CN205686608U - Quadrotor frame is patrolled and examined in well site - Google Patents
Quadrotor frame is patrolled and examined in well site Download PDFInfo
- Publication number
- CN205686608U CN205686608U CN201620598725.XU CN201620598725U CN205686608U CN 205686608 U CN205686608 U CN 205686608U CN 201620598725 U CN201620598725 U CN 201620598725U CN 205686608 U CN205686608 U CN 205686608U
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- CN
- China
- Prior art keywords
- horn
- lower platform
- mounting plate
- patrolled
- examined
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- 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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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses a kind of simple in construction, flight stability, it is simple to arrange the equipment that oil well is patrolled and examined, and quadrotor frame is patrolled and examined in the good well site of explosion-proof effect.Including fuselage, horn, fuselage includes the upper mounting plate of Rectangular Plate Structure, lower platform, upper mounting plate is provided with and flies to control fixed bin, upper mounting plate, pillar is fixed between lower platform, make upper mounting plate, cube cavity is formed between lower platform, it is provided with battery case in cube cavity, the lower end of battery case is fixed on lower platform, for placing the battery that aircraft is powered in battery case, horn is Z-shape, Z-shaped horn is by upper arm, underarm, linking arm forms, four horns are positioned at the corner of fuselage, the underarm of each horn is fixed on the lower end of lower platform corresponding angles, the upper arm of horn is provided for installing the motor cabinet of rotor direct current generator, the electricity being provided for installing electron speed regulator on the linking arm of each horn adjusts fixed bin；The protection cap that insulation explosion-proof material is made it is stamped on fuselage.
Description
Technical field
This utility model relates to unmanned vehicle technical field, particularly relates to a kind of well site and patrols and examines quadrotor machine
Frame.
Background technology
The frame of existing quadrotor designs for conventional environment, and its structure is complicated, is not easy within it
Portion arranges the equipment that oil well is patrolled and examined；Further, this frame center of gravity is higher, and stability is bad, is unfavorable in narrow space
Interior flight, is unsuitable for oil well this use environment；Further, this frame insulating properties are poor, in oil well, use can bring
Serious potential safety hazard.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, it is provided that a kind of simple in construction, flight stability, it is simple to
Arrange the equipment patrolled and examined of oil well, and quadrotor frame is patrolled and examined in the good well site of explosion-proof effect.
The purpose of this utility model is achieved in that
Quadrotor frame is patrolled and examined in a kind of well site, and including fuselage, four horns, described fuselage includes rectangular tabular
The upper mounting plate of structure, lower platform, the upper surface of described upper mounting plate be provided with for install flying vehicles control plate fly control fixed bin, institute
State and between the corner of upper mounting plate, lower platform, be respectively fixedly connected with a pillar, make between upper mounting plate, lower platform, to form cube empty
Chamber, is provided with battery case in described cube cavity, the lower end of described battery case is fixed on lower platform, is used for placing in battery case
The battery powering aircraft, described horn is Z-shape, and Z-shaped horn is made up of upper arm, underarm, linking arm, described four horn positions
In the corner of fuselage, the underarm of each horn is fixed on the lower end of lower platform corresponding angles, and the upper arm of described horn is provided for installing
The motor cabinet of rotor direct current generator, the electricity linking arm of described each horn being provided for install electron speed regulator adjusts fixed bin；
Also including the protection cap using insulation explosion-proof material to make, the area of described lower platform is more than the area of upper mounting plate,
The lower end of described protection cap is positioned the marginal portion of lower platform, is used for protecting fuselage.
Preferably, described electricity adjusts fixed bin one-body molded with horn.
Preferably, described horn is weldingly fixed on lower platform.
Preferably, described motor cabinet is one-body molded with horn.
Preferably, described electricity adjust be uniformly provided with on fixed bin some for the circular hole to heat dissipation of electronic speed regulator.
Owing to have employed technique scheme, this utility model has the advantages that
1. horn described in is Z-type bending shape, handsome in appearance, can reduce aircraft center of gravity, improves aircraft stress.
2. with the addition of the protection cap that insulation explosion-proof material is made, explosion-proof effect is good, is used for ensureing the safety of petroleum well field.
