CN209700983U - A kind of solar wing convenient for extension - Google Patents
A kind of solar wing convenient for extension Download PDFInfo
- Publication number
- CN209700983U CN209700983U CN201920422357.7U CN201920422357U CN209700983U CN 209700983 U CN209700983 U CN 209700983U CN 201920422357 U CN201920422357 U CN 201920422357U CN 209700983 U CN209700983 U CN 209700983U
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- CN
- China
- Prior art keywords
- control
- fixedly installed
- push rod
- wing
- movable wing
- 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.)
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Abstract
The utility model discloses a kind of solar wings convenient for extension, including bottom plate, the upper end outer surface of the bottom plate is fixedly installed with fixed-wing, the lower end outer surface of the control-rod is fixedly installed with control cabinet, the lower end outer surface of the bottom plate is fixedly installed with reinforcing supporting block, the inside of the control cabinet is fixedly installed with limit push rod, the inside of the control cabinet is fixedly installed with control push rod, the inside of the control cabinet is fixedly installed with groove plate, and the lower end outer surface of the control-rod is fixedly installed with gear.The utility model utilizes control-rod, control cabinet, limit push rod, control push rod, groove plate and gear, control push rod pushes groove plate to travel forward, the rotation of groove strip moving gear, the solar wing model- following control bar being mounted on control-rod rotates together, movable wing expansion, when controlling push rod contraction, movable wing folds therewith, space valuable on satellite is saved, satellite is allowed to stay there are three faces to arrange load.
Description
Technical field
The utility model relates to solar wing field, in particular to a kind of solar wing convenient for extension.
Background technique
Solar wing is the energy source of satellite.That is solar energy sailboard is a kind of collection solar device, is usually applied to
The energy supply of satellite, spaceship, existing solar wing almost all are arranged on the satellite plane of symmetry, occupy the two of satellite in this way
A face causes the number of sensors for being mounted on satellite surface to be restricted.
Therefore, it is necessary to solve the above problems to invent a kind of solar wing convenient for extension.
Utility model content
The purpose of this utility model is to provide a kind of solar wings convenient for extension, are pushed away using control-rod, control cabinet, limit
Bar, control push rod, groove plate and gear, control push rod push groove plate to travel forward, and the rotation of groove strip moving gear is mounted on
Solar wing model- following control bar on control-rod rotates together, and movable wing expansion, when controlling push rod contraction, movable wing is rolled over therewith
It is folded, to achieve the purpose that for solar wing to be arranged in one face of satellite, to solve the problems mentioned in the above background technology.
To achieve the above object, the utility model provides the following technical solutions: a kind of solar wing convenient for extension, including bottom
Plate, the upper end outer surface of the bottom plate are fixedly installed with fixed-wing, and the upper end outer surface of the bottom plate is solid close to the position of one end
Dingan County is equipped with the first movable wing, and the upper end outer surface of the bottom plate is fixedly installed with the second movable wing close to the position of the other end,
One end outer surface of first movable wing and the second movable wing is fixedly installed with control-rod, the lower end outer surface of the control-rod
It is fixedly installed with control cabinet, the lower end outer surface of the bottom plate is fixedly installed with reinforcing supporting block, and the inside of the control cabinet is solid
Equipped with limit push rod, the inside of the control cabinet is fixedly installed with control push rod for Dingan County, and the inside of the control cabinet is fixedly mounted
Card with teeth, the lower end outer surface of the control-rod are fixedly installed with gear, and the outer surface of the groove plate offers location hole,
The outer surface of the groove plate is provided with groove.
Preferably, the lower end outer surface of first movable wing and the second movable wing is fixedly installed with reinforcing supporting block, institute
Stating and reinforcing the material of supporting block is alfer.
Preferably, the front end of the limit push rod is provided with push rod, and the push rod and location hole are fitting to connection.
Preferably, the specification size of first movable wing and the second movable wing is completely the same.
Preferably, first movable wing is fixedly connected by control-rod with bottom plate with the second movable wing.
Preferably, the gear is fitting to connection by groove and groove plate.
