CN206494123U - A kind of aircraft - Google Patents
A kind of aircraft Download PDFInfo
- Publication number
- CN206494123U CN206494123U CN201621466498.1U CN201621466498U CN206494123U CN 206494123 U CN206494123 U CN 206494123U CN 201621466498 U CN201621466498 U CN 201621466498U CN 206494123 U CN206494123 U CN 206494123U
- Authority
- CN
- China
- Prior art keywords
- hole
- lower house
- center
- upper shell
- connecting rod
- Prior art date
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- Expired - Fee Related
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Abstract
The utility model discloses the main machine body of a kind of aircraft, including sphere structure, horn in main machine body with cup-shaped motor connection, cup-shaped motor is connected with propeller, and electric motor protecting circle part is provided with cup-shaped motor；Main machine body includes upper shell and the lower house being connected with upper shell, it is connected with upper shell on controller and circuit board, lower house and is connected with battery, center bearing bracket is provided with lower house, drive mechanism is provided with center bearing bracket, drive mechanism is connected with upper shell by center connecting rod.A kind of aircraft has the flat VTOL flown with helicopter of fixed-wing concurrently upon deployment, it is not necessary to big place, adapts to the flight condition of interior.
Description
Technical field
The utility model belongs to aeromodelling aerocraft technical field, is related to a kind of aircraft.
Background technology
Existing most fixed wing aircrafts in life, dummy vehicle, for the manipulator without systematic training
For, improper damage aircraft easy to operate causes people's wealth to injure, and loses game-play enjoyment, and is required for wide field mostly
Ground is used for takeoff and landing, it is impossible to adapt to the flight condition under some indoor and complex environments.
Utility model content
The purpose of this utility model is the provision of a kind of aircraft, and the aircraft does not need big place, adapts to room
Interior flight condition.
The utility model is the technical scheme adopted is that a kind of aircraft, is included in the main machine body of sphere structure, main machine body
Horn with cup-shaped motor connection, cup-shaped motor is connected with propeller, and electric motor protecting circle part is provided with cup-shaped motor；
Main machine body includes being provided with controller and circuit board in upper shell and the lower house being connected with upper shell, upper shell,
Be provided with lower house in battery, lower house and be provided with center bearing bracket, be provided with drive mechanism on center bearing bracket, drive mechanism with
Upper shell is connected by center connecting rod.
The characteristics of the utility model, also resides in, and is provided with the top of lower house on several spacing holes, the side of lower house
Four spacing convex bodys are provided with, lower house structure includes guard circle shrinkage hole and the stent collapses connected with guard circle shrinkage hole
Battery board bracket connecting hole is provided with hole, lower house.
The bottom of upper shell is provided with the spacing convex body being engaged with spacing hole, upper shell and is provided with circuit board mounting hole
With center nut mounting hole b.
Electric motor protecting circle part includes motor base, and cup-shaped motor is located in motor base, is set on each motor base
There is heat emission hole, one end of motor base is connected with horn, and the other end of motor base is connected with foot support, foot support upper end is set
There is propeller guard circle.
Drive mechanism includes driving gear, and driving gear is connected by center connecting rod with center bearing bracket, on driving gear
Four driven gears are engaged with, driven gear is connected with driven gear connecting rod, and driven gear connecting rod is connected with center bearing bracket,
Driven gear connecting rod is connected with horn, and horn may be collapsed in guard circle shrinkage hole.
Drive mechanism includes pull bar rotating disk, is provided with centre bore on pull bar rotating disk, pull bar rotating disk by center connecting rod with
Center bearing bracket is connected, and pull bar rotating disk is cross, and cross four end points of pull bar rotating disk are provided with pull bar screw hole, and screw is worn
Cross pull bar screw hole to be connected horn with pull bar rotating disk, horn part is stretched into guard circle shrinkage hole.
Circuit board is connected by circuit board support with upper shell, be provided with circuit board support center nut mounting hole a and
Lower house is installed in bayonet socket, upper shell and is provided with circuit board mounting hole and center nut mounting hole b, circuit board mounting hole and lower casing
Body is installed bayonet socket and connected by nut, and center connecting rod passes through centre bore, and center connecting rod one end connects with center nut mounting hole b
Connect, the center connecting rod other end is connected through battery board bracket mounting hole with center nut mounting hole a.
