CN108382611A - A kind of aerospace outdoor illumination - Google Patents
A kind of aerospace outdoor illumination Download PDFInfo
- Publication number
- CN108382611A CN108382611A CN201810082176.4A CN201810082176A CN108382611A CN 108382611 A CN108382611 A CN 108382611A CN 201810082176 A CN201810082176 A CN 201810082176A CN 108382611 A CN108382611 A CN 108382611A
- Authority
- CN
- China
- Prior art keywords
- headlamp
- motor
- cleaning sponge
- aerospace
- fixed
- 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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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
Abstract
The invention discloses a kind of aerospace outdoor illuminations, including spacecraft shell and headlamp, fixed otic placode is arranged on the outside of spacecraft shell, pass through the upper end of activity axis connection headlamp between two fixed otic placodes, one end of the movable axis is fixed with first motor, first motor is fixedly mounted on the fixation otic placode of side, it is fixed with bottom plate on the spacecraft shell of fixed otic placode lower end, protection groove is recessed in the top surface of bottom plate, it protects on the center of groove and is recessed with cleaning sponge mounting groove, cleaning sponge block is equipped in cleaning sponge mounting groove, cleaning sponge block bottom end is fixedly connected with the driving end of the second motor, bottom plate is run through at the driving end of second motor, and second motor be mounted on bottom plate on.The present invention drives headlamp to rotate by first motor, controls the rotation that headlamp carries out 180 degree in vertical plane respectively, to adjust illumination zone, and can be according to the position of service condition adjusting illuminating lamp.
Description
Technical field
The present invention relates to aerospace equipment technical field, specially a kind of aerospace outdoor illumination.
Background technology
The development of aerospace cause is the science and technology leap progress of 20th century, the result that social production is advanced by leaps and bounds.Boat
The achievement of empty space flight has concentrated numerous New TownMovements of science and technology.Aerospace operations so far, although being also the mankind
Initial several steps of this cradle of the earth are left, but its effect is far beyond science and technology field, to politics, economic, military
So that human society life all produces extensively and far-reaching influence.
September 27 in 2008, China astronaut has stepped the first step in space, with the development of China's Space Science and Technology, meeting
There are more and more astronaut to set foot on space, and in space, when spacecraft runs to certain position, certain time can be lost
Illumination, the headlamp for just needing spacecraft self-contained at this time is illuminated, while existing space trash is more, and headlamp is long
Time is fixed on the outside of spacecraft and is easy to be damaged, at present thus it is proposed that a kind of aerospace is used with outdoor illumination
In solving the above problems.
Invention content
The purpose of the present invention is to provide a kind of aerospace outdoor illuminations, to solve to carry in above-mentioned background technology
The problem of going out.
To achieve the above object, the present invention provides the following technical solutions：A kind of aerospace outdoor illumination, including
Spacecraft shell and headlamp, are arranged with fixed otic placode on the outside of the spacecraft shell, between two fixed otic placodes
By the upper end of activity axis connection headlamp, one end of the movable axis is fixed with first motor, and the first motor fixes peace
On the fixation otic placode of side, bottom plate, the top of the bottom plate are fixed on the spacecraft shell of the fixed otic placode lower end
Be recessed with protection groove in face, on the center of the protection groove in be recessed with cleaning sponge mounting groove, the cleaning is extra large
It is equipped with cleaning sponge block in continuous mounting groove, cleaning sponge block bottom end is fixedly connected with the driving end of the second motor, and described second
Bottom plate is run through at the driving end of motor, and the second motor is mounted on bottom plate.
Preferably, the upper end of the headlamp is protection shell, and bottom end is equipped with lighting bulb, and the top of the headlamp is logical
It crosses connecting shaft and is installed with protective plate, the protective plate is rectangle plane plate or Curved plate structure.
Preferably, limit shaft is fixed on the end face of the protective plate side, the limit shaft sliding is connected to side
In the limiting slot of the inner side end of fixed otic placode, the limiting slot is semi-circular shape structure.
Preferably, when the limit shaft is located at limiting slot lower end, the light bulb of the headlamp faces on spacecraft shell
Side, when limit shaft is located at limiting slot upper end, the light bulb of the headlamp faces below spacecraft shell, when limit shaft is located at
When limiting slot centre position, the bulb irradiation direction of the headlamp is vertical with spacecraft shell side.
