CN207664124U - A kind of battery bracket for adjusting unmanned plane machine gravity - Google Patents
A kind of battery bracket for adjusting unmanned plane machine gravity Download PDFInfo
- Publication number
- CN207664124U CN207664124U CN201721812265.7U CN201721812265U CN207664124U CN 207664124 U CN207664124 U CN 207664124U CN 201721812265 U CN201721812265 U CN 201721812265U CN 207664124 U CN207664124 U CN 207664124U
- Authority
- CN
- China
- Prior art keywords
- battery
- shaft
- unmanned plane
- battery bracket
- guide rail
- 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.)
- Active
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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Battery Mounting, Suspending (AREA)
Abstract
A kind of battery bracket for adjusting unmanned plane machine gravity, including two guide rails, battery mounting plate, pulley, knurled nut, bandage, it is characterized in that：Two guide rails are erected in the framework of fuselage interior in advance；The battery mounting plate includes a supporting plate, 4 ribs and two reinforcing beams, and the supporting plate rear and front end is respectively there are two rectangular opening, and battery is bundled on supporting plate by the bandage by the rectangular opening, and two reinforcing beams are arranged in parallel among guide rail；Pulley described in every group is made of a wheel and a shaft, and 4 through-holes are uniformly distributed on the rib, and for fixing the shaft, the wheel can rotate in shaft；Shaft in the most front-seat pulley of every guide rail is equipped with screw thread, can coordinate with knurled nut, forms retaining mechanism.
Description
Technical field
The utility model is applied to unmanned plane field, is a kind of battery bracket for adjusting unmanned plane machine gravity.It should
Holder can fix avionics battery, and realize that battery carries out position movement, to play the role of adjusting machine gravity.
Background technology
Nowadays the application field of unmanned plane is very extensive.The design gravity of unmanned plane often has centainly with actual center gravity
At this moment deviation just needs the center of gravity of trim unmanned plane.According to different application environments, often type is not or not the load of UAV flight
Together, its weight of different loads differs, and when replacing load, due to the weight difference of load, necessarily so that drone center of unmanned aerial vehicle will produce
Offset.To make unmanned plane keep balance, the center of gravity of trim unmanned plane is usually carried out using some mass, these mass increase
The take-off weight for having added aircraft, to reduce the cruising ability of aircraft.
Utility model content
In order to solve the deficiencies in the prior art, a kind of electricity for adjusting unmanned plane machine gravity of the present utility model
Pond holder, to solve deficiency in the prior art.Its technical solution is as follows：
A kind of battery bracket for adjusting unmanned plane machine gravity, including two guide rails (1), battery mounting plate (2), cunning
(3), knurled nut (4), bandage (5) are taken turns, it is characterized in that：Two guide rails (1) are erected in the framework of fuselage interior in advance；Institute
It includes a supporting plate (8), 4 ribs (9) and two reinforcing beams (10), supporting plate (8) rear and front end to state battery mounting plate (2)
Battery is bundled on supporting plate (8) by rectangular opening there are two each, the bandage (5) by the rectangular opening, and two reinforcing beams are parallel
It is arranged among guide rail；Pulley (3) described in every group is made of a wheel (6) and a shaft (7), on the rib (9)
4 through-holes of even distribution, for fixing the shaft (7), the wheel (6) can rotate in shaft (7)；Every guide rail is most front-seat
Shaft (7) in the pulley is equipped with screw thread, can coordinate with knurled nut (4), forms retaining mechanism.
Preferably：Battery mounting plate (2) material is the aviation laminate of carbon cloth package.
Preferably：Four groups of pulleys are set on every guide rail.
Preferably：The shaft (7) is stainless steel, wherein latter three groups in four groups of pulleys of every guide rail setting
Shaft (7) in pulley does not have screw thread, the shaft and the rib (9) on battery mounting plate (2) fixed.
Preferably：The knurled nut (4) is the stainless steel nut of outer diameter φ 20mm, internal thread M2.5.
