CN205819558U - aircraft rotor driver mounting seat - Google Patents
aircraft rotor driver mounting seat Download PDFInfo
- Publication number
- CN205819558U CN205819558U CN201620729384.5U CN201620729384U CN205819558U CN 205819558 U CN205819558 U CN 205819558U CN 201620729384 U CN201620729384 U CN 201620729384U CN 205819558 U CN205819558 U CN 205819558U
- Authority
- CN
- China
- Prior art keywords
- mounting seat
- rotor driver
- seat body
- horn
- aircraft rotor
- 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
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- Toilet Supplies (AREA)
Abstract
The utility model discloses a kind of aircraft rotor driver mounting seat, including mounting seat body, mounting seat body is downward opening shell structure, the top of mounting seat body is provided with the mounting plane for installing rotor driver, connect on mounting seat body portion sidewall and have the horn branch sleeve forwards stretched out, the endoporus of horn branch sleeve and the intracavity inter-connection of mounting seat body.This aircraft rotor driver mounting seat can connect with horn and be used for installing rotor driver, after using this aircraft rotor driver mounting seat, horn and rotor driver are installed toilet and be can be designed as general version, be conducive to the cross-species transferability of aircraft, reduce the workload of design.
Description
Technical field
This utility model relates to a kind of aircraft rotor driver mounting seat.
Background technology
Many rotor unmanned aircrafts are able in recent years because it has the advantages such as simple in construction, flexible operation, load capacity are strong
Developing rapidly, this aircraft is widely used in fields such as shooting, plant protection.Many rotor unmanned aircrafts include body, on body
It is provided with multiple horn, horn is provided with rotor driver, rotor driver is provided with rotor, rotor driver drive rotation
The wing rotates.Existing rotor driver is to be directly installed on horn, it is therefore desirable to horn does special design, to adapt to rotation
The installation requirements of wing driver.And the model of aircraft is varied, the aircraft of each model is required for being equipped with special machine
Arm, the workload of design is bigger.
Summary of the invention
The purpose of this utility model is for a kind of aircraft rotor driver can being connected with horn of above-mentioned not enough offer
Mounting seat, after using this aircraft rotor driver mounting seat, horn may be designed as general form, beneficially aircraft
Cross-species transferability.
For achieving the above object, this utility model includes mounting seat body, and it is structurally characterized in that described mounting seat body is
Downward opening shell structure, the top of mounting seat body is provided with the mounting plane for installing rotor driver, and mounting seat is originally
Connecting on the sidewall of body front portion and have the horn branch sleeve forwards stretched out, the endoporus of horn branch sleeve is interior with mounting seat body
Chamber is connected.
It is provided with the reinforcement connecting portion protruding its surface inside the roof of described mounting seat body, strengthens connecting portion and include middle part
Boss and be four strip convex tendons of radiation profiles to its periphery after middle part boss is drawn, middle part boss is provided with circular logical
Hole, bar shaped convex tendon is provided with the strip through hole consistent with its length direction.
The front end of described horn branch sleeve is provided with two adjustment gaps extended along its length, and two adjust gap phase
To setting, the both sides adjusting gap respectively set a lug, and lug is provided with and is fastenedly connected hole.
Described horn branch sleeve is provided with hole, location.
The profile of described horn branch sleeve is prism-shaped.
Described mounting seat body roof is provided with the through wires hole that supply lines passes.
The sidewall of described mounting seat body is provided with multiple louvre.
Described horn branch sleeve is provided with multiple lightening hole.
The bottom of described mounting seat body connects cover plate.
Described cover plate is provided with the adnexa connecting portion protruded to sidepiece.
