CN209581842U - Folding joint and multi-rotor unmanned aerial vehicle with it - Google Patents

Folding joint and multi-rotor unmanned aerial vehicle with it Download PDF

Info

Publication number
CN209581842U
CN209581842U CN201822265809.3U CN201822265809U CN209581842U CN 209581842 U CN209581842 U CN 209581842U CN 201822265809 U CN201822265809 U CN 201822265809U CN 209581842 U CN209581842 U CN 209581842U
Authority
CN
China
Prior art keywords
connector
detent
folding joint
lock shaft
angle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201822265809.3U
Other languages
Chinese (zh)
Inventor
陈豹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201822265809.3U priority Critical patent/CN209581842U/en
Application granted granted Critical
Publication of CN209581842U publication Critical patent/CN209581842U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Aerials With Secondary Devices (AREA)

Abstract

The utility model relates to a kind of folding joint and with its multi-rotor unmanned aerial vehicle.The folding joint includes: the first connector;Second connector;Connecting shaft, the connecting shaft are connected between first connector and second connector, so as to have the freedom degree being relatively rotatable to each other between first connector and second connector;Lock shaft, the lock shaft are slidably disposed in the sliding slot being opened on second connector;When angle between second connector and first connector is the first predetermined angle, the lock shaft can slide into the first detent on first connector along the sliding slot;When angle between second connector and first connector is the second predetermined angle, the lock shaft can slide into the second detent on first connector along the sliding slot;When the lock shaft slides into first detent or the second detent, second connector loses the freedom degree relative to first connector rotation.

