mission. The cruise ship and the cruise ship separation guide are both arranged in the carrier cabin 18, and the cruise ship separation guide is used for fixing and separating the cruise ship and the carrier cabin 18. The patrol device can be smoothly released, and the release effect is good.
The inner wall of the carrying cabin 18 is provided with inner teeth which are meshed with the outer teeth 11 on the tooth lock 1. The engagement of the internal teeth with the external teeth 11 ensures that the cruise control guide can be stably secured within the cargo bay 18.
The guide way is arranged on the inner wall of the carrying cabin 18, when the guide wheel 7 is not arranged on the dowel bar 6, the guide way can be in sliding fit with the dowel bar 6, and when the guide wheel 7 is arranged on the dowel bar 6, the guide way can be matched with the guide wheel 7, and the two settings play a guiding role.
The cargo bay 18 has a plurality of bays, each for holding a cruise ship. This allows for simultaneous release of multiple flyers.
The working process of the utility model is as follows:
other vehicles (automobiles or airplanes) move on the external carrier 18, and the aircraft patrol is arranged in the carrier 18, so that when the vehicle arrives at a preset place, the aircraft patrol is released from the carrier 18 to perform tasks. When the explosion bolt 3 is detonated when the explosion bolt reaches a preset place, the parachute can be released by the speed reducing parachute cabin 17 to reduce the speed, then a pulling force is generated on the parachute cabin connector 2, the parachute cabin connector 2 drives the connecting rod 5 to move, the connecting rod 5 drives the tooth lock 1 to move along the sliding direction of the guide pin 9, so that the engagement between the inner teeth and the outer teeth 11 is separated, and the dowel bar 6 always acts on the inner wall of the carrying cabin 18 under the action of the spring 16 and the thimble 15 until the dowel bar 6 is completely separated from the limitation of the cylindrical pin 14; meanwhile, in the process of the action, the separating guide device of the patrol device and the patrol device simultaneously move to the outside of the carrying cabin 18 under the action of the cooperation of the guide wheel 7 and the guide groove and the parachute pulling force, and when the separating guide device of the patrol device and the patrol device are released to the outside of the carrying cabin 18, the dowel bar 6 can fall off under the action of the spring 16 and the thimble 15, so that the separating guide device is separated from the patrol device, and the release of the patrol device is completed.
From the foregoing description of the present specification, it will be further understood by those skilled in the art that terms such as "upper", "lower", "front", "rear", "left", "right", "width", "horizontal", "top", "bottom", "inner", "outer", and the like, which indicate an azimuth or a positional relationship, are based on the azimuth or the positional relationship shown in the drawings of the present specification, are for convenience only in explaining aspects of the present utility model and simplifying the description, and do not explicitly or implicitly refer to devices or elements having to have the specific azimuth, be constructed and operate in the specific azimuth, and thus the azimuth or positional relationship terms described above should not be interpreted or construed as limitations of aspects of the present utility model.
In addition, in the description of the present specification, the meaning of "plurality" means at least two, for example, two, three or more, etc., unless specifically defined otherwise.
Claims (8)
1. The separating and guiding device for the cruise ship is characterized by comprising a base (4) and an explosion bolt (3), wherein one end of the explosion bolt (3) is fixedly arranged on one side of the base (4), an parachute cabin connector (2) is fixedly arranged at the other end of the explosion bolt (3), and a speed-reducing parachute cabin (17) is fixedly connected with the parachute cabin connector (2);
the two opposite ends of the base (4) are slidably provided with tooth-shaped locks (1), the two tooth-shaped locks (1) can move relatively, external teeth (11) are arranged on the tooth-shaped locks (1), and the external teeth (11) are used for being inserted with the internal teeth on the inner wall of the carrying cabin (18) so as to prevent the base (4) from being separated from the carrying cabin (18); a connecting rod (5) is arranged between the parachute cabin connector (2) and each tooth-shaped lock (1), one end of the connecting rod (5) is hinged on the parachute cabin connector (2), the other end of the connecting rod (5) is hinged on the tooth-shaped locks (1), and after explosion separation of the explosion bolts (3), the speed-reducing parachute cabin (17) pulls the tooth-shaped locks (1) on two sides of the base (4) to move oppositely through the parachute cabin connector (2) and separate from corresponding inner teeth; a dowel bar (6) is arranged on one side of the base (4) or the tooth-shaped lock (1) which is away from the parachute cabin connector (2), and the base (4) or the tooth-shaped lock (1) is used for pulling the patrol aircraft out of the carrying cabin (18) through the dowel bar (6).