Preferably, the width of the protection groove is more than the width of headlamp lower end, is open type on the outside of the protection groove
Structure, the headlamp slides on the outside of protection groove, and the top surface of bottom plate is located at the upper end of headlamp bottom surface.
Preferably, cleaning sponge block bottom end is equipped with metal mounting plate, which is fixedly mounted on the second electricity
On the driving end of machine, the section of the cleaning sponge block and metal mounting plate is the circular configuration of same size, when illumination lamp position
When protecting in groove, the cleaning sponge block is just in close contact the clear lamp blister of headlamp.
Compared with prior art, the beneficial effects of the invention are as follows：
1, the present invention drives headlamp to be rotated by first motor, controls headlamp respectively and is carried out in vertical plane
The rotation of 180 degree, to adjust illumination zone, and can be according to the position of service condition adjusting illuminating lamp；
2, it can make being positioned against for protective plate by the position of control headlamp, pass through when headlamp need not use
Protective plate can avoid impact of the space trash to headlamp shell, and the activity of headlamp lower end is connected in protection groove, passes through
Bottom plate protects light bulb part more weak on headlamp；
3, when headlamp is located in protection groove, cleaning sponge block is just in close contact the clear lamp blister of headlamp,
The rotation of cleaning sponge block can also be driven by the second motor, and cleaning is carried out to the clear lamp blister of headlamp.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is Cutting platform structural schematic diagram of the present invention；
Fig. 3 is Cutting platform structural schematic diagram of the present invention；
Fig. 4 is that the cleaning sponge block of the present invention is mounted on the structural schematic diagram in bottom plate.
In figure：Otic placode, 201 limiting slots, 3 movable axis, 4 protective plates, 401 limit shafts, 5 first are fixed in 1 spacecraft shell, 2
Motor, 6 bottom plates, 601 protection grooves, 602 cleaning sponge mounting grooves, 7 cleaning sponge blocks, 8 second motors.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 4 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of aerospace outdoor illumination, including boat
The outside of its device shell 1 and headlamp 3, spacecraft shell 1 is arranged with fixed otic placode 2, passes through work between two fixed otic placodes 2
Moving axis connects the upper end of headlamp 3, and the upper end of headlamp 3 is protection shell, and bottom end is equipped with lighting bulb, the headlamp 3
Top is installed with protective plate 4 by connecting shaft, and protective plate 4 is rectangle plane plate or Curved plate structure, is illuminated in the present invention
Lamp 3 can be made being positioned against for protective plate 4, can be kept away by protective plate 4 when need not use by the position of control headlamp 3
Impact of the space trash to 3 shell of headlamp is opened, because headlamp 3 is commonly installed accumulator in position at this.
As shown in Figure 1-Figure 3, limit shaft 401, the sliding clamping of limit shaft 401 are fixed on the end face of 4 side of protective plate
It is fixed in side in the limiting slot 201 of the inner side end of otic placode 2, limiting slot 201 is semi-circular shape structure, wherein on protective plate 4
Limit shaft 401 and fixed otic placode 2 on 201 device of limiting slot can ensure stability of the headlamp 3 in rotation process.
When limit shaft 401 is located at 201 lower end of limiting slot, the light bulb of headlamp 3 faces 1 top of spacecraft shell, works as limit
When position axis 401 is located at 201 upper end of limiting slot, the light bulb of headlamp 3 faces 1 lower section of spacecraft shell, when limit shaft 401 is located at
When 201 centre position of limiting slot, the bulb irradiation direction of headlamp 3 is vertical with 1 side of spacecraft shell.
One end of movable axis 3 is fixed with first motor 5, and first motor 5 is fixedly mounted on the fixation otic placode 2 of side,
It is fixed with bottom plate 6 on the spacecraft shell 1 of 2 lower end of fixed otic placode, protection groove 601, protection are recessed in the top surface of bottom plate 6
It is recessed with cleaning sponge mounting groove 602 on the center of groove 601, cleaning sponge is equipped in cleaning sponge mounting groove 602
Block 7,7 bottom end of cleaning sponge block are fixedly connected with the driving end of the second motor 8, and bottom plate 6 is run through at the driving end of the second motor 8, and the
Two motors 8 are mounted on bottom plate 6.
