CN209553496U

CN209553496U - A kind of four axis aircrafts

Info

Publication number: CN209553496U
Application number: CN201920222373.1U
Authority: CN
Inventors: 郑顺发
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-02-22
Filing date: 2019-02-22
Publication date: 2019-10-29
Anticipated expiration: 2029-02-22

Abstract

The utility model discloses a kind of four axis aircrafts, including fuselage and the folding flight wing of fuselage outer side, wherein flight wing is four, and circumferentially array is arranged in the outside of fuselage to four flight wings, the two sides of fuselage are equipped with bindiny mechanism, the inside of bindiny mechanism is cavity, shaft is equipped in its hollow cavity, and the outside of shaft is equipped with the position of bone of protrusion, there are two the openings being connected with cavity for the side wall dislocation arrangement of bindiny mechanism, and the direction of two openings is respectively facing afterbody and fuselage head, the head end of flight wing is set to cavity inside through opening, wherein the head end of flight wing is equipped with the mounting groove being adapted to shaft, and the inner wall of mounting groove is circumferentially arranged with the detent being adapted to the position of bone, the top of the end of flight wing is equipped with motor and accommodates column, wherein motor, which accommodates, is equipped with motor in column, and motor is connected with propeller, in fuselage Equipped with control panel, and control panel controls the rotation of motor.The utility model is designed reasonably, structure is simple, small in size, and flight wing is foldable, reduces occupied space, facilitates collection, is easy to carry about with one, and avoids the damage to screw blade.

Description

A kind of four axis aircrafts

Technical field

The utility model belongs to flying toy field, and in particular to a kind of four axis aircrafts.

Background technique

Four axis aircrafts are a kind of multi-rotor aerocrafts, its four propellers are all the simple mechanisms of motor direct-connected, it is deep by People's likes, but existing four axis aircaft configuration is fixed, not easily contained, be easy to cause the damage of propeller.

Utility model content

The purpose of this utility model is to provide a kind of four axis aircrafts, to solve to ask proposed in above-mentioned background technique Topic.

To achieve the above object, the utility model is the following technical schemes are provided: a kind of four axis aircrafts, structural feature exist In: including fuselage and the folding flight wing of fuselage outer side, wherein flight wing is four, and four flight wings circumferentially arrange by array It is listed in the outside of fuselage, the two sides of fuselage are equipped with bindiny mechanism, and the inside of bindiny mechanism is cavity, are equipped with and turn in hollow cavity Axis, and the outside of shaft is equipped with the position of bone of protrusion, the side wall dislocation of bindiny mechanism is arranged there are two the opening being connected with cavity, And the direction of two openings is respectively facing afterbody and fuselage head, the head end of flight wing is set to cavity inside through opening, Wherein the head end of flight wing is equipped with the mounting groove being adapted to shaft, and the inner wall of mounting groove is circumferentially arranged with the card being adapted to the position of bone Position, the top of the end of flight wing are equipped with motor and accommodate column, and wherein motor, which accommodates, is equipped with motor in column, and motor is connected with spiral Paddle, fuselage is interior to be equipped with control panel, and the rotation of control panel control motor.

Preferably, fuselage is from top to bottom followed successively by upper cover, battery, battery mounting base, fuselage mounting plate, control Plate, WIFI module and lower cover, and upper cover and lower cover are detachably connected by screw or buckle structure.

Preferably, fuselage head is equipped with camera, and camera is connected by WIFI module with mobile electronic device It connects, and mobile electronic device is mobile phone or tablet computer.

Preferably, afterbody is equipped with switch and battery charging jack.

Preferably, being arranged in parallel when flight wing is packed up with fuselage.

Preferably, opening includes upper opening and under shed, wherein upper opening is towards afterbody side, under shed court To fuselage head side, and the rotation angle for the flight wing being set in upper opening is 0-35 °, the flight wing under shed Rotating angle is 0-35 °.

Preferably, bindiny mechanism includes upper housing and lower case, and upper housing is wholely set with fuselage mounting plate, under Shell is wholely set with lower cover.