Description

Folding joint and multi-rotor unmanned aerial vehicle with it
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of folding joint and with its more rotors nobody Machine.
Background technique
Unmanned plane not only has very important status in modern military activity, also has in civil field very wide Application prospect, for example, take photo by plane, plant protection, express transportation, disaster relief, wild animal observation etc..Unmanned plane include fixed-wing nobody Machine and rotor wing unmanned aerial vehicle, wherein multi-rotor unmanned aerial vehicle because have the advantages that can VTOL, can hover, low etc. to site requirements, by Gradually become the main product of civilian unmanned plane.However it also has larger, not readily portable and transport of horn extending space etc. no Foot place.
Utility model content
The purpose of this utility model is at least to solve one of above-mentioned problems of the prior art.For this purpose, this is practical new Type proposes a kind of folding joint and the multi-rotor unmanned aerial vehicle with it.
The folding joint of the utility model embodiment, comprising: the first connector;Second connector;Connecting shaft, the connection Axis connection is between first connector and second connector, so that first connector and second connector Between there is the freedom degree that is relatively rotatable to each other;Lock shaft, the lock shaft, which is slidably disposed on, is opened in second company In sliding slot on fitting;It is described when angle between second connector and first connector is the first predetermined angle Lock shaft can slide into the first detent on first connector along the sliding slot;Second connector and described first connects When angle between fitting is the second predetermined angle, the lock shaft can slide on first connector along the sliding slot Second detent;When the lock shaft slides into first detent or the second detent, second connector is lost relative to described The freedom degree of first connector rotation.
The folding joint of the utility model embodiment can be applied to the company between the body of multi-rotor unmanned aerial vehicle and horn It connects, specifically, the first connector and the second connector can be connect with body and horn respectively, when the angle between horn and body When in the first predetermined angle or the second predetermined angle, it can realize that the angle between horn and body is fixed by lock shaft, Therefore, as long as reasonable setting the first predetermined angle and the second predetermined angle, so that it may realize horn relative to the stretching, extension of body or It folds, thus realize a kind of multi-rotor unmanned aerial vehicle that horn can fold, it, can be by horn when multi-rotor unmanned aerial vehicle does not work It is folded, reduces occupied space, improve the convenience of carrying.
In some embodiments of the utility model, first detent and the second detent are that setting connects described first Right-angle notch on fitting.
In some embodiments of the utility model, first predetermined angle is 180 ° to 190 °, and described second is default Angle is 90 ° to 100 °.
In some embodiments of the utility model, first connector and the second connector are square connecting member.
The multi-rotor unmanned aerial vehicle of the utility model embodiment, the folding joint with any of the above-described embodiment.
The multi-rotor unmanned aerial vehicle of the utility model embodiment may be implemented horn and flex outward or be folded in relative to body The side of body, so that multi-rotor unmanned aerial vehicle be allow to be converted between working morphology and folded form, when more rotors without It is man-machine be in folded form when, occupy little space, it is easy to carry and transport.
In some embodiments of the utility model, the multi-rotor unmanned aerial vehicle includes body and multiple horns, Mei Yisuo It states horn and passes through the folding joint and connect with the body.
Detailed description of the invention
By reading the following detailed description of the preferred embodiment, various other advantages and benefits are common for this field Technical staff will become clear.The drawings are only for the purpose of illustrating a preferred embodiment, and is not considered as practical to this Novel limitation.And throughout the drawings, the same reference numbers will be used to refer to the same parts.In the accompanying drawings:
Fig. 1 is the structural schematic diagram of the folding joint of the utility model embodiment.
Respectively label is expressed as follows in attached drawing:
1: the first connector, 2: the second connectors, 3: connecting shaft, 4: lock shaft, 5: sliding slot.
Specific embodiment
The illustrative embodiments of the disclosure are more fully described below with reference to accompanying drawings.Although showing this public affairs in attached drawing The illustrative embodiments opened, it being understood, however, that may be realized in various forms the disclosure without the reality that should be illustrated here The mode of applying is limited.It is to be able to thoroughly understand the disclosure on the contrary, providing these embodiments, and can be by this public affairs The range opened is fully disclosed to those skilled in the art.
It should be understood that term used herein merely for description particular example embodiment purpose, and have no intention into Row limitation.Unless the context clearly indicates otherwise, otherwise singular " one " as used in the text, "one" and " described " Can also indicate to include plural form.The terms "include", "comprise", " containing " and " having " are inclusives, and therefore It indicates the presence of stated feature, step, operations, elements, and/or components, but presence or addition one or more is not precluded A other feature, step, operation, component, assembly unit, and/or their combination.
Although can be described in the text using term first, second, third, etc. multiple element, component, region, layer and/ Or section, still, these component, assembly units, region, layer and/or section should not be limited by these terms.These terms can be only For a component, assembly unit, region, layer or section are distinguished with another region, layer or section.Unless context clearly refers to Out, do not implied that when otherwise the term and other numerical terms of such as " first ", " second " etc use in the text sequence or Person's order.Therefore, first element discussed below, component, region, layer or section are in the introduction for not departing from example embodiment In the case of can be referred to as second element, component, region, layer or section.
As shown in Figure 1, the folding joint of the utility model embodiment, including the first connector 1, the second connector 2, connection Axis 3 and lock shaft 4.Connecting shaft 3 is connected between the first connector 1 and the second connector 2, so that the first connector 1 and second There is the freedom degree being relatively rotatable to each other between connector 2.Lock shaft 4, which is slidably disposed on, to be opened on the second connector 2 Sliding slot 5 in.When the angle between the second connector 2 and the first connector 1 is the first predetermined angle, lock shaft 4 being capable of edge Sliding slot 5 slides into the first detent on the first connector 1;When the angle between the second connector 2 and the first connector 1 is second pre- If when angle, lock shaft 4 can along the chute 5 slide into the first connectors 1 on the second detent.Lock shaft 4 slide into the first detent or When the second detent, the second connector 2 loses the freedom degree relative to the rotation of the first connector 1.
The folding joint of the utility model embodiment can be applied to the company between the body of multi-rotor unmanned aerial vehicle and horn It connects, specifically, the first connector 1 and the second connector 2 can be connect with body and horn respectively, when the folder between horn and body When angle is in the first predetermined angle or the second predetermined angle, it can realize that the angle between horn and body is solid by lock shaft 4 It is fixed, therefore, as long as rationally the first predetermined angle of setting and the second predetermined angle, so that it may realize stretching, extension of the horn relative to body Or fold, thus realize a kind of multi-rotor unmanned aerial vehicle that horn can fold, it, can be by machine when multi-rotor unmanned aerial vehicle does not work Arm is folded, and is reduced occupied space, is improved the convenience of carrying.
In some embodiments, the first detent and the second detent are the right-angle notch being arranged on the first connector 1, when Lock shaft 4 slides into the bottom of the first detent or the second detent, and two right-angle sides of right-angle notch offset with lock shaft 4, makes the A connection piece 1 can neither be rotated in the clockwise direction relative to the second connector 2, can not be relative to the second connector 2 along inverse Clockwise rotation.
In some embodiments, the first predetermined angle is 180 ° to 190 °, and the second predetermined angle is 90 ° to 100 °, wherein First predetermined angle corresponds to the state that the horn of multi-rotor unmanned aerial vehicle is stretched relative to body, and the second predetermined angle corresponds to horn folding It is laminated on the state of the side of body.
In some embodiments, the first connector 1 and the second connector 2 are square connecting member, so that folding joint exists The abrupt change of cross-section is not present during power transmission, so that stress mutation is avoided, to improve the stability of mechanical movement.
The multi-rotor unmanned aerial vehicle of the utility model embodiment, the folding joint with any of the above-described embodiment.
Further, multi-rotor unmanned aerial vehicle includes body and multiple horns, and each horn passes through folding joint and body Connection.
The multi-rotor unmanned aerial vehicle of the utility model embodiment may be implemented horn and flex outward or be folded in relative to body The side of body, so that multi-rotor unmanned aerial vehicle be allow to be converted between working morphology and folded form, when more rotors without It is man-machine be in folded form when, occupy little space, it is easy to carry and transport.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not It is confined to this, anyone skilled in the art within the technical scope disclosed by the utility model, can readily occur in Change or replacement, should be covered within the scope of the utility model.Therefore, the protection scope of the utility model should be with Subject to the scope of protection of the claims.