As shown in Figure 1 and Figure 4, protect the width of groove 601 more than the width of 3 lower end of headlamp, outside the protection groove 601
Side is open type structure, and headlamp 3 slides into from 601 outside of protection groove, and the top surface of bottom plate 6 is located at the upper of 3 bottom surface of headlamp
End, when headlamp 3 need not use its lower end activity be connected to protection groove 601 in, by bottom plate 6 on headlamp 3 more
It is protected weak light bulb part.
As shown in Figure 1 and Figure 4,7 bottom end of cleaning sponge block is equipped with metal mounting plate, which is fixedly mounted on the
On the driving end of two motors 8, the section of cleaning sponge block 7 and metal mounting plate is the circular configuration of same size, when headlamp 3
When in protection groove 601, cleaning sponge block 7 is just in close contact the clear lamp blister of headlamp 3, can also pass through second
Motor 8 drives cleaning sponge block 7 to rotate, and cleaning is carried out to the clear lamp blister of headlamp 3.
Operation principle：The present invention drives headlamp 3 to rotate by first motor 5, controls headlamp 3 respectively vertical
The rotation that 180 degree is carried out in plane, to adjust illumination zone, and can according to the position of service condition adjusting illuminating lamp 3, wherein
Headlamp 3 can make being positioned against for protective plate 4 when need not use by the position of control headlamp 3, can by protective plate 4
To avoid impact of the space trash to 3 shell of headlamp, 3 lower end activity of headlamp is connected in protection groove 601, passes through bottom plate
Light bulb part more weak is protected on 6 pairs of headlamps 3, when headlamp 3 is located in protection groove 601, cleaning sponge
Block 7 is just in close contact the clear lamp blister of headlamp 3, cleaning sponge block 7 can also be driven to rotate by the second motor 8, right
The clear lamp blister of headlamp 3 carries out cleaning.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of aerospace outdoor illumination, including spacecraft shell (1) and headlamp (3), it is characterised in that：It is described
It is arranged with fixed otic placode (2) on the outside of spacecraft shell (1), passes through activity axis connection between two fixed otic placodes (2)
One end of the upper end of headlamp (3), the movable axis (3) is fixed with first motor (5), and the first motor (5) is fixedly mounted
On the fixation otic placode (2) of side, bottom plate (6), institute are fixed on the spacecraft shell (1) of fixed otic placode (2) lower end
It states and is recessed with protection groove (601) in the top surface of bottom plate (6), it is interior on the center of the protection groove (601) to be recessed with clearly
Clean sponge mounting groove (602), the cleaning sponge mounting groove (602) is interior to be equipped with cleaning sponge block (7), the cleaning sponge block
(7) bottom end is fixedly connected with the driving end of the second motor (8), and bottom plate (6), and second are run through in the driving end of second motor (8)
Motor (8) is mounted on bottom plate (6).
2. a kind of aerospace outdoor illumination according to claim 1, it is characterised in that：The headlamp (3)
Upper end be protection shell, bottom end be equipped with lighting bulb, the top of the headlamp (3) is installed with protection by connecting shaft
Plate (4), the protective plate (4) are rectangle plane plate or Curved plate structure.
3. a kind of aerospace outdoor illumination according to claim 1, it is characterised in that：The protective plate (4)
Limit shaft (401) is fixed on the end face of side, limit shaft (401) sliding is connected to side and fixes the interior of otic placode (2)
In the limiting slot (201) of side end face, the limiting slot (201) is semi-circular shape structure.
4. a kind of aerospace outdoor illumination according to claim 3, it is characterised in that：The limit shaft
(401) when being located at limiting slot (201) lower end, the light bulb of the headlamp (3) faces above spacecraft shell (1), works as limit
When axis (401) is located at limiting slot (201) upper end, the light bulb of the headlamp (3) faces below spacecraft shell (1), works as limit
When position axis (401) is located at limiting slot (201) centre position, bulb irradiation direction and the spacecraft shell (1) of the headlamp (3)
Side is vertical.
5. a kind of aerospace outdoor illumination according to claim 1, it is characterised in that：The protection groove
(601) width is more than the width of headlamp (3) lower end, is open type structure, the headlamp on the outside of the protection groove (601)
(3) it is slid on the outside of protection groove (601), and the top surface of bottom plate (6) is located at the upper end of headlamp (3) bottom surface.