2. The aircraft patrol separation guide device according to claim 1, wherein each tooth lock (1) is provided with a dowel bar (6), the dowel bars (6) are used for clamping the aircraft patrol together, and the dowel bars (6) are used for sliding on the inner wall of the carrying cabin (18); the tooth-shaped lock (1) is provided with a cylindrical pin (14), the dowel bar (6) is provided with a U-shaped groove, the U-shaped groove is inserted and sleeved outside the cylindrical pin (14) along the interval direction of the two dowel bars (6), a spring (16) is arranged between the tooth-shaped lock (1) and the dowel bars (6) in a pressing mode, and the spring (16) is used for pushing the U-shaped groove of the dowel bars (6) away from the cylindrical pin (14) after the dowel bars (6) are separated from the carrying cabin (18) so that the two dowel bars (6) are separated in opposite directions and the patrol aircraft is released.
3. The separating and guiding device of the cruise ship according to claim 2, wherein the tooth lock (1) is provided with a spring hole, the spring (16) is embedded into the spring hole, a thimble (15) is also slidably arranged in the spring hole, and the spring (16) drives the thimble (15) to push against the dowel bar (6).
4. The separating and guiding device of the cruise ship according to claim 2, characterized in that a guiding wheel (7) is arranged on the outer side of the dowel bar (6), and the guiding wheel (7) is used for being in sliding fit with the inner wall of the carrying cabin (18).
5. A cruise control according to any one of claims 1-4, characterized in that the canopy connector (2) is of a sleeve construction, that the explosive bolts (3) penetrate into the canopy connector (2), and that the respective ends of the explosive bolts (3) are connected to the canopy connector (2).
6. The aircraft patrol assembly is characterized by comprising an aircraft patrol, a carrier cabin (18) and the aircraft patrol separation guide device according to any one of claims 1-5, wherein internal teeth are fixedly arranged on the inner wall of the carrier cabin (18), two internal teeth are oppositely arranged, and the external teeth (11) are meshed with the internal teeth to fix and separate the aircraft patrol and the carrier cabin (18).
7. An aircraft assembly according to claim 6, characterized in that the inner wall of the carrying compartment (18) is provided with guide grooves which cooperate with guide wheels (7).
8. A cruise control assembly according to claim 6, wherein the carrier pod (18) has a plurality of bays, each bay being adapted for receiving a cruise control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310845395.4A CN116588371B (en) | 2023-07-11 | 2023-07-11 | Patrol aircraft separation guiding device and patrol aircraft assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310845395.4A CN116588371B (en) | 2023-07-11 | 2023-07-11 | Patrol aircraft separation guiding device and patrol aircraft assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116588371A true CN116588371A (en) | 2023-08-15 |
| CN116588371B CN116588371B (en) | 2023-09-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310845395.4A Active CN116588371B (en) | 2023-07-11 | 2023-07-11 | Patrol aircraft separation guiding device and patrol aircraft assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116588371B (en) |
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| CN115991295A (en) * | 2023-03-03 | 2023-04-21 | 中国工程物理研究院总体工程研究所 | Folding wing patrol aircraft mounting and throwing device and throwing method |
| CN116176840A (en) * | 2023-03-09 | 2023-05-30 | 南京航空航天大学 | Spring lock catch spring-open type separating mechanism for split flying wing layout aircraft |
| CN116447932A (en) * | 2023-03-15 | 2023-07-18 | 上海机电工程研究所 | Active separating device for missile-borne patrol device |
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| CN116588371B (en) | 2023-09-29 |
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