3., for the use Environment Design of oil well, improve other aircraft frame and cannot fix electricity adjusted position and battery
The problem of position, reasonable structural arrangement.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
Quadrotor frame is patrolled and examined in a kind of well site, and including fuselage, four horns, described fuselage includes rectangular tabular
The upper mounting plate 3 of structure, lower platform 8, the upper surface of described upper mounting plate 3 be provided with for install flying vehicles control plate fly control fixed bin
2, described upper mounting plate 3, lower platform 8 corner between be respectively fixedly connected with a pillar 7, make shape between upper mounting plate 3, lower platform 8
Becoming cube cavity, be provided with battery case 9 in described cube cavity, the lower end of described battery case 9 is fixed on lower platform 8, electricity
For placing the battery powering aircraft in pond box 9, described horn is Z-shape, and Z-shaped horn is by upper arm, underarm, linking arm group
Becoming, described four horns are positioned at the corner of fuselage, and the underarm of each horn is fixed on the lower end of lower platform 8 corresponding angles, the present embodiment
In, described horn 5 is weldingly fixed on lower platform 8.The upper arm of described horn is provided for installing the motor of rotor direct current generator
Seat 6, in the present embodiment, described motor cabinet 6 is one-body molded with horn 5.It is provided on the linking arm of described each horn electricity is installed
The electricity of sub-speed regulator adjusts fixed bin 4, and in the present embodiment, described electricity adjusts fixed bin 4 one-body molded with horn 5, and described electricity is adjusted fixing
It is uniformly provided with some for the circular hole to heat dissipation of electronic speed regulator on box 4.
Also including the protection cap 1 using insulation explosion-proof material to make, the area of described lower platform 8 is more than the face of upper mounting plate 3
Long-pending, the lower end of described protection cap 1 is positioned the marginal portion of lower platform 8, to be used for protecting fuselage.
Finally illustrating, preferred embodiment above is only in order to illustrate the technical solution of the utility model and unrestricted, to the greatest extent
This utility model is described in detail by pipe by above preferred embodiment, but those skilled in the art should manage
Solve, in the form and details it can be made various change, without departing from this utility model claims institute
The scope limited.
Claims (5)
1. a quadrotor frame is patrolled and examined in well site, including fuselage, four horns, it is characterised in that: described fuselage includes
The upper mounting plate (3) of rectangular platy structure, lower platform (8), the upper surface of described upper mounting plate (3) is provided with for installing aircraft control
Making sheet fly control fixed bin (2), described upper mounting plate (3), lower platform (8) corner between be respectively fixedly connected with a pillar (7),
Make to be formed between upper mounting plate (3), lower platform (8) cube cavity, in described cube cavity, be provided with battery case (9), described electricity
The lower end of pond box (9) is fixed on lower platform (8), for placing the battery powering aircraft, described horn in battery case (9)
Z-shape, Z-shaped horn is made up of upper arm, underarm, linking arm, and described four horns are positioned at the corner of fuselage, and the underarm of each horn is solid
Being scheduled on the lower end of lower platform (8) corresponding angles, the upper arm of described horn is provided for installing the motor cabinet (6) of rotor direct current generator,
The electricity being provided for installing electron speed regulator on the linking arm of described each horn adjusts fixed bin (4)；
Also including the protection cap (1) using insulation explosion-proof material to make, the area of described lower platform (8) is more than upper mounting plate (3)
Area, the lower end of described protection cap (1) is positioned the marginal portion of lower platform (8), to be used for protecting fuselage.
Quadrotor frame is patrolled and examined in well site the most according to claim 1, it is characterised in that: described electricity adjusts fixed bin
(4) one-body molded with horn (5).
Quadrotor frame is patrolled and examined in well site the most according to claim 1, it is characterised in that: described horn (5) welds
It is fixed on lower platform (8).
Quadrotor frame is patrolled and examined in well site the most according to claim 1, it is characterised in that: described motor cabinet (6) with
Horn (5) is one-body molded.
Quadrotor frame is patrolled and examined in well site the most according to claim 1, it is characterised in that: described electricity adjusts fixed bin
(4) it is uniformly provided with some for the circular hole to heat dissipation of electronic speed regulator on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620598725.XU CN205686608U (en) | 2016-06-17 | 2016-06-17 | Quadrotor frame is patrolled and examined in well site |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620598725.XU CN205686608U (en) | 2016-06-17 | 2016-06-17 | Quadrotor frame is patrolled and examined in well site |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205686608U true CN205686608U (en) | 2016-11-16 |
Family
ID=57414798
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620598725.XU Expired - Fee Related CN205686608U (en) | 2016-06-17 | 2016-06-17 | Quadrotor frame is patrolled and examined in well site |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205686608U (en) |
-
2016
- 2016-06-17 CN CN201620598725.XU patent/CN205686608U/en not_active Expired - Fee Related
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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: 20161116 Termination date: 20180617 |