6. a kind of aerospace outdoor illumination according to claim 1, it is characterised in that：The cleaning sponge block
(7) bottom end is equipped with metal mounting plate, which is fixedly mounted on the driving end of the second motor (8), the cleaning sea
The section of continuous block (7) and metal mounting plate is the circular configuration of same size, when headlamp (3) is located in protection groove (601)
When, the cleaning sponge block (7) is just in close contact the clear lamp blister of headlamp (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810082176.4A CN108382611A (en) | 2018-01-23 | 2018-01-23 | A kind of aerospace outdoor illumination |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810082176.4A CN108382611A (en) | 2018-01-23 | 2018-01-23 | A kind of aerospace outdoor illumination |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108382611A true CN108382611A (en) | 2018-08-10 |
Family
ID=63074147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810082176.4A Pending CN108382611A (en) | 2018-01-23 | 2018-01-23 | A kind of aerospace outdoor illumination |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108382611A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1153914A (en) * | 1997-07-31 | 1999-02-26 | San Fueibaa Japan:Kk | Sunlight-tracking type sunlight condensing device |
| CN101463949A (en) * | 2008-12-15 | 2009-06-24 | 中国科学院上海技术物理研究所 | LED illumination device suitable for extravehicular activity of astronaut |
| CN102128372A (en) * | 2011-01-24 | 2011-07-20 | 林万炯 | LED (light-emitting diode) daylight lamp |
| CN202024296U (en) * | 2011-03-10 | 2011-11-02 | 安徽华东光电技术研究所 | Novel outboard space suit illuminating lamp |
| CN204153684U (en) * | 2014-09-25 | 2015-02-11 | 合肥晶晨光伏能源有限公司 | The lamp system of a kind of large-scale automated cleaning LED |
| WO2016110594A1 (en) * | 2015-01-08 | 2016-07-14 | Beckers Francis | Portable lighting device for diver or astronaut |
| CN105855202A (en) * | 2016-04-25 | 2016-08-17 | 国网山东省电力公司经济技术研究院 | Prompting device for illuminating lamp in power plant |
| CN205640632U (en) * | 2016-04-25 | 2016-10-12 | 陈杭楚 | Illumination lamps and lanterns with angular adjustment function |
| CN206386747U (en) * | 2017-02-08 | 2017-08-08 | 广州恒沅舞台灯光音响设备有限公司 | A kind of Multifunctional stage LED revolving lights |
| CN206802862U (en) * | 2017-04-19 | 2017-12-26 | 广州市玛雅文化传播有限公司 | Light of stage control device based on wireless network |
-
2018
- 2018-01-23 CN CN201810082176.4A patent/CN108382611A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1153914A (en) * | 1997-07-31 | 1999-02-26 | San Fueibaa Japan:Kk | Sunlight-tracking type sunlight condensing device |
| CN101463949A (en) * | 2008-12-15 | 2009-06-24 | 中国科学院上海技术物理研究所 | LED illumination device suitable for extravehicular activity of astronaut |
| CN102128372A (en) * | 2011-01-24 | 2011-07-20 | 林万炯 | LED (light-emitting diode) daylight lamp |
| CN202024296U (en) * | 2011-03-10 | 2011-11-02 | 安徽华东光电技术研究所 | Novel outboard space suit illuminating lamp |
| CN204153684U (en) * | 2014-09-25 | 2015-02-11 | 合肥晶晨光伏能源有限公司 | The lamp system of a kind of large-scale automated cleaning LED |
| WO2016110594A1 (en) * | 2015-01-08 | 2016-07-14 | Beckers Francis | Portable lighting device for diver or astronaut |
| CN105855202A (en) * | 2016-04-25 | 2016-08-17 | 国网山东省电力公司经济技术研究院 | Prompting device for illuminating lamp in power plant |
| CN205640632U (en) * | 2016-04-25 | 2016-10-12 | 陈杭楚 | Illumination lamps and lanterns with angular adjustment function |
| CN206386747U (en) * | 2017-02-08 | 2017-08-08 | 广州恒沅舞台灯光音响设备有限公司 | A kind of Multifunctional stage LED revolving lights |
| CN206802862U (en) * | 2017-04-19 | 2017-12-26 | 广州市玛雅文化传播有限公司 | Light of stage control device based on wireless network |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180810 |