After using said mechanism, horn branch sleeve is for connecting with horn, and after installation, mounting plane is upward, rotor
Driver may be installed at mounting plane, can install the electric unit suitable with rotor driver in the inner chamber of mounting seat body
Part, the wire drawn from aircraft body can be incorporated into mounting seat by the inner chamber of horn through the endoporus of horn branch sleeve
Connecting with electrical equipment in the inner chamber of body, electrical equipment is connected with rotor driver by wire again, and the most whole circuit can set
Put the inside at aircraft, it is ensured that the safety and stability of aircraft work.This aircraft rotor driver mounting seat can be with horn
Connecting and be used for installing rotor driver, after using this aircraft rotor driver mounting seat, horn and rotor driver are installed
Toilet can be designed as the cross-species transferability of general version, beneficially aircraft, reduces the workload of design.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings detailed description of the invention of the present utility model is further described in detail:
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the top view of Fig. 1；
Fig. 3 is the right view of Fig. 1；
Fig. 4 is along the structural representation after line A-A cutting in Fig. 1；
Fig. 5 is along the structural representation after line B-B cutting in Fig. 4.
Detailed description of the invention
Referring to the drawings, this aircraft rotor driver mounting seat includes that mounting seat body 1, mounting seat body 1 are opening court
Under shell structure, the top of mounting seat body 1 is provided with the mounting plane 2 for installing rotor driver, before mounting seat body 1
Connecting on portion's sidewall and have the horn branch sleeve 3 forwards stretched out, the endoporus of horn branch sleeve 3 is interior with mounting seat body 1
Chamber is connected.Horn branch sleeve 3 is for connecting with horn, and horn may be designed to cylinder or prism structure, horn branch sleeve 3
Endoporus be corresponding shape, preferred horn is cylindrical, and the endoporus of horn branch sleeve 3 is circular hole, and horn connects
Sleeve 3 is sleeved on the end of horn connection fixed thereto, and after installation, mounting plane 2 is upward, and rotor driver can be installed
At mounting plane 2, rotor driver is generally motor, owing to mounting seat body 1 is downward opening shell structure, and horn
The endoporus of branch sleeve 3 and the intracavity inter-connection of mounting seat body 1, can install in the inner chamber of mounting seat body 1 and drive with rotor
The electrical equipment that dynamic device is suitable, the wire drawn from aircraft body can be by the inner chamber of horn through horn branch sleeve 3
Endoporus be incorporated in the inner chamber of mounting seat body 1 with electrical equipment connects, electrical equipment is again by wire and rotor driver
Connecting, the most whole circuit may be provided at the inside of aircraft, it is ensured that the safety and stability of aircraft work.This aircraft is used to revolve
After wing driver mounting seat, horn and rotor driver are installed toilet and be can be designed as general version, are conducive to flight
The cross-species transferability of device.
It is provided with the reinforcement connecting portion protruding its surface inside the roof of mounting seat body 1, strengthens connecting portion and include that middle part is convex
Platform 14 and be four strip convex tendons 15 of radiation profiles to its periphery after middle part boss 14 is drawn, middle part boss 14 is provided with
Manhole, bar shaped convex tendon 15 is provided with the strip through hole consistent with its length direction.Strengthen connecting portion as a rib
Position is for connecting with rotor driver, and manhole can carry out location and installation to rotor driver, and strip through hole is for rotation
The bolt of wing driver is fixed.
The front end of horn branch sleeve 3 is provided with two adjustment gaps 5 extended along its length, and two adjust gap 5 phase
To setting, the both sides adjusting gap 5 respectively set a lug 6, and lug 6 is provided with and is fastenedly connected hole 7.Article two, adjust gap 5 by machine
The fore-end of arm branch sleeve 3 is slit into two connecting portions, and two connecting portions have certain deformation quantity, and two connecting portions can mutually lean on
Closely, thus with horn linking together tightly, the lug 6 being located at the both sides adjusting gap 5 and the fastening that is located on lug 6 even
Connect hole 7 to connect for bolt.
Horn branch sleeve 3 is provided with hole 8, location.Hole 8, location may be provided in any position of horn branch sleeve 3, location
Alignment pin or bolt, the location between horn branch sleeve 3 and horn can be installed at hole 8.
The profile of horn branch sleeve 3 is prism-shaped.After being designed to this shape, can be easy to during assembling it is pressed from both sides
Hold.
Mounting seat body 1 roof is provided with the through wires hole 9 that supply lines passes, on the electrical equipment in mounting seat body 1 inner chamber
Connection wire can from through wires hole 9 pass after be attached with rotor driver.