Claims (6)

1. a kind of folding joint characterized by comprising
First connector;
Second connector;
Connecting shaft, the connecting shaft are connected between first connector and second connector, so that described first connects There is the freedom degree being relatively rotatable to each other between fitting and second connector;
Lock shaft, the lock shaft are slidably disposed in the sliding slot being opened on second connector;
When angle between second connector and first connector is the first predetermined angle, the lock shaft being capable of edge The sliding slot slides into the first detent on first connector;
When angle between second connector and first connector is the second predetermined angle, the lock shaft being capable of edge The sliding slot slides into the second detent on first connector;
When the lock shaft slides into first detent or the second detent, second connector loses to be connected relative to described first The freedom degree of fitting rotation.
2. folding joint according to claim 1, which is characterized in that first detent and the second detent are that setting exists Right-angle notch on first connector.
3. folding joint according to claim 2, which is characterized in that first predetermined angle is 180 ° to 190 °, institute Stating the second predetermined angle is 90 ° to 100 °.
4. folding joint according to claim 1 or 2 or 3, which is characterized in that first connector and the second connector It is square connecting member.
5. a kind of multi-rotor unmanned aerial vehicle, which is characterized in that have folding joint according to any one of claim 1 to 4.
6. multi-rotor unmanned aerial vehicle according to claim 5, which is characterized in that each described including body and multiple horns Horn passes through the folding joint and connect with the body.
CN201822265809.3U 2018-12-31 2018-12-31 Folding joint and multi-rotor unmanned aerial vehicle with it Expired - Fee Related CN209581842U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822265809.3U CN209581842U (en) 2018-12-31 2018-12-31 Folding joint and multi-rotor unmanned aerial vehicle with it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822265809.3U CN209581842U (en) 2018-12-31 2018-12-31 Folding joint and multi-rotor unmanned aerial vehicle with it

Publications (1)

Publication Number Publication Date
CN209581842U true CN209581842U (en) 2019-11-05

Family

ID=68350769

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201822265809.3U Expired - Fee Related CN209581842U (en) 2018-12-31 2018-12-31 Folding joint and multi-rotor unmanned aerial vehicle with it

Country Status (1)

Country Link
CN (1) CN209581842U (en)

Similar Documents

Publication Publication Date Title
CN203528812U (en) Foldable four-rotor aircraft
US10513332B2 (en) Tiltwing aircraft
EP3241741B1 (en) Foldable unmanned aerial vehicle
CN207072432U (en) A kind of undercarriage and the unmanned plane with this undercarriage
EP1057724A3 (en) Tilt-rotor aircraft
CN204895844U (en) Many rotor unmanned aerial vehicle
CN206394882U (en) A kind of Novel crashproof folding rotor arm configuration
CN209581842U (en) Folding joint and multi-rotor unmanned aerial vehicle with it
CN207580155U (en) A kind of unmanned plane undercarriage folded piece
CN202481312U (en) Unidirectional flapping mechanism capable of realizing two-dimensional motion
CN109606634B (en) Double-shaft wing folding mechanism
CN106229604B (en) A kind of large size two-stage telescopic circular flat antenna
CN106347649B (en) Blade connector and coaxial double-oar structure and unmanned plane
CN205469768U (en) Support arm turn mechanism suitable for large -scale many rotors
CN206407117U (en) Folding multi-rotor unmanned aerial vehicle
CN204452927U (en) For the folding device of many rotor wing unmanned aerial vehicles
CN109025025A (en) A kind of plane retractable Roof Structures that achievable two-way linkage folds
CN106672233A (en) Novel folding rotor arm structure of unmanned aerial vehicle
CN205469799U (en) Six collapsible rotor crafts
CN208085992U (en) Novel multi-rotor unmanned aerial vehicle airframe structure and unmanned plane
CN110203421A (en) Empennage and aircraft comprising the empennage
CN206417201U (en) Unmanned plane
CN207712283U (en) A kind of folding arm configuration suitable for multi-rotor unmanned aerial vehicle
CN109606468A (en) A kind of steering link structure
CN206885330U (en) Horn, Power Component and unmanned plane

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: 20191105

Termination date: 20201231