Lower house is connected by battery board bracket and battery, and battery charging hole and cell panel branch are provided with battery board bracket
Frame mounting hole, battery board bracket in battery board bracket connecting hole with lower house by being connected.
The base of cup-shaped motor is equipped with LED mounting seat, each LED mounting seat and is provided with LED and LED
Cover.
LED Colour lamps are provided with upper shell and lower house.
The beneficial effects of the utility model are：A kind of aircraft has the flat winged vertical with helicopter of fixed-wing concurrently upon deployment
Straight landing, it is not necessary to big place, it is not necessary to particularly preferred operating technology, can just fly indoors, overall after shrinking to protect
Hold as a spheroid form that can be lighted；Secondly, the utility model overall construction design is compact, and whole electronic equipments are realized
Encapsulation, appearance looks elegant is generous, handling good, and operation facility, accurate positioning, cost is relatively low.The utility model realizes collection function
With entertaining integrated bionical personalized designs, whole aircraft reliability height, manipulation is flexibly.It disclosure satisfy that different age group flight hobby
The demand of person.
Brief description of the drawings
Fig. 1 is a kind of structural representation of aircraft of the utility model；
Fig. 2 is the structural representation of drive mechanism embodiment one in a kind of aircraft of the utility model；
Fig. 3 is the connection figure of aircraft guard circle, support and motor in a kind of aircraft of the utility model；
Fig. 4 is the structural representation of lower house in a kind of aircraft reality of the utility model；
Fig. 5 is the structural representation of upper shell in a kind of aircraft reality of the utility model；
Fig. 6 is the structural representation of battery bracket in a kind of aircraft reality of the utility model；
Fig. 7 is the structural representation of circuit board support in a kind of aircraft reality of the utility model；
Fig. 8 is the structural representation for removing upper shell embodiment one in a kind of aircraft of the utility model；
Fig. 9 is to remove the structural representation that upper shell applies example two in a kind of aircraft of the utility model；
Figure 10 is the structural representation that drive mechanism applies example two in a kind of aircraft reality of the utility model.
In figure, 1. drive mechanisms, 1-1. driving gears, 1-2. driven gears, 1-3. driven gear connecting rods, 1-4. centers
Hole, 1-5. centers connecting rod, 1-6. center bearing brackets, 1-7. pull bar rotating disks, 1-8. pull bar screw holes,
2. electric motor protecting circle part, 2-1. propellers, 2-2. horns, 2-3. motor bases, 2-4. foot supports, 2-5. spiral shells
Oar guard circle is revolved,
3. lower house, 3-1. spacing holes, 3-2. guard circle shrinkage holes, 3-3. stent collapses hole, 3-4. battery board brackets connect
Connect hole,
4. upper shell, the spacing convex bodys of 4-1., 4-2 circuit board mounting holes, 4-3. center nut mounting hole b,
5-1. battery board brackets, 5-2. battery board bracket mounting holes, 5-3. batteries charging hole,
6-1. circuit board supports, 6-2. lower houses install bayonet socket, 6-3. center nut mounting holes a.
Embodiment
The utility model is described in detail with reference to the accompanying drawings and detailed description.