The sidewall of mounting seat body 1 is provided with multiple louvre 10.Can be to being arranged on installation by these louvres 10
Electrical equipment in seat body 1 inner chamber dispels the heat, and can also alleviate the entirety of mounting seat body 1 by arranging of louvre 10
The light-duty design of weight, beneficially aircraft.
Horn branch sleeve 3 is provided with multiple lightening hole 11.It is beneficial to alleviate horn connection by being provided with of lightening hole 11
The weight of sleeve 3.
The bottom of mounting seat body 1 connects cover plate 12.Cover plate 12 can block the opening part at mounting seat body 1, with more
Other adnexa can also be connected on good protection its internal electric elements, and cover plate 12.
Cover plate 12 is provided with the adnexa connecting portion 13 protruded to sidepiece, and adnexa connecting portion 13 can connect aircraft phase Radix Aconiti Coreani
Part, it is for passing through away from rotor, beneficially air-flow that adnexa connecting portion 13 protrudes to sidepiece, it is ensured that aircraft working stability.
In sum, this utility model is not limited to above-mentioned detailed description of the invention.Those skilled in the art, without departing from this reality
On the premise of novel spirit and scope, some changes and modification can be done.Protection domain of the present utility model should be with this reality
It is as the criterion by novel claim.
Claims (10)
1. an aircraft rotor driver mounting seat, including mounting seat body (1), is characterized in that described mounting seat body (1)
For downward opening shell structure, the top of mounting seat body (1) is provided with the mounting plane (2) for installing rotor driver,
Connect on the anterior sidewall of mounting seat body (1) and have the horn branch sleeve (3) forwards stretched out, horn branch sleeve (3) interior
Hole and the intracavity inter-connection of mounting seat body (1).
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that the top of described mounting seat body (1)
It is provided with the reinforcement connecting portion protruding its surface inside wall, strengthens connecting portion and include middle part boss (14) and draw from middle part boss (14)
After going out is four strip convex tendons (15) of radiation profiles to its periphery, and middle part boss (14) is provided with manhole, and bar shaped is convex
Muscle (15) is provided with the strip through hole consistent with its length direction.
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that described horn branch sleeve (3)
Front end is provided with two adjustment gaps (5) extended along its length, and two adjust gap (5) is oppositely arranged, and adjusts gap (5)
Both sides respectively set a lug (6), and lug (6) is provided with and is fastenedly connected hole (7).
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that on described horn branch sleeve (3)
It is provided with hole, location (8).
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that described horn branch sleeve (3)
Profile is prism-shaped.
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that described mounting seat body (1) roof
It is provided with the through wires hole (9) that supply lines passes.
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that the side of described mounting seat body (1)
Wall is provided with multiple louvre (10).
Aircraft rotor driver mounting seat the most according to claim 1, is characterized in that on described horn branch sleeve (3)
It is provided with multiple lightening hole (11).
9., according to the aircraft rotor driver mounting seat described in any claim in claim 1 to 8, it is characterized in that described
The bottom of mounting seat body (1) connects cover plate (12).
Aircraft rotor driver mounting seat the most according to claim 9, it is characterized in that described cover plate (12) be provided with to
The adnexa connecting portion (13) that sidepiece protrudes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620729384.5U CN205819558U (en) | 2016-07-12 | 2016-07-12 | aircraft rotor driver mounting seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620729384.5U CN205819558U (en) | 2016-07-12 | 2016-07-12 | aircraft rotor driver mounting seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205819558U true CN205819558U (en) | 2016-12-21 |
Family
ID=57565406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620729384.5U Expired - Fee Related CN205819558U (en) | 2016-07-12 | 2016-07-12 | aircraft rotor driver mounting seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205819558U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109969375A (en) * | 2019-04-30 | 2019-07-05 | 广州极飞科技有限公司 | Unmanned plane |
-
2016
- 2016-07-12 CN CN201620729384.5U patent/CN205819558U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109969375A (en) * | 2019-04-30 | 2019-07-05 | 广州极飞科技有限公司 | Unmanned plane |
| CN109969375B (en) * | 2019-04-30 | 2024-04-26 | 广州极飞科技股份有限公司 | Unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20161221 Termination date: 20190712 |