CN102180257A

CN102180257A - Modular quickly-spliced unmanned aerial vehicle

Info

Publication number: CN102180257A
Application number: CN201110095531XA
Authority: CN
Inventors: 权军; 田凯
Original assignee: CHINA-TIMES AEROSPACE TECHNOLOGY Co Ltd
Current assignee: CHINA-TIMES AEROSPACE TECHNOLOGY Co Ltd
Priority date: 2011-04-15
Filing date: 2011-04-15
Publication date: 2011-09-14
Anticipated expiration: 2031-04-15
Also published as: CN102180257B

Abstract

The invention relates to a modular quickly-spliced unmanned aerial vehicle. The unmanned aerial vehicle comprises a left wing module, a hatch module, a vertical module, a body module, a parachute cabin module and a right wing module which are connected with one another through uniformly distributed latch devices, wherein each latch device consists of a latch seat and a locking column; and the latch devices are fixedly arranged on interconnected module materials respectively, and one latch device is a locking latch device. The main constituent parts of the unmanned aerial vehicle are subjected to modular manufacturing, so that smallest volume can be realized for packaging, vehicle-mounted space is increased, and transportation is facilitated; meanwhile, the modular parts are subjected to standardized manufacturing, so that easily damaged parts can be quickly supplemented, installed and used, can be quickly assembled and disassembled and accurately matched when a task is executed, and can be applied to the task immediately, and work efficiency is improved. The unmanned aerial vehicle has a simple integral structure and a scientific and reasonable design, perfectly solves a large number of problems of the conventional unmanned aerial vehicle, and lays a foundation for the development and utilization of the unmanned aerial vehicle.

Description

The quick spliced unmanned plane of modular

Technical field

The invention belongs to aviation field, relate to unmanned plane, the quick spliced unmanned plane of especially a kind of modular.

Background technology

China's SUAV (small unmanned aerial vehicle) industry is started late, in the design process in that one is with reference to external active service unmanned plane design aspect the equipment of profile, specification and lift-launch, fuselage and airfoil member still adopt the mode of captive joint, exist big not enough at aspects such as transportation, making, be embodied in: 1, when executing the task, can not realize quick assembly and disassembly, can not drop into task at once once more; 2, the unmanned plane volume is bigger, cause vehicle-mounted and install, the transportation difficulty; 3, can not be in time when a certain damage parts of unmanned plane, exchange fast, can not effectively match during maintenance, can only rebuild.

In recent years, the up-to-date technology and the new material development of China's composite material industry are very fast, because of its material light weight, excellent in cushion effect, temperature deformation is little (" creep " that the difference of Yin Wendu causes), antiageing (serviceable bife prolongation), characteristics such as corrosion prevention, thunder and lightning, static and various storeroom compatibility height are used very extensive in many industries.At present, China's unmanned plane can adopt advanced composite material, becomes possibility for the modular production of unmanned plane thus.

By retrieval, find one piece of open source literature relevant with present patent application: a kind of folding small-sized unmanned aerial vehicle (CN101712379A), it comprises: a blended wing-body; A pair of wing, be separately positioned on the left and right sides of described blended wing-body, each described wing and described blended wing-body junction are provided with one first fold mechanism, and described first fold mechanism is set to make described wing the described wing that launches can be locked in deployed condition with respect to downward the folding also of described blended wing-body; An empennage; A shoe, the one end connects described empennage, the other end is connected with described blended wing-body by one second fold mechanism, and described second fold mechanism is set to make described shoe the described shoe that launches can be locked in deployed condition with respect to downward the folding also of described blended wing-body.Described SUAV (small unmanned aerial vehicle) can be accommodated in the cuboid packing chest after its housing construction is folding, can utilize pneumatic acting device to be expanded to state of flight automatically to carry out aerial mission such as aerial input, simultaneously the loadingunloading time shorter, convenient transportation.

Though above-mentioned patent application and present patent application purpose are basic identical, have more different with the technical scheme of present patent application.

Summary of the invention

The object of the invention is to overcome the deficiencies in the prior art part, provides a kind of modular quick spliced unmanned plane.

The present invention solves its technical matters and is achieved through the following technical solutions:

The quick spliced unmanned plane of a kind of modular, it is characterized in that: unmanned plane comprises port wing module, hatchcover module, vertical module, fuselage module, umbrella cabin module, starboard wing module, above-mentioned adjacent modules all adopts uniform latching system to connect each other, latching system is made of snap close seat and lock, and corresponding respectively being packed on the interconnected module material, one of them latching system is a fixed latching system with lock.

And described unmanned plane also comprises port wingtip module and right flank point module.

And, the lockhole locking of described lock front end and snap close seat, install with the permanent seat that is packed on the module material lock rear end.

And, described fixed latching system with lock reaches the lockhole of being made by locking pressure handle, snap close seat, spring and constitutes on the snap close seat, on the snap close seat stuck-module material, the locking pressure handle vertically is installed in the made orienting sleeve of snap close seat, its front end is made and is colluded the shape front end and be installed in the lockhole, colludes at lockhole right part and locking pressure handle and forms the lock in place hole between the shape front end.

And described latching system is made of snap close seat and lockhole.

And described lock is installed together by screw-threaded engagement and permanent seat.

Advantage of the present invention and good effect are:

1, this unmanned plane carries out the modular manufacturing with the main composition parts, can realize minimum volume packing, and vehicle-mounted space is increased, and has made things convenient for transportation.

2, this unmanned plane carries out the normalisation manufacturing with modular component, and consumable accessory can replenish fast thus, and Fast Installation is used, and can realize quick assembly and disassembly when executing the task, and cooperates accurately, can drop into task at once, increases work efficiency.

3, this unmanned plane can directly be changed when a certain standard modular damage parts fast; Connect between the modular parts quick and precisely quick, the intensity height, fastening design is rigorous, stable no diastema.

4, this unmanned plane integral structure is simple, and design science is reasonable, and perfection has overcome the problems that existing unmanned plane exists, for the development and use of unmanned plane are laid a good foundation.

Description of drawings

Fig. 1 is a unmanned plane blast structural representation of the present invention;

Fig. 2 is each module connection structure confined explosion enlarged diagram of the present invention;

Fig. 3 is the perspective view (lock-out state) of the present invention's fixed snap close seat with lock;

Fig. 4 is the perspective view of the lockhole release position of Fig. 3;

Fig. 5 is the present invention's fixed snap close seat perspective view not with lock;

Fig. 6 is the mounting structure scheme drawing of lock of the present invention and wing.

The specific embodiment

The invention will be further described by specific embodiment below in conjunction with accompanying drawing, and following examples are descriptive, are not determinate, can not limit protection scope of the present invention with this.

The quick spliced unmanned plane of a kind of modular comprises eight kinds of modules and the latching system of being installed therebetween.Wherein, eight kinds of modules are respectively: port wingtip module 1, port wing module 2, hatchcover module 3, vertical module 4, fuselage module 5, umbrella cabin module 7, starboard wing module 8 and right flank point module 9, the positional structure of above-mentioned module is a prior art, does not repeat them here.

Above-mentioned module all adopts latching system to connect fast each other, being provided with according to bonded assembly area between each module of latching system decided, in the present embodiment accompanying drawing, left and right wing module adopts three latching systems with being connected of fuselage, one of them snap close has locking, be usefulness in order to locate, in addition two not with lock fixed.

Concrete latching system structure is referring to Fig. 2,3,4,5,6.Latching system is made of snap close seat (12 and 15) and lock 17, the structure of lock is referring to Fig. 6, its front end is made the dead bolt shape, be shaped on latch recess, install by screw-threaded engagement mode and the bonding permanent seat 18 that is packed in (the present embodiment accompanying drawing is depicted as starboard wing) on the module material rear end, by screw-threaded engagement, can regulate the extension elongation of lock.

Fixed latching system with lock is referring to Fig. 3,4, reaching the lockhole of being made 13 by locking pressure handle 10, snap close seat 12, spring 11 on the snap close seat constitutes, the snap close seat is fixed on each module by mode such as gluing, the locking pressure handle vertically is installed in the made orienting sleeve of snap close seat (not having label), its front end is made and is colluded shape front end and can being installed in the lockhole, colludes formation lock in place hole 14 between the shape front end at lockhole right part and locking pressure handle.During use, as long as depress the locking pressure handle, it colludes the shape front end and withdraws downwards, can discharge lockhole thus, and lock can insert in the lockhole, and side travel arrives the lock in place sky; After unclamping the locking pressure handle, the restoring force effect of spring can make colludes the shape front end and protrudes upward, and locks lock thus.

Fixed latching system not with lock referring to Fig. 5, only is to be made of snap close seat 15 and lockhole 16.

The latching system of installing between adjacent modules will guarantee that one of them is fixed getting final product with lock.

Among the present invention, latching system can adopt resin material to make.

Claims

1. quick spliced unmanned plane of modular, it is characterized in that: unmanned plane comprises port wing module, hatchcover module, vertical module, fuselage module, umbrella cabin module, starboard wing module, above-mentioned adjacent modules all adopts uniform latching system to connect each other, latching system is made of snap close seat and lock, and corresponding respectively being packed on the interconnected module material, one of them latching system is a fixed latching system with lock.

2. the quick spliced unmanned plane of modular according to claim 1 is characterized in that: described unmanned plane also comprises port wingtip module and right flank point module.

3. the quick spliced unmanned plane of modular according to claim 1 and 2 is characterized in that: the lockhole locking of described lock front end and snap close seat, install with the permanent seat that is packed on the module material lock rear end.

4. the quick spliced unmanned plane of modular according to claim 1 and 2, it is characterized in that: described fixed latching system with lock reaches the lockhole of being made by locking pressure handle, snap close seat, spring and constitutes on the snap close seat, on the snap close seat stuck-module material, the locking pressure handle vertically is installed in the made orienting sleeve of snap close seat, its front end is made and is colluded the shape front end and be installed in the lockhole, colludes at lockhole right part and locking pressure handle and forms the lock in place hole between the shape front end.

5. the quick spliced unmanned plane of modular according to claim 1, it is characterized in that: described latching system is made of snap close seat and lockhole.

6. the quick spliced unmanned plane of modular according to claim 3, it is characterized in that: described lock is installed together by screw-threaded engagement and permanent seat.