The utility model provides a kind of aircraft, as Figure 1-Figure 8, includes the main machine body of sphere structure, main machine body
On horn 2-2 with cup-shaped motor connection, cup-shaped motor is connected with propeller 2-1, and electric motor protecting is provided with cup-shaped motor
Enclose part 2；
Main machine body includes being connected with controller and circuit in upper shell 4 and the lower house 3 being connected with upper shell 4, upper shell 4
It is connected with plate, lower house 3 in battery, lower house 3 and is provided with center bearing bracket 1-6, drive mechanism is provided with center bearing bracket 1-6
1, drive mechanism 1 is connected with upper shell 4 by center connecting rod 1-5；
The top periphery of lower house 3 be provided with several spacing holes 3-1, the side of lower house 3 be provided with four it is spacing
Structure, lower house includes guard circle shrinkage hole 3-2 and the stent collapses hole 3-3 connected with guard circle shrinkage hole 3-2, lower house 3
On be provided with battery board bracket connecting hole 3-4；
Electric motor protecting circle part 2 includes motor base 2-3, and cup-shaped motor is located in motor base 2-3, each motor bottom
Heat emission hole is provided with seat 2-3, motor base 2-3 one end is connected with horn 2-2, motor base the 2-3 other end and pin branch
Frame 2-4 connections, foot support 2-4 upper ends are provided with propeller guard circle 2-5；
As shown in Fig. 2 drive mechanism 1 includes being provided with centre bore 1-4 on driving gear 1-1, driving gear 1-1, actively
Gear 1-1 is connected by center connecting rod 1-5 with center bearing bracket 1-6, and four driven gear 1- are engaged with driving gear 1-1
2, driven gear 1-2 are connected with driven gear connecting rod 1-3, and driven gear connecting rod 1-3 is connected with center bearing bracket 1-6, driven
Gear connecting rod 1-3 is connected with horn 2-2, and horn 2-2 is stretched into guard circle shrinkage hole 3-2 part；
As shown in Figure 9 and Figure 10, drive mechanism 1 includes being provided with centre bore 1- on pull bar rotating disk 1-7, pull bar rotating disk 1-7
4, pull bar rotating disk 1-7 are connected by center connecting rod 1-5 with center bearing bracket 1-6, and pull bar rotating disk 1-7 is cross to be cross
Tetra- end points of pull bar rotating disk 1-7 are provided with pull bar screw hole 1-8, and screw turns horn 2-2 and pull bar through pull bar screw hole 1-8
Disk 1-7 connections, horn 2-2 is stretched into guard circle shrinkage hole 3-2 part；
The bottom of upper shell 4 is provided with the spacing convex body 4-1 being engaged with spacing hole 3-1, upper shell 4 and is provided with circuit
Plate mounting hole 4-2 and center nut mounting hole b4-3；
Circuit board is connected by circuit board support 6-1 with upper shell 4, and center nut peace is provided with circuit board support 6-1
Fill hole a6-3 and lower house is installed in bayonet socket 6-2, upper shell 4 and is provided with circuit board mounting hole 4-2 and center nut mounting hole b4-
3, circuit board mounting hole 4-2 install bayonet socket 6-2 with lower house and are connected by nut, and center connecting rod 1-5 passes through centre bore 1-4,
Center connecting rod 1-5 one end is connected with center nut mounting hole b4-3, and the center connecting rod 1-5 other ends are pacified through battery board bracket
Dress hole 5-2 is connected with center nut mounting hole a6-3；
Lower house 3 is connected by battery board bracket 5-1 and battery, and battery charging hole 5-3 is provided with battery board bracket 5-1
With battery board bracket mounting hole 5-2, battery board bracket 5-1 in battery board bracket connecting hole 3-4 with lower house 3 by being connected；
The base of cup-shaped motor is equipped with LED mounting seat, each LED mounting seat and is provided with LED and LED
Cover；
LED Colour lamps are provided with upper shell 4 and lower house 3.
A kind of operation principle of aircraft of the utility model is：
When external force acts on upper shell 4, upper shell 4 drives driving gear 1-1 to rotate by center connecting rod 1-5, main
Moving gear 1-1 drives driven gear 1-2 rotations, and driven gear 1-2 is connected with driven gear connecting rod 1-3, driven gear connection
Bar 1-3 is connected with center bearing bracket 1-6, and driven gear connecting rod 1-3 is connected with horn 2-2, and horn 2-2 is around driven gear connecting rod
1-3 rotate so that foot support 2-4 be located at position limiting structure guard circle shrinkage hole 3-2 and with guard circle shrinkage hole 3-2, motor
Base 2-3 is being shunk inside lower house 3, and propeller guard circle 2-5 and foot support 2-4 are close to the shell of lower house 3, pin branch
Frame 2-4 deploys simultaneously with motor base 2-3 in the deployed state, plays a part of support；
Or when external force acts on upper shell 4, upper shell 4 drives pull bar rotating disk 1-7 to revolve by center connecting rod 1-5
Turn, pull bar rotating disk 1-7 drives horn 2-2 to be rotated around pull bar rotating disk 1-7 so that foot support 2-4 is located at the guard circle of position limiting structure
Shrinkage hole 3-2 and with guard circle shrinkage hole 3-2, motor base 2-3 shrink be located at lower house 3 inside, propeller guard circle
2-5 and foot support 2-4 are close to the shell of lower house 3, and foot support 2-4 deploys simultaneously with motor base 2-3 in the deployed state,
Play a part of support；
Cup-shaped motor is located in motor base 2-3, and motor base 2-3 is provided with heat emission hole, plays a part of motor radiating；
Controller, battery and circuit board apparatus all wrap up in the main frame that abdomen connects into sphere structure in upper shell 4 and lower house 3
Within body, compact conformation is realized, propeller 2-1 has been included in inside main machine body while employing propeller guard circle 2-5,
Enhance the security performance of flight, and will not change of flight device aeroperformance；
Meanwhile, LED Colour lamps are provided with upper shell 4 and lower house 3, in the state of being shunk generally in one kind
It can work as and become a kind of illuminator of spheroid.