Compared with prior art, the utility model is designed reasonably, structure is simple, small in size, and flight wing is foldable, reduces Occupied space facilitates collection, is easy to carry about with one, and avoids the damage to screw blade.

Detailed description of the invention

Fig. 1 is the structural schematic diagram of the utility model collapsed state；

Fig. 2 is the structural schematic diagram of the utility model unfolded state；

Fig. 3 is the configuration schematic diagram of the utility model；

Fig. 4 is the mounting structure schematic diagram of the utility model flight wing；

In figure: 1- fuselage, 2- flight wing, 3- bindiny mechanism, 4- cavity, 5- shaft, 7- motor accommodate column, 8- motor, 9- Propeller, 10- control panel, 11- upper cover, 12- battery, 13- battery mounting base, 14- fuselage mounting plate, 15-WIFI module, 16- lower cover, 17- camera, 18- switch, 19- battery charging jack, 20- upper housing, 21- lower case, 22- upper opening, 23- Under shed, the 24- position of bone, 25- mounting groove, 26- detent.

Specific embodiment

Explanation is further explained to the utility model with reference to the accompanying drawing, but does not limit the protection model of the utility model It encloses.

In the description of the present invention, it should be noted that term " on ", "lower", "left", "right", "inner", "outside" etc. The orientation or positional relationship of instruction is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of description the utility model It is described with simplifying, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific orientation structure It makes and operates, therefore should not be understood as limiting the present invention.

Fig. 1-4 is please referred to, the utility model provides a kind of technical solution, a kind of four axis aircrafts, including fuselage 1 and fuselage 1 The folding flight wing 2 in outside, wherein flight wing 2 is four, and circumferentially array is arranged in the outer of fuselage 1 to four flight wings 2 Side, the two sides of the fuselage 1 are equipped with bindiny mechanism 3, and the inside of the bindiny mechanism 3 is cavity 4, in hollow cavity 4 Equipped with shaft 5, and the outside of shaft 5 is equipped with the position of bone 24 of protrusion, the side wall dislocation arrangement of the bindiny mechanism 3 there are two with The opening that cavity 4 is connected, and the direction of two openings is respectively facing afterbody and fuselage head, the flight wing 2 Head end is set to inside cavity 4 through opening, and wherein the head end of flight wing 2 is equipped with the mounting groove 25 being adapted to shaft 5, and mounting groove 25 inner wall is accommodated circumferentially arranged with the detent 26 being adapted to the position of bone 24, the top of the end of the flight wing 2 equipped with motor Column 7, wherein motor accommodates and is equipped with motor 8 in column 7, and motor 8 is connected with propeller 9, is equipped with control panel in the fuselage 1 10, and control panel 10 controls the rotation of motor 8.

Wherein, in the present embodiment, the fuselage 1 is from top to bottom followed successively by upper cover 11, battery 12, battery installation Seat 13, fuselage mounting plate 14, control panel 10, WIFI module 15 and lower cover 16, and upper cover 11 and lower cover 16 pass through screw or buckle Structure is detachably connected.

Wherein, in the present embodiment, the fuselage head is equipped with camera 17, and camera 17 passes through WIFI module 15 It is connected with mobile electronic device, and mobile electronic device is mobile phone or tablet computer.

Wherein, in the present embodiment, the afterbody is equipped with switch 18 and battery charging jack 19.

Wherein, in the present embodiment, it is arranged in parallel when the flight wing 2 is packed up with fuselage 1.

Wherein, in the present embodiment, the opening includes upper opening 22 and under shed 23, and wherein upper opening 22 is towards machine Body tail portion side, under shed 23 is towards fuselage head side, and the rotation angle for the flight wing 2 being set in upper opening 22 is 0- 35 °, the rotation angle of the flight wing 2 under shed 23 is 0-35 °.

Wherein, in the present embodiment, the bindiny mechanism 3 include upper housing 20 and lower case 21, and upper housing 20 with Fuselage mounting plate 14 is wholely set, and lower case 21 is wholely set with lower cover 16.

The flight wing 2 of four axis aircraft of the utility model uses overlapping combinations mode, flies using 1 side central point of fuselage as front and back The superposition central point of row wing 2,

When being packed up respectively to fuselage head and afterbody side positioned at two ipsilateral flight wings 2 of fuselage 1, flight wing 2 are arranged in parallel with fuselage 1, and are set to two ipsilateral flight wings 2 of fuselage 1 on same perpendicular, and four axis can be made to fly The overall volume of machine is small, easily contained, and folded flight wing 2 it is possible to prevente effectively from flight wing 2 stretches out 1 outside of fuselage, receive by reduction The damaged probability of flight wing 2 and propeller 9 after receiving when playing, flight wing 2 is rotated to the side far from fuselage 1, adjusts flight The rotation detent of flight wing 2, Ke Yigu may be implemented in the expanded angle of wing 2 to suitable position, the cooperation of the position of bone 24 and detent 26 The expanded angle of fixed postrotational flight wing, control panel 10 can control the operating of motor 8 to drive propeller 9 to rotate, make four Axis aircraft flight.Control panel 10 can control motor 8 and carry out positive and negative rotation, realize the aerial tumbling action of four axis aircrafts.

The utility model is designed reasonably, structure is simple, has a smooth flight, small in size, and flight wing is foldable, and it is empty to reduce occupancy Between, facilitate collection, be easy to carry about with one, avoids the damage to screw blade.

The technological core of the utility model is that flight wing can be realized folding, and control panel, circuit structure, motor are positive and negative Turn, aerial tumbling action etc. is no difference with existing aircraft, can be by being commercially available, therefore, it is can be real Existing.

It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in All changes in justice and range are embraced therein, and should not treat any reference in the claims as limiting Related claim.

In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiments being understood that.

Claims

1. a kind of four axis aircrafts, it is characterised in that: including fuselage and the folding flight wing of fuselage outer side, wherein flight wing is four It is a, and circumferentially array is arranged in the outside of fuselage to four flight wings, the two sides of the fuselage are equipped with bindiny mechanism, described The inside of bindiny mechanism be cavity, shaft is equipped in hollow cavity, and the outside of shaft is equipped with the position of bone of protrusion, the company There are two the openings being connected with cavity for the side wall dislocation arrangement of connection mechanism, and the direction of two openings is respectively facing afterbody And fuselage head, the head end of the flight wing are set to cavity inside through opening, wherein the head end of flight wing is equipped with and shaft The mounting groove of adaptation, and the inner wall of mounting groove is circumferentially arranged with the detent being adapted to the position of bone, the end of the flight wing it is upper Side is equipped with motor and accommodates column, and wherein motor, which accommodates, is equipped with motor in column, and motor is connected with propeller, is equipped in the fuselage Control panel, and the rotation of control panel control motor.

2. a kind of four axis aircraft according to claim 1, it is characterised in that: the fuselage is from top to bottom followed successively by Lid, battery, battery mounting base, fuselage mounting plate, control panel, WIFI module and lower cover, and upper cover and lower cover pass through screw Or buckle structure is detachably connected.

3. a kind of four axis aircraft according to claim 1, it is characterised in that: the fuselage head is equipped with camera, and Camera is connected by WIFI module with mobile electronic device, and mobile electronic device is mobile phone or tablet computer.

4. a kind of four axis aircraft according to claim 1, it is characterised in that: the afterbody is equipped with switch and electric power storage Pond charging jack.

5. a kind of four axis aircraft according to claim 1, it is characterised in that: the flight wing is parallel with fuselage when packing up Setting.

6. a kind of four axis aircraft according to claim 1, it is characterised in that: the opening includes that upper opening is opened under Mouthful, wherein upper opening is towards afterbody side, and under shed is towards fuselage head side, and the flight wing that is set in upper opening Rotating angle is 0-35 °, and the rotation angle of the flight wing under shed is 0-35 °.

7. a kind of four axis aircraft according to claim 1, it is characterised in that: the bindiny mechanism includes upper housing under Shell, and upper housing is wholely set with fuselage mounting plate, lower case is wholely set with lower cover.