The technical effect and advantage of the utility model:
(1) the utility model utilizes control-rod, control cabinet, limit push rod, control push rod, groove plate and tooth by setting
Wheel controls push rod when in use and groove plate is pushed to travel forward, the rotation of groove strip moving gear, the sun being mounted on control-rod
Wing model- following control bar rotates together, and movable wing expansion, when controlling push rod contraction, movable wing folds therewith, saves on satellite
Valuable space allows satellite to stay there are three faces to arrange load.
Detailed description of the invention
Fig. 1 is the whole expanded schematic diagram of the utility model；
Fig. 2 is the foldable integral schematic diagram of the utility model；
Fig. 3 is the schematic diagram of the utility model control cabinet；
Fig. 4 is the schematic diagram of the utility model movable wing；
Fig. 5 is the schematic diagram of the utility model groove plate；
Fig. 6 is the schematic diagram that the utility model reinforces supporting block.
In figure: 1 bottom plate, 2 fixed-wings, 3 first movable wings, 4 second movable wings, 5 control-rods, 6 control cabinets, 7 reinforce support
Block, 8 limit push rods, 9 control push rods, 10 groove plates, 11 gears, 12 location holes, 13 grooves.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The utility model provides as shown in figures 1 to 6 to achieve the above object, and the utility model provides following technical side
Case: a kind of solar wing convenient for extension, including bottom plate 1, the upper end outer surface of the bottom plate 1 is fixedly installed with fixed-wing 2, described
The upper end outer surface of bottom plate 1 is fixedly installed with the first movable wing 3 close to the position of one end, and the upper end outer surface of the bottom plate 1 is leaned on
The position of the nearly other end is fixedly installed with the second movable wing 4, one end outer surface of first movable wing 3 and the second movable wing 4
It is fixedly installed with control-rod 5, the lower end outer surface of the control-rod 5 is fixedly installed with control cabinet 6, outside the lower end of the bottom plate 1
Surface, which is fixedly installed with, reinforces supporting block 7, and the inside of the control cabinet 6 is fixedly installed with limit push rod 8, the control cabinet 6
Inside is fixedly installed with control push rod 9, and the inside of the control cabinet 6 is fixedly installed with groove plate 10, the lower end of the control-rod 5
Outer surface is fixedly installed with gear 11, and the outer surface of the groove plate 10 offers location hole 12, the appearance of the groove plate 10
Face is provided with groove 13.
Further, in the above scheme, the fixed peace in the lower end outer surface of first movable wing 3 and the second movable wing 4
Equipped with supporting block 7 is reinforced, the material for reinforcing supporting block 7 is alfer, and reinforcing supporting block 7 supports the first movable wing 3
With the second movable wing 4, the first movable wing 3 and the second movable wing 4 is made to keep vertical with control-rod 5；
Further, in the above scheme, the front end of the limit push rod 8 is provided with push rod, the push rod and location hole
12 are fitting to connection, and after the first movable wing 3 and the expansion of the second movable wing 4, limit push rod 8 starts, and will limit pushing away for 8 front end of push rod
Bar is pushed into location hole 12, limits the movement of groove plate 10；
Further, in the above scheme, the specification size of first movable wing 3 and the second movable wing 4 is completely the same,
Solar energy can be absorbed to greatest extent after first movable wing 3 and the expansion of the second movable wing 4；
Further, in the above scheme, first movable wing 3 and the second movable wing 4 pass through control-rod 5 and bottom plate 1
It is fixedly connected, the first movable wing 3 on control-rod 5 rotates together with 4 model- following control bar 5 of the second movable wing, and movable wing is opened up immediately
It opens；
Further, in the above scheme, the gear 11 is fitting to connection by groove 13 and groove plate 10, when using
Control push rod 9 pushes groove plate 10 to travel forward, and groove plate 10 is rotated with moving gear 11, the solar wing being mounted on control-rod 5
Model- following control bar 5 rotates together, and movable wing expansion, when controlling the contraction of push rod 9, movable wing folds therewith, saves on satellite
Valuable space allows satellite to stay there are three faces to arrange load.
This practical working principle:
Referring to Figure of description 1-5, when people need solar wing spreading, needs to open control push rod 9, control push rod
9 can push groove plate 10 to travel forward, the groove 13 on groove plate 10 and the gear 11 on both sides are embedding simultaneously by push rod to being pushed forward
It closes, the gear 11 that will drive both sides when groove plate 10 is mobile rotates together with, and the rotation of gear 11, which has driven, to be mounted on
Control-rod 5 on gear 11, the first movable wing 3 on control-rod 5 rotate together with 4 model- following control bar 5 of the second movable wing, activity
The wing is unfolded immediately, then limits push rod 8 and starts, and limits the motor in push rod 8 after The gear deceleration, drives a pair of of screw rod spiral shell
Mother, the rotation motion of motor is in line movement will limit push rod 8 using the push-in movement of motor rotating forward completion push rod
The push rod of front end is pushed into location hole 12, limits the movement of groove plate 10, when controlling the contraction of push rod 9, controls the electricity in push rod 9
Motivation drives a pair of of feed screw nut after The gear deceleration, and the rotation motion of motor is in line movement, is inverted using motor
The contractive action of push rod is completed, the first movable wing 3 folds therewith with the second movable wing 4, and reinforcing supporting block 7 supports the first activity
The wing 3 and the second movable wing 4 make the first movable wing 3 and the second movable wing 4 keep vertical with control-rod 5, save valuable on satellite
Space, satellite is stayed and arranges load there are three face.
Finally, it should be noted that the above descriptions are merely preferred embodiments of the present invention, it is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic
It is equivalently replaced, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (6)
1. a kind of solar wing convenient for extension, including bottom plate (1), it is characterised in that: the upper end outer surface of the bottom plate (1) is fixed
It being equipped with fixed-wing (2), the upper end outer surface of the bottom plate (1) is fixedly installed with the first movable wing (3) close to the position of one end,
The upper end outer surface of the bottom plate (1) is fixedly installed with the second movable wing (4) close to the position of the other end, first movable wing
(3) it is fixedly installed with control-rod (5) with one end outer surface of the second movable wing (4), the lower end outer surface of the control-rod (5) is solid
Dingan County is equipped with control cabinet (6), and the lower end outer surface of the bottom plate (1), which is fixedly installed with, reinforces supporting block (7), the control cabinet
(6) inside is fixedly installed with limit push rod (8), and the inside of the control cabinet (6) is fixedly installed with control push rod (9), described
The inside of control cabinet (6) is fixedly installed with groove plate (10), and the lower end outer surface of the control-rod (5) is fixedly installed with gear
(11), the outer surface of the groove plate (10) offers location hole (12), and the outer surface of the groove plate (10) is provided with groove
(13).
2. a kind of solar wing convenient for extension according to claim 1, it is characterised in that: first movable wing (3) with
The lower end outer surface of second movable wing (4), which is fixedly installed with, reinforces supporting block (7), and the material for reinforcing supporting block (7) is aluminium
Ferroalloy.
3. a kind of solar wing convenient for extension according to claim 1, it is characterised in that: before the limit push rod (8)
End is provided with push rod, and the push rod and location hole (12) are fitting to connection.
4. a kind of solar wing convenient for extension according to claim 1, it is characterised in that: first movable wing (3) with
The specification size of second movable wing (4) is completely the same.
5. a kind of solar wing convenient for extension according to claim 1, it is characterised in that: first movable wing (3) with
Second movable wing (4) is fixedly connected by control-rod (5) with bottom plate (1).
6. a kind of solar wing convenient for extension according to claim 1, it is characterised in that: the gear (11) passes through groove
(13) it is fitting to connection with groove plate (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920422357.7U CN209700983U (en) | 2019-03-31 | 2019-03-31 | A kind of solar wing convenient for extension |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920422357.7U CN209700983U (en) | 2019-03-31 | 2019-03-31 | A kind of solar wing convenient for extension |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209700983U true CN209700983U (en) | 2019-11-29 |
Family
ID=68648230
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920422357.7U Expired - Fee Related CN209700983U (en) | 2019-03-31 | 2019-03-31 | A kind of solar wing convenient for extension |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209700983U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112298618A (en) * | 2020-09-30 | 2021-02-02 | 北京空间飞行器总体设计部 | Two-dimensional secondary expansion solar wing |
-
2019
- 2019-03-31 CN CN201920422357.7U patent/CN209700983U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112298618A (en) * | 2020-09-30 | 2021-02-02 | 北京空间飞行器总体设计部 | Two-dimensional secondary expansion solar wing |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191129 Termination date: 20200331 |