A kind of aircraft of the present utility model has the flat VTOL flown with helicopter of fixed-wing concurrently upon deployment, is not required to
Big place is wanted, the flight condition of interior is adapted to, it is not necessary to particularly preferred operating technology, can just fly indoors, is being received
A spheroid form that can be lighted integrally is remained after contracting；Secondly, the utility model overall construction design is compact, whole electronics
Equipment realizes encapsulation, and appearance looks elegant is generous, handling good, and operation facility, accurate positioning, cost is relatively low.The utility model is real
Collection function and entertaining integrated bionical personalized designs are showed, whole aircraft reliability is high, and manipulation is flexible.It disclosure satisfy that all ages and classes
The demand of section airhog.
Claims (10)
1. a kind of aircraft, it is characterised in that：Horn (2-2) in main machine body including sphere structure, main machine body is and cup-shaped
Motor connection, cup-shaped motor is connected with propeller (2-1), and electric motor protecting circle part (2) is provided with cup-shaped motor；
Main machine body include being connected with upper shell (4) and the lower house (3) that be connected with upper shell (4), upper shell (4) controller with
It is connected with to be provided with center bearing bracket (1-6), center bearing bracket (1-6) in battery, lower house (3) on circuit board, lower house (3) and sets
Drive mechanism (1) is equipped with, drive mechanism (1) is connected with upper shell (4) by center connecting rod (1-5).
2. a kind of aircraft according to claim 1, it is characterised in that：It is provided with the top of the lower house (3) some
Four position limiting structures are provided with individual spacing hole (3-1), the side of lower house (3), position limiting structure includes guard circle shrinkage hole (3-
2) battery board bracket connection is provided with the stent collapses hole (3-3) and with guard circle shrinkage hole (3-2) connected, lower house (3)
Hole (3-4).
3. a kind of aircraft according to claim 2, it is characterised in that：The bottom of the upper shell (4) is provided with and limited
Circuit board mounting hole (4-2) and center nut peace are provided with the spacing convex body (4-1) that position hole (3-1) is engaged, upper shell (4)
Fill hole b (4-3).
4. a kind of aircraft according to claim 3, it is characterised in that：The electric motor protecting circle part (2) includes motor
Base (2-3), cup-shaped motor is located in motor base (2-3), and heat emission hole, motor bottom are provided with each motor base (2-3)
One end of seat (2-3) is connected with horn (2-2), and the other end of motor base (2-3) is connected with foot support (2-4), foot support (2-
4) upper end is provided with propeller guard circle (2-5).
5. a kind of aircraft according to claim 4, it is characterised in that：The drive mechanism (1) includes driving gear (1-
1) centre bore (1-4), is provided with driving gear (1-1), driving gear (1-1) passes through center connecting rod (1-5) and center branch
Frame (1-6) is connected, and four driven gears (1-2) are engaged with driving gear (1-1), and driven gear (1-2) connects with driven gear
Extension bar (1-3) is connected, and driven gear connecting rod (1-3) is connected with center bearing bracket (1-6), driven gear connecting rod (1-3) and machine
Arm (2-2) is connected, and horn (2-2) is partly stretched into guard circle shrinkage hole (3-2).
6. a kind of aircraft according to claim 4, it is characterised in that：The drive mechanism (1) includes pull bar rotating disk (1-
7) centre bore (1-4), is provided with pull bar rotating disk (1-7), pull bar rotating disk (1-7) passes through center connecting rod (1-5) and center branch
Frame (1-6) is connected, and pull bar rotating disk (1-7) is cross, and cross four end points of pull bar rotating disk (1-7) are provided with pull bar screw
Horn (2-2) is connected by hole (1-8), screw through pull bar screw hole (1-8) with pull bar rotating disk (1-7), and horn (2-2) is partly stretched
Enter in guard circle shrinkage hole (3-2).
7. a kind of aircraft according to claim 5 or 6, it is characterised in that：The circuit board passes through circuit board support (6-
1) it is connected with upper shell (4), center nut mounting hole a (6-3) is provided with circuit board support (6-1) and lower house installs bayonet socket
Circuit board mounting hole (4-2) and center nut mounting hole b (4-3), circuit board mounting hole are provided with (6-2), upper shell (4)
(4-2) installs bayonet socket (6-2) with lower house and is connected by nut, and center connecting rod (1-5) passes through centre bore (1-4), and center connects
Extension bar (1-5) one end is connected with center nut mounting hole b (4-3), and center connecting rod (1-5) other end is pacified through battery board bracket
Dress hole (5-2) is connected with center nut mounting hole a (6-3).
8. a kind of aircraft according to claim 5 or 6, it is characterised in that：The lower house (3) passes through battery board bracket
(5-1) and battery are connected, and battery charging hole (5-3) and battery board bracket mounting hole (5- are provided with battery board bracket (5-1)
2), battery board bracket (5-1) in battery board bracket connecting hole (3-4) with lower house (3) by being connected.
9. a kind of aircraft according to claim 5 or 6, it is characterised in that：The base of the cup-shaped motor is equipped with LED
LED and LED lamp cover are provided with lamp mounting seat, each LED mounting seat.
10. a kind of aircraft according to claim 5 or 6, it is characterised in that：In the upper shell (4) and lower house (3)
It is provided with LED Colour lamps.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621466498.1U CN206494123U (en) | 2016-12-29 | 2016-12-29 | A kind of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621466498.1U CN206494123U (en) | 2016-12-29 | 2016-12-29 | A kind of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206494123U true CN206494123U (en) | 2017-09-15 |
Family
ID=59801832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621466498.1U Expired - Fee Related CN206494123U (en) | 2016-12-29 | 2016-12-29 | A kind of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206494123U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911171A (en) * | 2019-04-30 | 2019-06-21 | 杜双昱 | Horn rotates synchronously structure and the industrial unmanned plane with the structure |
| CN111559506A (en) * | 2020-05-27 | 2020-08-21 | 上海倬彼云汉航空科技有限公司 | A many rotor unmanned aerial vehicle for agricultural expelling |
| CN111591471A (en) * | 2020-04-30 | 2020-08-28 | 南京理工大学 | Braking sail derailing device applied to standing satellite |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
-
2016
- 2016-12-29 CN CN201621466498.1U patent/CN206494123U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911171A (en) * | 2019-04-30 | 2019-06-21 | 杜双昱 | Horn rotates synchronously structure and the industrial unmanned plane with the structure |
| CN109911171B (en) * | 2019-04-30 | 2023-11-14 | 杜双昱 | Synchronous rotating structure of horn and have industry unmanned aerial vehicle of this structure |
| CN111591471A (en) * | 2020-04-30 | 2020-08-28 | 南京理工大学 | Braking sail derailing device applied to standing satellite |
| CN111559506A (en) * | 2020-05-27 | 2020-08-21 | 上海倬彼云汉航空科技有限公司 | A many rotor unmanned aerial vehicle for agricultural expelling |
| CN111559506B (en) * | 2020-05-27 | 2021-08-24 | 上海倬彼云汉航空科技有限公司 | A many rotor unmanned aerial vehicle for agricultural expelling |
| CN111776214A (en) * | 2020-06-17 | 2020-10-16 | 广东工业大学 | Real-time imaging device for road survey |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170915 Termination date: 20171229 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |