CN210293261U - Protection mechanism of space flight detection equipment - Google Patents
Protection mechanism of space flight detection equipment Download PDFInfo
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- CN210293261U CN210293261U CN201921472580.9U CN201921472580U CN210293261U CN 210293261 U CN210293261 U CN 210293261U CN 201921472580 U CN201921472580 U CN 201921472580U CN 210293261 U CN210293261 U CN 210293261U
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- fixedly connected
- detection equipment
- protecting crust
- protective shell
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Abstract
The utility model discloses a protection machanism of space flight detection equipment, including the detection equipment body, the sliding surface of detection equipment body is connected with the protecting crust, the positive fixedly connected with apron of protecting crust, the back of protecting crust is provided with the mounting panel, the equal fixedly connected with fixed block in the positive both sides of mounting panel, the inboard of fixed block and the sliding surface of protecting crust are connected, the equal fixedly connected with fixed establishment in both sides of protecting crust. The utility model discloses a set up the cooperation of detection equipment body, protecting crust, apron, mounting panel, fixed block, fixed establishment, piece, fixture block, horizontal piece and spring and used, solved current detection equipment at the in-process that uses, can't protect detection equipment, lead to detection equipment easily because of the collision friction, lead to the problem that detection equipment damaged, this space flight detection equipment's protection machanism possesses the advantage of protection, has improved detection equipment's practicality.
Description
Technical Field
The utility model relates to an aerospace technical field specifically is a protection machanism of space flight detection equipment.
Background
Space flight is also called space flight, cosmonautic or space flight, and refers to the general name of various activities of entering, exploring, developing and utilizing space and celestial bodies outside the earth, the space activities include three major parts of space technology, space application and space science, the space technology refers to comprehensive engineering technology providing technical means and guarantee conditions for space activities, and most visible light photodetectors adopted on space remote sensors are mainly photon detectors.
In the process of spaceflight, the detection equipment is required to be used for detecting the environment, but the existing detection equipment cannot protect the detection equipment in the using process, so that the detection equipment is easily damaged due to collision and friction, and the practicability of the detection equipment is reduced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a protection machanism of space flight detection equipment possesses the advantage of protection, has solved current detection equipment and at the in-process that uses, can't protect detection equipment, leads to detection equipment to lead to the problem of detection equipment damage because of the collision friction easily.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a protection machanism of space flight detection equipment, includes the detection equipment body, the surperficial sliding connection of detection equipment body has the protecting crust, the positive fixedly connected with apron of protecting crust, the back of protecting crust is provided with the mounting panel, the equal fixedly connected with fixed block in the positive both sides of mounting panel, the inboard of fixed block and the surperficial sliding connection of protecting crust, the equal fixedly connected with fixed establishment in both sides of protecting crust, fixed establishment's inboard runs through to the inside of protecting crust.
Preferably, the fixing mechanism comprises a supporting block, the inner side of the supporting block is fixedly connected with the outer side of the protective shell, a placing groove is formed in the supporting block, a clamping block is arranged in the placing groove, the outer side of the clamping block penetrates through the outer side of the supporting block, the inner side of the clamping block penetrates through the inner side of the protective shell, a transverse block is fixedly connected with the surface of the clamping block, the top and the bottom of the transverse block are both in sliding connection with the inner wall of the placing groove, a spring is sleeved on the surface of the clamping block, the outer side of the spring is fixedly connected with the inner wall of the placing groove, and the inner side of the spring is fixedly connected with the outer side of the transverse block.
Preferably, the back fixedly connected with of apron is sealed fills up, the back of sealed pad and the front contact of protecting crust, first recess has been seted up in the front of apron, and the inside of first recess is provided with the bolt, and the screw thread end of bolt runs through to the back and the protecting crust fixed connection of apron, and the quantity of first recess and bolt is four, and four first recesses and four bolts all are the equidistance and distribute.
Preferably, the fixed slot that uses with the fixed block cooperation is all seted up to the both sides of protecting crust, the card hole that uses with the fixture block cooperation is seted up in the outside of fixed block, the draw-in groove that uses with the fixture block cooperation is seted up to the inner wall of fixed slot, the shape of fixed block and fixed slot is semi-circular.
Preferably, the through-hole has been seted up in the front of apron, the inner wall fixedly connected with transparent plate of through-hole, the shape of transparent plate and through-hole is square, the back fixedly connected with gasket of apron, the back of gasket and the front contact of detection equipment body, the quantity of gasket is four, and four gaskets are the equidistance and distribute.
Preferably, the equal fixedly connected with stopper in top and the bottom of protecting crust inner wall, the spacing groove that uses with the stopper cooperation is seted up on the surface of detection equipment body, the shape of stopper and spacing groove is semi-circular, the equal fixedly connected with supporting shoe in both sides of mounting panel bottom, the movable groove that uses with the supporting shoe cooperation is seted up to the bottom of protecting crust, the bottom fixedly connected with dog of protecting crust, the back of dog is seted up and is supported the groove that uses with the supporting shoe cooperation, the top of protecting crust both sides all has the riser through hinge swing joint, the second recess has been seted up to the inboard of riser, and the second recess uses with fixture block and a piece cooperation.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a set up the cooperation of detection equipment body, protecting crust, apron, mounting panel, fixed block, fixed establishment, piece, fixture block, horizontal piece and spring and used, solved current detection equipment at the in-process that uses, can't protect detection equipment, lead to detection equipment easily because of the collision friction, lead to the problem that detection equipment damaged, this space flight detection equipment's protection machanism possesses the advantage of protection, has improved detection equipment's practicality.
2. The utility model can reduce the friction between the cover plate and the protective shell by arranging the sealing gasket, prolong the service life of the cover plate, simultaneously play a sealing role for the protective shell, prevent the cover plate from separating from the protective shell by arranging the bolt, play a limiting role for the protective shell by matching the fixed block and the fixed groove, prevent the protective shell from moving when not moving by arranging the clamping hole and the clamping groove, simultaneously play a limiting role for the protective shell, facilitate the detection of the detection equipment body to the outer side of the protective shell by matching the through hole and the transparent plate, play a limiting role for the position of the detection equipment body by arranging the gasket, play a limiting role for the position of the detection equipment body by matching the limiting block and the limiting groove, and play a limiting role for the position of the detection equipment body by arranging the supporting block, can play spacing and supported effect to the protecting crust, through the setting in activity groove, can reduce the friction of supporting shoe and protecting crust, prolonged the life of supporting shoe.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view of the structure A in FIG. 1 according to the present invention;
fig. 3 is a left side sectional view of the structure of fig. 1 according to the present invention.
In the figure: 1 detection equipment body, 2 protecting crust, 3 apron, 4 mounting panels, 5 fixed blocks, 6 fixed establishment, 61 piece, 62 fixture blocks, 63 horizontal block, 64 springs, 7 sealed pad, 8 transparent plates, 9 gaskets, 10 stopper, 11 supporting shoe, 12 dogs, 13 risers.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, a protection mechanism of an aerospace detection device comprises a detection device body 1, a protective shell 2 is slidably connected to the surface of the detection device body 1, a cover plate 3 is fixedly connected to the front surface of the protective shell 2, a mounting plate 4 is arranged on the back surface of the protective shell 2, fixing blocks 5 are fixedly connected to both sides of the front surface of the mounting plate 4, the inner side of each fixing block 5 is slidably connected to the surface of the protective shell 2, fixing mechanisms 6 are fixedly connected to both sides of the protective shell 2, each fixing mechanism 6 comprises a support block 61, the inner side of each support block 61 is fixedly connected to the outer side of the protective shell 2, a placement groove is formed in each support block 61, a fixture block 62 is arranged in each placement groove, the outer side of each fixture block 62 penetrates through the outer side of the support block 61, the inner side of each fixture block 62 penetrates through the inner side of the protective shell 2, a cross block 63 is fixedly connected to the surface of, the surface of the clamping block 62 is sleeved with a spring 64, the outer side of the spring 64 is fixedly connected with the inner wall of the placing groove, the inner side of the spring 64 is fixedly connected with the outer side of the cross block 63, the inner side of the fixing mechanism 6 penetrates into the protective shell 2, the back surface of the cover plate 3 is fixedly connected with a sealing gasket 7, the back surface of the sealing gasket 7 is contacted with the front surface of the protective shell 2, the front surface of the cover plate 3 is provided with a first groove, a bolt is arranged in the first groove, the threaded end of the bolt penetrates into the back surface of the cover plate 3 and is fixedly connected with the protective shell 2, the number of the first groove and the number of the bolts are four, the four first grooves and the four bolts are distributed at equal intervals, through the arrangement of the sealing gasket 7, the friction between the cover plate 3 and the protective shell 2 can be reduced, the service life of the cover plate 3 is prolonged, meanwhile, the sealing effect, fixing grooves matched with the fixing blocks 5 are formed in two sides of the protective shell 2, clamping holes matched with the clamping blocks 62 are formed in the outer sides of the fixing blocks 5, clamping grooves matched with the clamping blocks 62 are formed in the inner walls of the fixing grooves, the fixing blocks 5 and the fixing grooves are semicircular, the protective shell 2 can be limited through the matching of the fixing blocks 5 and the fixing grooves, the protective shell 2 can be prevented from moving when not required to move due to the arrangement of the clamping holes and the clamping grooves, the protective shell 2 can be limited, through holes are formed in the front face of the cover plate 3, transparent plates 8 are fixedly connected to the inner walls of the through holes, the transparent plates 8 and the through holes are square, gaskets 9 are fixedly connected to the back face of the cover plate 3, the back faces of the gaskets 9 are in contact with the front face of the detection device body 1, the number of the gaskets 9 is four, and the, through the matching use of the through hole and the transparent plate 8, the detection device body 1 can conveniently detect the outer side of the protective shell 2, through the arrangement of the gasket 9, the position of the detection device body 1 can be limited, the top and the bottom of the inner wall of the protective shell 2 are both fixedly connected with the limiting blocks 10, the surface of the detection device body 1 is provided with limiting grooves matched with the limiting blocks 10 for use, the shapes of the limiting blocks 10 and the limiting grooves are both semicircular, the two sides of the bottom of the mounting plate 4 are both fixedly connected with the supporting blocks 11, the bottom of the protective shell 2 is provided with the movable grooves matched with the supporting blocks 11 for use, the bottom of the protective shell 2 is fixedly connected with the stop blocks 12, the back of the stop blocks 12 is provided with supporting grooves matched with the supporting blocks 11 for use, the tops of the two sides of the protective shell 2 are both movably connected with the vertical plates 13 through hinges, the inner sides, the limiting device has the advantages that the limiting device is used through the matching of the limiting block 10 and the limiting groove, the limiting effect can be achieved on the position of the detection device body 1, the limiting and supporting effects can be achieved on the protective shell 2 through the arrangement of the supporting block 11, the friction between the supporting block 11 and the protective shell 2 can be reduced through the arrangement of the movable groove, and the service life of the supporting block 11 is prolonged.
When the device is used, a user rotates the vertical plate 13 to enable the vertical plate 13 to rotate around the hinge, the supporting block 61 and the clamping block 62 are separated from the second groove, then the clamping block 62 is pulled outwards, the clamping block 62 moves outwards to drive the transverse block 63 to move outwards, the clamping block 62 is separated from the clamping groove and the clamping hole in sequence, the transverse block 63 moves outwards to move the compression spring 64, then the protective shell 2 is pulled forwards to enable the fixing block 6 to be separated from the fixing groove and the supporting block 11 to be separated from the supporting groove and the movable groove in sequence, at the moment, the protective shell 2 can be disassembled, then the user rotates the bolt to enable the bolt to be separated from the protective shell 2, the cover plate 3 is pulled forwards, then the detection device body 1 is pulled forwards to enable the detection device body 1 to be separated from the protective shell 2, at the moment, the detection device body 1 can be disassembled, during installation, the user pushes, promote apron 3 backward, then the rotation bolt, make the bolt card advance the inside of protecting crust 2, fix the position of apron 3, can protect the detection equipment body 1 through protecting crust 2 and apron 3 this moment, then promote protecting crust 2 backward, make the inside of fixed block 5 card advance the fixed slot, loosen fixture block 62 simultaneously, spring 64's resilience force drives horizontal bar 63 and fixture block 62 and resets, make fixture block 62 block in proper order into the inside of card hole and draw-in groove, fix the position of protecting crust 2, can fix the position of protecting crust 2 this moment.
In summary, the following steps: this protection machanism of space flight detection equipment uses through the cooperation that sets up detection equipment body 1, protecting crust 2, apron 3, mounting panel 4, fixed block 5, fixed establishment 6, piece 61, fixture block 62, horizontal piece 63 and spring 64, has solved current detection equipment and at the in-process that uses, can't protect detection equipment, leads to detection equipment to lead to because of collision friction easily, leads to the problem of detection equipment damage.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a protection machanism of space flight detection equipment, includes detection equipment body (1), its characterized in that: the surface sliding connection of detection equipment body (1) has protecting crust (2), the positive fixedly connected with apron (3) of protecting crust (2), the back of protecting crust (2) is provided with mounting panel (4), the equal fixedly connected with fixed block (5) in the positive both sides of mounting panel (4), the inboard of fixed block (5) and the surface sliding connection of protecting crust (2), the equal fixedly connected with fixed establishment (6) in both sides of protecting crust (2), the inboard of fixed establishment (6) runs through to the inside of protecting crust (2).
2. A protection mechanism for an aerospace detection device according to claim 1, wherein: the fixing mechanism (6) comprises a supporting block (61), the inner side of the supporting block (61) is fixedly connected with the outer side of the protective shell (2), a placing groove is formed in the supporting block (61), a clamping block (62) is arranged in the placing groove, the outer side of the clamping block (62) penetrates through the outer side of the supporting block (61), the inner side of the clamping block (62) penetrates through the inner side of the protective shell (2), a transverse block (63) is fixedly connected to the surface of the clamping block (62), the top and the bottom of the transverse block (63) are both in sliding connection with the inner wall of the placing groove, a spring (64) is sleeved on the surface of the clamping block (62), the outer side of the spring (64) is fixedly connected with the inner wall of the placing groove, and the inner side of the spring (64) is fixedly connected with the outer side of the transverse block (63).
3. A protection mechanism for an aerospace detection device according to claim 1, wherein: the utility model discloses a safety protection device for cable, including apron (3), the sealed pad (7) of back fixedly connected with of apron (3), the front contact of the back of sealed pad (7) and protecting crust (2), first recess has been seted up in the front of apron (3), and the inside of first recess is provided with the bolt, and the screw thread end of bolt runs through back and protecting crust (2) fixed connection to apron (3), and the quantity of first recess and bolt is four, and four first recesses and four bolts all are the equidistance and distribute.
4. A protection mechanism for an aerospace detection device according to claim 2, wherein: the fixed slot that uses with fixed block (5) cooperation is all seted up to the both sides of protecting crust (2), the card hole that uses with fixture block (62) cooperation is seted up in the outside of fixed block (5), and the draw-in groove that uses with fixture block (62) cooperation is seted up to the inner wall of fixed slot, the shape of fixed block (5) and fixed slot is semi-circular.
5. A protection mechanism for an aerospace detection device according to claim 1, wherein: the through-hole has been seted up in the front of apron (3), the inner wall fixedly connected with transparent plate (8) of through-hole, the shape of transparent plate (8) and through-hole is square, back fixedly connected with gasket (9) of apron (3), the back of gasket (9) and the front contact of detection equipment body (1), the quantity of gasket (9) is four, and four gaskets (9) are the equidistance and distribute.
6. A protection mechanism for an aerospace detection device according to claim 1, wherein: the top and the bottom of the inner wall of the protective shell (2) are both fixedly connected with a limiting block (10), the surface of the detection device body (1) is provided with a limit groove which is matched with the limit block (10), the limiting blocks (10) and the limiting grooves are semicircular, the two sides of the bottom of the mounting plate (4) are fixedly connected with supporting blocks (11), the bottom of the protective shell (2) is provided with a movable groove which is matched with the supporting block (11) for use, the bottom of the protective shell (2) is fixedly connected with a stop block (12), the back of the stop block (12) is provided with a supporting groove matched with the supporting block (11), the tops of both sides of the protective shell (2) are movably connected with vertical plates (13) through hinges, a second groove is formed in the inner side of the vertical plate (13), and the second groove is matched with the clamping block (62) and the supporting block (61) for use.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921472580.9U CN210293261U (en) | 2019-09-05 | 2019-09-05 | Protection mechanism of space flight detection equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921472580.9U CN210293261U (en) | 2019-09-05 | 2019-09-05 | Protection mechanism of space flight detection equipment |
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| CN210293261U true CN210293261U (en) | 2020-04-10 |
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| CN201921472580.9U Active CN210293261U (en) | 2019-09-05 | 2019-09-05 | Protection mechanism of space flight detection equipment |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112129417A (en) * | 2020-09-23 | 2020-12-25 | 合肥科塑信息科技有限公司 | Pyroelectric infrared sensor |
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2019
- 2019-09-05 CN CN201921472580.9U patent/CN210293261U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112129417A (en) * | 2020-09-23 | 2020-12-25 | 合肥科塑信息科技有限公司 | Pyroelectric infrared sensor |
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