Preferably：The guide rail (1) is " returning " font structure that aviation laminate is spliced, and surface spreads carbon cloth and increases by force
Degree；There is the opening of 180mm long in the front of guide rail (1), makes when disposing battery bracket as the initial makeup location of battery bracket
The wheel (6) is stuck in the guide groove of guide rail (1).
Advantageous effect：The timbering material and stable structure, dead weight is lighter, without tool, behaviour when assembling and adjusting
Make very convenient.
Description of the drawings
Fig. 1 is the utility model general structure schematic diagram.
Fig. 2 is the structural schematic diagram of the utility model battery mounting plate (2).
Fig. 3 is the utility model pulley (3) installation distribution schematic diagram.
Fig. 4 is the most front-seat pulley of the utility model (3) and knurled nut (4) scheme of installation.
Fig. 5 is structural schematic diagram when the utility model battery bracket installs.
Wherein：Guide rail (1), battery mounting plate (2), pulley (3), nut (4), bandage (5), wheel (6), shaft (7), support
Plate (8), rib (9), reinforcing beam (10).
Specific implementation mode
Shown in attached drawing 1-5.
A kind of battery bracket for adjusting unmanned plane machine gravity, by position of the regulating cell in fuselage, to adjust
Planisher center of gravity.The holder by two guide rails (1), battery mounting plate (2), eight groups of pulleys (3), two knurled nuts (4), two
Bandage (5) forms.Battery mounting plate (2) is made of a supporting plate (8), 4 ribs (9) and two reinforcing beams (10), and material is equal
It is bonded with glue for the aviation laminate of carbon cloth package, between each component secured.Rectangular opening there are two supporting plate (8) rear and front end is each,
For tying band (5), battery can be firmly bundled on supporting plate (8) by bandage (5).It is uniformly distributed 4 through-holes on rib (9), uses
Carry out fixed rotating shaft (7).Every group of pulley (3) is made of a wheel (6) and a shaft (7), and wheel (6) can be in shaft (7)
Smooth rotation is each side uniformly distributed four groups of pulleys (3), such as Fig. 3.Shaft (7) is stainless steel, wherein rear three rows
6 shafts (7) be adhesively fixed with glue without the rib (8) on screw thread, with battery mounting plate (2), so that 6 of rear three row is turned
Axis can not be rotated and be moved axially.There are M2.5 screw threads on two most front-seat shafts (7), can coordinate with knurled nut (4), forms
Retaining mechanism.When unclamping knurled nut (4), position adjusting can be carried out, after adjusting suitable position, knurled nut (4) is tightened, tightens
When shaft (7) most front-seat wheel (6) will be clamped together with guide rail (1), generate frictional force, twisted to axial medial movement
It is next can fixing bracket position.There is " rectangular block " structure on two most front-seat shafts (7), can prevent from screwing knurled nut
(4) shaft (7) also and then rotates when.Knurled nut (4) is the stainless steel nut of outer diameter φ 20mm, internal thread M2.5, is convenient for hand
It twists.Guide rail (1) is " returning " font structure that aviation laminate is spliced, and surface spreads carbon cloth and increases intensity.Two pre- framves of guide rail (1)
It is located in the framework of fuselage interior, keeps guide rail (1) horizontal fixed.There is the opening of 180mm long in the front of guide rail (1), makees
For the initial makeup location of battery bracket, when disposing battery bracket, make in 8 wheel (6) card such as guide grooves of guide rail (1), then
It rearward slides, you can realize the position movement of battery.
Embodiment 1
Before use, guide rail (1) is fixed with fuselage frame structure, and keep horizontal.It is load A that example is carried for the first time.It will be electric
Pond mounting plate (2), pulley (3), knurled nut (4), bandage (5) are all assemblied together.Knurled nut (4) turns with most front-seat
It the threaded connection of axis (7) but does not tighten.By assembled battery bracket on guide rail (1), make each wheel of battery bracket
Sub (6) all enter in the guide groove of guide rail (1).Battery is placed on battery mounting plate (2) again, tightens bandage (5).By battery to
Guide rail rear is moved, and is pushed into the position of probably energy leveling machine gravity, is tightened knurled nut (4), entire unmanned plane is sling, such as
Fruit drone center of unmanned aerial vehicle deviates, then according to deviation of gravity center situation regulating cell position.The method of adjusting position is to unclamp knurled nut
(4), it is tightened again behind mobile battery position.Repeatedly, until finding the electricity in equilibrium state when unmanned plane complete machine is lifted
Pond position, and record the position.The method of record position can draw groove on guide rail (1), which is to carry load A
When, battery answers the position at place.If carrying load is changed to load B, load A and B there are certain weight difference, at this time unmanned plane
Necessarily lead to deviation of gravity center.Solution is：Knurled nut (4) regulating cell position is unclamped, when finding carrying load B, nobody
Machine complete machine is lifted, and under equilibrium state, the position where battery, locking knurled nut (4) fixes battery, while recording should
Position.The position is when carrying load B, and battery answers the position at place.By way of regulating cell position, trim unmanned plane
Center of gravity, can avoid or be greatly decreased using mass.The take-off weight of unmanned plane directly affects unmanned plane efficiency of navigation
Key factor, the battery bracket of adjustable drone center of unmanned aerial vehicle of the present utility model, can mitigate unmanned plane to greatest extent
Take-off weight.And the timbering material and stable structure, dead weight is lighter, assembly and when adjusting without tool, operation ten
It is convenient to divide.
Many details are elaborated in the above description in order to fully understand the utility model.But above description
Only it is the preferred embodiment of the utility model, the utility model can be much to come different from other manner described here
Implement, therefore the utility model is not limited by specific implementation disclosed above.Any those skilled in the art exist simultaneously
It does not depart under technical solutions of the utility model ambit, it is all new to this practicality using the methods and technical content of the disclosure above
Type technical solution makes many possible changes and modifications, or is revised as the equivalent embodiment of equivalent variations.It is every without departing from this
The content of utility model technical solution any is simply repaiied according to the technical essence of the utility model is made to the above embodiment
Change, equivalent variations and modification, in the range of still falling within technical solutions of the utility model protection.
Claims (6)
1. a kind of battery bracket for adjusting unmanned plane machine gravity, including two guide rails (1), battery mounting plate (2), pulley
(3), knurled nut (4), bandage (5), it is characterized in that：Two guide rails (1) are erected in the framework of fuselage interior in advance；It is described
Battery mounting plate (2) includes a supporting plate (8), 4 ribs (9) and two reinforcing beams (10), and supporting plate (8) rear and front end is each
There are two rectangular opening, battery is bundled on supporting plate (8) by the bandage (5) by the rectangular opening, and two reinforcing beams are parallel to be set
It sets among two guide rails；Pulley (3) described in every group is made of a wheel (6) and a shaft (7), on the rib (9)
4 through-holes are uniformly distributed, for fixing the shaft (7), the wheel (6) can rotate in shaft (7)；Every guide rail most before
The shaft (7) arranged in the pulley is equipped with screw thread, can coordinate with knurled nut (4), forms retaining mechanism.
2. a kind of battery bracket for adjusting unmanned plane machine gravity according to claim 1, it is characterized in that：The electricity
Pond mounting plate (2) material is the aviation laminate of carbon cloth package.
3. a kind of battery bracket for adjusting unmanned plane machine gravity according to claim 1, it is characterized in that：Every is led
Four groups of pulleys are set on rail (1).
4. a kind of battery bracket for adjusting unmanned plane machine gravity according to claim 1, it is characterized in that：Described turn
Axis (7) is stainless steel, wherein the shaft (7) in rear three groups of pulleys in four groups of pulleys of every guide rail setting does not have spiral shell
Line, the shaft and the rib (9) on battery mounting plate (2) are fixed.
5. a kind of battery bracket for adjusting unmanned plane machine gravity according to claim 1, it is characterized in that：The rolling
Clamp nut (4) is the stainless steel nut of outer diameter φ 20mm, internal thread M2.5.
6. a kind of battery bracket for adjusting unmanned plane machine gravity according to claim 1, it is characterized in that：It is described to lead
Rail (1) is " returning " font structure that aviation laminate is spliced, and surface spreads carbon cloth and increases intensity；The front of the guide rail (1) has
The opening of 180mm long when disposing battery bracket, makes the wheel (6) be stuck in described as the initial makeup location of battery bracket
In the guide groove of guide rail (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721812265.7U CN207664124U (en) | 2017-12-22 | 2017-12-22 | A kind of battery bracket for adjusting unmanned plane machine gravity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721812265.7U CN207664124U (en) | 2017-12-22 | 2017-12-22 | A kind of battery bracket for adjusting unmanned plane machine gravity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207664124U true CN207664124U (en) | 2018-07-27 |
Family
ID=62942079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721812265.7U Active CN207664124U (en) | 2017-12-22 | 2017-12-22 | A kind of battery bracket for adjusting unmanned plane machine gravity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207664124U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547203A (en) * | 2020-05-28 | 2020-08-18 | 中国船舶工业集团公司第七0八研究所 | Modular-design inland river small-sized lithium battery power ship and construction method |
| US20210323619A1 (en) * | 2020-04-16 | 2021-10-21 | Korea Advanced Institute Of Science And Technology | Wall-climbing drone using auxiliary arm and method for controlling therefor |
-
2017
- 2017-12-22 CN CN201721812265.7U patent/CN207664124U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210323619A1 (en) * | 2020-04-16 | 2021-10-21 | Korea Advanced Institute Of Science And Technology | Wall-climbing drone using auxiliary arm and method for controlling therefor |
| CN111547203A (en) * | 2020-05-28 | 2020-08-18 | 中国船舶工业集团公司第七0八研究所 | Modular-design inland river small-sized lithium battery power ship and construction method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104002994B (en) | A kind of slide block executing agency for Solar sail spacecraft gesture stability | |
| CN207664124U (en) | A kind of battery bracket for adjusting unmanned plane machine gravity | |
| US9205922B1 (en) | Systems and methods for implementing a payload distribution system | |
| CN206590103U (en) | A kind of collapsible arm fuselage based on integral type multi-rotor unmanned aerial vehicle central frame | |
| CN104608923A (en) | Honeycomb-type six-rotor transport aircraft | |
| CN205176666U (en) | Solar energy multiaxis aircraft | |
| CN106394933B (en) | A kind of distributed satellites traction Solar sail spacecraft configuration | |
| CN104058105A (en) | Deep space solar sail spacecraft driven by utilizing sunlight pressure | |
| CN204452950U (en) | Convertible The Cloud Terrace accommodation device | |
| CN104908936A (en) | Unmanned helicopter | |
| CN107600463B (en) | A kind of agility small satellite attitude fast reserve control method | |
| CN112607008A (en) | Anti-collision device based on large-scale many rotor unmanned aerial vehicle | |
| CN201175582Y (en) | Model aircraft | |
| CN103803070B (en) | Engineering-type rotary wind type unmanned vehicle | |
| CN206050068U (en) | Aircraft | |
| CN206050066U (en) | A kind of portable multi-rotor aerocraft of Spliced type | |
| CN205327391U (en) | Many rotor unmanned aerial vehicle frame | |
| CN205068870U (en) | Precession effect presentation device is controld in flight | |
| CN204233763U (en) | Ultralight energy-conservation flight instruments | |
| CN205602124U (en) | Fin and helicopter of helicopter | |
| CN210101983U (en) | Six rotor unmanned aerial vehicle | |
| CN114353604A (en) | Experimental platform for simulating vector thrust redundancy configuration of recoverable rocket | |
| CN207758986U (en) | A kind of light-duty sport plane fuselage having manhole | |
| CN203996884U (en) | Four-axle aircraft motor system | |
| CN106800097A (en) | A kind of space flight self start type propeller |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |