CN206417204U - A kind of aircraft power fixed mount - Google Patents
A kind of aircraft power fixed mount Download PDFInfo
- Publication number
- CN206417204U CN206417204U CN201621350161.4U CN201621350161U CN206417204U CN 206417204 U CN206417204 U CN 206417204U CN 201621350161 U CN201621350161 U CN 201621350161U CN 206417204 U CN206417204 U CN 206417204U
- Authority
- CN
- China
- Prior art keywords
- contact site
- crossbeam
- copper sheet
- fixed mount
- supporting plate
- 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
Links
Classifications
-
- 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
Landscapes
- Battery Mounting, Suspending (AREA)
Abstract
A kind of aircraft power fixed mount, including two blocks of symmetrically arranged side plates and some crossbeams between two blocks of side plates, the bottom of side plate are provided with the supporting plate extended internally, and chute is formed between supporting plate, side plate and crossbeam；Wherein one crossbeam is provided with two panels spring copper sheet, spring copper sheet includes fixed part, contact site and guide part, contact site is provided with screw, contact site is bolted on crossbeam, contact site relative level is in tilt down setting, guide part relative level is in the setting that is inclined upwardly, and fixed part, contact site and guide part are by spring copper sheet bending forming.The battery case of power supply is arranged in the chute of fixed mount, and battery case is fixed by supporting plate；Then it is in electrical contact by the lead-out terminal progress of spring copper sheet and power supply, so as to obtain the electricity of power supply；Realized and electrically connected by Elastic Contact due to spring copper sheet, it is possible to separated at any time, to realize the replacing of battery.
Description
Technical field
The utility model is related to aircraft, especially a kind of aircraft power fixed mount.
Background technology
Unmanned plane application technology is a upcoming technology.There are many new technologies on unmanned plane to be opened
Hair.Unmanned plane has very big potentiality to play a significant role in following logistics or monitoring activity.But still have some shortcomings.One
It is individual primary disadvantage is that the limitation of flight range, therefore a kind of technology should be developed to expand flight range.Allow unmanned plane during flying when
Between extension have many different methods.For example, unmanned plane can carry more or more preferable battery.This will extend the electricity of unmanned plane
Pond use time.However, it is not a nothing the matter to improve battery.Many companies are directed to improving the energy density of battery
Or the new battery technology of exploitation.However, in a short time, energy density does not have big improvement.If unmanned plane carries more
Battery, it can fly farther.But in a certain critical condition, the weight of battery becomes big, and flight range can decline again.So
The endurance of real improvement unmanned plane is can be only achieved by changing battery, in unmanned plane power technology is intelligently changed, nobody
Power supply fixed support on machine body is most important.
The content of the invention
Technical problem to be solved in the utility model is to provide a kind of aircraft power fixed mount, can realize power supply
Change.
In order to solve the above technical problems, the technical solution of the utility model is：A kind of aircraft power fixed mount, including two
The symmetrically arranged side plate of block and some crossbeams between two blocks of side plates, the bottom of the side plate, which is provided with, to extend internally
Supporting plate, form chute between the supporting plate, side plate and crossbeam；Wherein one crossbeam is provided with two flat spring copper
Piece, the spring copper sheet includes fixed part, contact site and guide part, and the contact site is provided with screw, and contact site passes through bolt
It is fixed on crossbeam, the contact site relative level is in updip in setting, the guide part relative level is tilted down
Tiltedly set, the fixed part, contact site and guide part are by spring copper sheet bending forming.Utility model works principle：Normal work
When making state, the battery case of power supply is arranged in the chute of fixed mount, and battery case is fixed by supporting plate；Then pass through
The lead-out terminal progress of spring copper sheet and power supply is in electrical contact, so as to obtain the electricity of power supply；Because spring copper sheet is relied on
Elastic Contact realizes electrical connection, it is possible to separated at any time, to realize the replacing of battery.
As an improvement, the bottom of the side plate is provided with some projections, the side correspondence high spot of the supporting plate
Provided with groove, the described raised and groove coordinates.
As an improvement, the supporting plate is bolted on the bottom of side plate.
As an improvement, the top of the crossbeam is provided with mounting hole.The mounting hole is used to be connected with the bottom plate of aircraft, so that
The whole fixed bottom for being placed on aircraft.
As an improvement, the two ends of the crossbeam are connected by bolt with side plate.
The beneficial effect that the utility model is brought compared with prior art is：
The battery case of power supply is arranged in the chute of fixed mount, and battery case is fixed by supporting plate；Then pass through
The lead-out terminal progress of spring copper sheet and power supply is in electrical contact, so as to obtain the electricity of power supply；Because spring copper sheet is relied on
Elastic Contact realizes electrical connection, it is possible to separated at any time, to realize the replacing of battery.
Brief description of the drawings
Fig. 1 is the utility model decomposition view.
Embodiment
With reference to Figure of description, the utility model is described in further detail.
As shown in figure 1, a kind of aircraft power fixed mount, including two blocks of symmetrically arranged side plates 1, located at two pieces of sides linings
Some crossbeams 2 between plate 1 and the supporting plate 3 located at the bottom of side plate 1.The crossbeam 2 equally be arranged in parallel, described
The two ends of crossbeam 2 respectively at both sides the contacts side surfaces of side plate 1 and be connected by bolt with side plate 1；The top of the crossbeam 2
Provided with mounting hole, the mounting hole is used to be connected with the bottom plate of aircraft, so that the entirely fixed bottom for being placed on aircraft.It is described
Supporting plate 3 extends internally, and the outside of supporting plate 3 is bolted on the bottom of side plate 1；The bottom of the side plate 1 is set
Have some raised 11, be provided with groove 31 at the side correspondence described raised 11 of the supporting plate 3, described raised 11 with the groove
31 coordinate.Between the supporting plate 3, side plate 1 and crossbeam 2 formed chute 4, the chute 4 can power supply source battery case insertion simultaneously
It is fixed.Wherein one crossbeam 2 is provided with two panels spring copper sheet 5, and the output end of power supply can be by the spring copper sheet 5 to flight
The control circuit of device is powered.The spring copper sheet 5 includes fixed part 51, contact site 52 and guide part 53；On the contact site 52
Provided with screw, contact site 52 is bolted on crossbeam 2；The relative level of contact site 52 is in tilt down setting,
Form the trend being pressed downward, the lead-out terminal reliable contacts that the contact site 52 can be with power supply；The relative level of guide part 53
Face enters after chute 4 in the setting that is inclined upwardly, the lead-out terminal of power supply, passes through the inclined-plane jack-up of the front end of guide part 53 guide part
53 and enter contact site 52；The fixed part 51, contact site 52 and guide part 53 are made it have by the bending forming of spring copper sheet 5
Certain elasticity.
Utility model works principle：During normal operating conditions, the battery case of power supply is arranged in the chute 4 of fixed mount,
Battery case is fixed by supporting plate 3；Then it is in electrical contact by the lead-out terminal progress of spring copper sheet 5 and power supply, from
And the electricity of power supply can be obtained；Realized and electrically connected by Elastic Contact due to spring copper sheet 5, it is possible to divided at any time
From to realize the replacing of battery.
Claims (5)
1. a kind of aircraft power fixed mount, it is characterised in that：Including two blocks of symmetrically arranged side plates and located at two pieces of side linings
Some crossbeams between plate, the bottom of the side plate is provided with the supporting plate extended internally, the supporting plate, side plate and crossbeam
Between form chute；Wherein one crossbeam is provided with two panels spring copper sheet, and the spring copper sheet includes fixed part, contact site
And guide part, the contact site is provided with screw, and contact site is bolted on crossbeam, the contact site relative level
In tilting down setting, the guide part relative level in the setting that is inclined upwardly, the fixed part, contact site and guide part by
Spring copper sheet bending forming.
2. a kind of aircraft power fixed mount according to claim 1, it is characterised in that：The bottom of the side plate is provided with
Some projections, the side correspondence high spot of the supporting plate is provided with groove, and the described raised and groove coordinates.
3. a kind of aircraft power fixed mount according to claim 2, it is characterised in that：The supporting plate is solid by bolt
It is scheduled on the bottom of side plate.
4. a kind of aircraft power fixed mount according to claim 1, it is characterised in that：The top of the crossbeam is provided with peace
Fill hole.
5. a kind of aircraft power fixed mount according to claim 1, it is characterised in that：The two ends of the crossbeam pass through spiral shell
Bolt is connected with side plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621350161.4U CN206417204U (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft power fixed mount |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621350161.4U CN206417204U (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft power fixed mount |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206417204U true CN206417204U (en) | 2017-08-18 |
Family
ID=59575149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621350161.4U Expired - Fee Related CN206417204U (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft power fixed mount |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206417204U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109941445A (en) * | 2017-12-21 | 2019-06-28 | 海鹰航空通用装备有限责任公司 | A kind of unmanned plane battery cabin structure |
-
2016
- 2016-12-09 CN CN201621350161.4U patent/CN206417204U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109941445A (en) * | 2017-12-21 | 2019-06-28 | 海鹰航空通用装备有限责任公司 | A kind of unmanned plane battery cabin structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171211 Address after: 519090 Guangdong province Zhuhai city Zhuhai town of Red Bay area, Shuanghu road Xihua Road on the north side of Xinrong Industrial Zone No. 6 building three Room 305 Patentee after: Zhuhai Luban automation equipment Co., Ltd. Address before: 510800 Guangzhou, Huadu District, Guangdong Province Road, No. 1 Patentee before: Guangzhou College of South China University of Technology |
|
| 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: 20170818 Termination date: 20191209 |