CN213928215U - Anti-falling aircraft maintenance support - Google Patents
Anti-falling aircraft maintenance support Download PDFInfo
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- CN213928215U CN213928215U CN202022557531.4U CN202022557531U CN213928215U CN 213928215 U CN213928215 U CN 213928215U CN 202022557531 U CN202022557531 U CN 202022557531U CN 213928215 U CN213928215 U CN 213928215U
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Abstract
The utility model discloses an anti-falling aircraft maintenance support, which comprises a bracket body, the constant head tank has been seted up on the right side at support body top, the inner chamber of constant head tank is provided with the guard plate, movable groove has all been seted up to the front side and the rear side of guard plate bottom, movable inslot chamber's bottom is provided with fixed establishment, the spout that uses with the fixed establishment cooperation is seted up to movable groove's bottom, the first through-hole that uses with the fixed establishment cooperation is seted up at the top of spout. Through the cooperation that sets up support body, constant head tank, guard plate, movable groove, fixed establishment, spout, first through-hole, fixed slot, stop gear, second through-hole and fourth through-hole, it is not convenient for protect repair tools to have solved current maintenance support, can use repair tools when maintaining the aircraft, and at the in-process that uses, repair tools drops from the maintenance support easily, influences the problem that the user used to repair tools.
Description
Technical Field
The utility model belongs to the technical field of the maintenance support, especially, relate to an anti-falling aircraft maintenance support.
Background
The maintenance has three explanations, namely, replacing accessories, maintaining the accessories, modifying according to functions, maintaining and recovering, maintaining and repairing.
Can use when maintaining the aircraft and take the maintenance support convenience to maintain the aircraft to sum up, the problem that prior art exists is: not convenient for protect repair tools, can use repair tools when the maintenance aircraft, and at the in-process that uses, repair tools drops from the maintenance support easily, influences the user and uses repair tools.
SUMMERY OF THE UTILITY MODEL
Problem to prior art exists, the utility model provides an aircraft maintenance support of anti-drop possesses the advantage of being convenient for protect maintenance tool, has solved current maintenance support and is not convenient for protect maintenance tool, can use maintenance tool when maintaining the aircraft, and at the in-process that uses, maintenance tool drops from maintenance support easily, influences the problem that the user used maintenance tool.
The utility model discloses a realize like this, an aircraft maintenance support of anti-drop, which comprises a bracket body, the constant head tank has been seted up on the right side at support body top, the inner chamber of constant head tank is provided with the guard plate, the activity groove has all been seted up to the front side and the rear side of guard plate bottom, the bottom of activity inslot chamber is provided with fixed establishment, the spout that uses with the fixed establishment cooperation is seted up to the bottom in activity groove, the first through-hole that uses with the fixed establishment cooperation is seted up at the top of spout, the fixed slot that uses with the fixed establishment cooperation is all seted up to the front side and the rear side of constant head tank both sides, the top in activity groove is provided with the stop gear who uses with the fixed establishment cooperation, the second through-hole that uses with the fixed establishment cooperation is all seted up at the top of activity groove both sides.
As the utility model discloses it is preferred, fixed establishment includes the spring, the both sides of spring all are provided with the fixed column, the equal fixedly connected with spliced pole in bottom of fixed column, first through-hole is passed and the inner chamber and the fixedly connected with slider that extend to the spout in the bottom of spliced pole, one side that the spring was kept away from to the fixed column runs through the guard plate and extends to the inner chamber of fixed slot, the third through-hole that uses with the stop gear cooperation is seted up on the surface of fixed column.
As the utility model discloses it is preferred, stop gear includes the limiting plate, the equal fixedly connected with connecting block in both sides of limiting plate, one side that the limiting plate was kept away from to the connecting block is passed the second through-hole and is extended to the outside and the fixedly connected with of guard plate and draw the piece, the equal fixedly connected with gag lever post in both sides of limiting plate bottom, the bottom fixedly connected with slide bar of gag lever post front side, the front side of slide bar extends to the inner chamber of third through-hole.
As the utility model discloses it is preferred, the guard plate is close to one side of constant head tank inner wall and the inner wall contact of constant head tank, the fourth through-hole that uses with the fixed column cooperation is all seted up to the both sides of activity tank bottom portion.
As the utility model discloses it is preferred, the both sides of spring all with fixed column fixed connection, the spliced pole is close to one side of first through-hole inner wall and the inner wall contact of first through-hole, the slider is close to one side of spout inner wall and the inner wall contact of spout, the fixed column is close to one side of fixed slot inner wall and the inner wall contact of fixed slot.
As the utility model discloses it is preferred, the limiting plate is close to the contact of one side of activity inslot wall and the inner wall of activity groove, the connecting block is close to one side of second through-hole inner wall and the inner wall contact of second through-hole, draw one side and the guard plate contact that the piece is close to the guard plate, the slide bar is close to one side of third through-hole inner wall and the inner wall contact of third through-hole.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a cooperation that sets up support body, constant head tank, guard plate, activity groove, fixed establishment, spout, first through-hole, fixed slot, stop gear, second through-hole and fourth through-hole is used, has solved current maintenance support and has not been convenient for protect service tool, can use service tool when maintaining the aircraft, and at the in-process that uses, service tool drops from the maintenance support easily, influences the problem that the user used service tool.
2. The utility model discloses a set up fixed establishment, can play the fixed action to the guard plate, the person of facilitating the use installs the guard plate.
3. The utility model discloses a set up stop gear, can play limiting displacement to fixed establishment, the person of facilitating the use uses fixed establishment.
4. The utility model discloses a set up the constant head tank, can play the positioning action to the guard plate, through setting up the fourth through-hole, can play limiting displacement to the fixed column.
5. The utility model discloses a set up the spring, can play the reset action to the fixed column, through setting up the spliced pole, can drive the slider and slide at the inner chamber of spout, through setting up the slider, can remove to the fixed column and play limiting displacement, through setting up fixed column and fixed slot, can play the fixed action to the guard plate.
6. The utility model discloses a set up the limiting plate, can drive the slide bar through the gag lever post and remove, draw the piece through the setting, can drive the limiting plate through the connecting block and slide at the inner chamber of activity groove, through setting up the slide bar, can drive the fixed column and remove.
Drawings
Fig. 1 is a schematic structural diagram provided in an embodiment of the present invention;
fig. 2 is a partial cross-sectional view of an embodiment of the invention providing a front view;
fig. 3 is a partial enlarged view of a portion a in fig. 2 according to an embodiment of the present invention.
In the figure: 1. a stent body; 2. positioning a groove; 3. a protection plate; 4. a movable groove; 5. a fixing mechanism; 6. a chute; 7. a first through hole; 8. fixing grooves; 9. a limiting mechanism; 10. a second through hole; 11. a fourth via hole; 501. a spring; 502. fixing a column; 503. connecting columns; 504. a slider; 505. a third through hole; 901. a limiting plate; 902. connecting blocks; 903. pulling the block; 904. a limiting rod; 905. a slide bar.
Detailed Description
In order to further understand the contents, features and effects of the present invention, the following embodiments are illustrated and described in detail with reference to the accompanying drawings.
The structure of the present invention will be described in detail with reference to the accompanying drawings.
As shown in fig. 1 to 3, the embodiment of the utility model provides a pair of anti-falling aircraft maintenance support, including support body 1, constant head tank 2 has been seted up on the right side at support body 1 top, the inner chamber of constant head tank 2 is provided with guard plate 3, movable groove 4 has all been seted up to the front side and the rear side of 3 bottoms of guard plate, the bottom of 4 inner chambers in movable groove is provided with fixed establishment 5, spout 6 that uses with the cooperation of fixed establishment 5 has been seted up to the bottom in movable groove 4, first through-hole 7 that uses with the cooperation of fixed establishment 5 has been seted up at the top of spout 6, fixed slot 8 that uses with the cooperation of fixed establishment 5 has all been seted up to the front side and the rear side of constant head tank 2 both sides, the top in movable groove 4 is provided with stop gear 9 that uses with the cooperation of fixed establishment 5, second through-hole 10 that uses with the cooperation of fixed establishment 5 has all been seted up at the top in movable groove 4 both sides.
Referring to fig. 2 and 3, the fixing mechanism 5 includes a spring 501, both sides of the spring 501 are provided with fixing columns 502, the bottom of each fixing column 502 is fixedly connected with a connecting column 503, the bottom of each connecting column 503 passes through a first through hole 7 and extends to an inner cavity of the sliding chute 6 and a sliding block 504, one side of each fixing column 502, which is far away from the spring 501, penetrates through the protection plate 3 and extends to the inner cavity of the fixing groove 8, and third through holes 505 matched with the limiting mechanisms 9 for use are formed in the surface of each fixing column 502.
Adopt above-mentioned scheme: through setting up fixed establishment 5, can play the fixed action to guard plate 3, the person of facilitating the use installs guard plate 3.
Referring to fig. 2 and 3, the limiting mechanism 9 includes a limiting plate 901, a connecting block 902 is fixedly connected to both sides of the limiting plate 901, one side of the connecting block 902, which is away from the limiting plate 901, passes through the second through hole 10 and extends to the outer side of the protection plate 3, and is fixedly connected with a pull block 903, a limiting rod 904 is fixedly connected to both sides of the bottom of the limiting plate 901, a sliding rod 905 is fixedly connected to the bottom of the front side of the limiting rod 904, and the front side of the sliding rod 905 extends to the inner cavity of the third through hole 505.
Adopt above-mentioned scheme: through setting up stop gear 9, can play limiting displacement to fixed establishment 5, the person of facilitating the use uses fixed establishment 5.
Referring to fig. 2 and 3, one side of the protection plate 3 close to the inner wall of the positioning groove 2 contacts the inner wall of the positioning groove 2, and the two sides of the bottom of the movable groove 4 are both provided with fourth through holes 11 matched with the fixing posts 502 for use.
Adopt above-mentioned scheme: through setting up constant head tank 2, can play the positioning action to guard plate 3, through setting up fourth through-hole 11, can play limiting displacement to fixed column 502.
Referring to fig. 2 and 3, both sides of the spring 501 are fixedly connected to the fixing column 502, one side of the connecting column 503 close to the inner wall of the first through hole 7 is in contact with the inner wall of the first through hole 7, one side of the slider 504 close to the inner wall of the sliding chute 6 is in contact with the inner wall of the sliding chute 6, and one side of the fixing column 502 close to the inner wall of the fixing chute 8 is in contact with the inner wall of the fixing chute 8.
Adopt above-mentioned scheme: through setting up spring 501, can play the effect that resets to fixed column 502, through setting up spliced pole 503, can drive slider 504 and slide in the inner chamber of spout 6, through setting up slider 504, can remove to fixed column 502 and play limiting displacement, through setting up fixed column 502 and fixed slot 8, can play the fixed action to guard plate 3.
Referring to fig. 2 and 3, one side of the limiting plate 901 close to the inner wall of the movable groove 4 contacts with the inner wall of the movable groove 4, one side of the connecting block 902 close to the inner wall of the second through hole 10 contacts with the inner wall of the second through hole 10, one side of the pulling block 903 close to the protection plate 3 contacts with the protection plate 3, and one side of the sliding rod 905 close to the inner wall of the third through hole 505 contacts with the inner wall of the third through hole 505.
Adopt above-mentioned scheme: through setting up limiting plate 901, can drive slide bar 905 and remove through gag lever post 904, draw piece 903 through the setting, can drive limiting plate 901 through connecting block 902 and slide in the inner chamber of activity groove 4, through setting up slide bar 905, can drive fixed column 502 and remove.
The utility model discloses a theory of operation:
when the protective device is used, a user pulls the pull block 903, the pull block 903 drives the limiting plate 901 to slide in the inner cavity of the movable groove 4 through the connecting block 902, the limiting plate 901 drives the fixing column 502 to enter the movable groove 4 through the limiting rod 904 and the sliding rod 905 and extrude the spring 501, the fixing column 502 drives the sliding block 504 to slide in the inner cavity of the sliding groove 6 through the connecting block, the user places the protective plate 3 in the inner cavity of the positioning groove 2 and then loosens the pull block 903, the fixing column 502 is pushed to move reversely by the force released after the spring 501 extrudes and enters the inner cavity of the fixing groove 8, the sliding block 504 is driven to slide reversely in the inner cavity of the sliding groove 6 through the connecting column 503, the fixing column 502 drives the limiting plate 901 to slide reversely in the inner cavity of the movable groove 4 through the sliding rod 905 and the limiting rod 904 and reset, and installation is completed.
In summary, the following steps: this anti-falling aircraft maintenance support, through setting up support body 1, constant head tank 2, guard plate 3, the activity groove 4, fixed establishment 5, spout 6, first through-hole 7, fixed slot 8, stop gear 9, the cooperation of second through-hole 10 and fourth through-hole 11 is used, it is not convenient for protect repair tools to have solved current maintenance support, can use repair tools when the maintenance aircraft, and at the in-process that uses, repair tools drops from the maintenance support easily, influence the user and carry out the problem that uses to repair tools.
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 an aircraft maintenance support of anti falling, includes support body (1), its characterized in that: a positioning groove (2) is arranged on the right side of the top of the bracket body (1), a protection plate (3) is arranged in the inner cavity of the positioning groove (2), the front side and the rear side of the bottom of the protection plate (3) are both provided with a movable groove (4), the bottom of the inner cavity of the movable groove (4) is provided with a fixed mechanism (5), the bottom of the movable groove (4) is provided with a sliding groove (6) matched with the fixed mechanism (5), the top of the sliding chute (6) is provided with a first through hole (7) which is matched with the fixing mechanism (5), the front side and the rear side of the two sides of the positioning groove (2) are both provided with fixing grooves (8) matched with the fixing mechanism (5), the top of the movable groove (4) is provided with a limiting mechanism (9) which is matched with the fixing mechanism (5), and second through holes (10) matched with the fixing mechanism (5) for use are formed in the tops of the two sides of the movable groove (4).
2. An anti-drop aircraft maintenance support according to claim 1, wherein: fixing mechanism (5) include spring (501), the both sides of spring (501) all are provided with fixed column (502), the equal fixedly connected with spliced pole (503) in bottom of fixed column (502), first through-hole (7) are passed and inner chamber and the fixedly connected with slider (504) of spout (6) are extended to the bottom of spliced pole (503), one side that spring (501) were kept away from in fixed column (502) runs through guard plate (3) and extends to the inner chamber of fixed slot (8), third through-hole (505) that use with stop gear (9) cooperation are seted up on the surface of fixed column (502).
3. An anti-drop aircraft maintenance support according to claim 2, wherein: the limiting mechanism (9) comprises a limiting plate (901), connecting blocks (902) are fixedly connected to the two sides of the limiting plate (901), one side, far away from the limiting plate (901), of each connecting block (902) penetrates through the second through hole (10) and extends to the outer side of the protection plate (3), each connecting block (903) is fixedly connected to the outer side of the corresponding protection plate, a limiting rod (904) is fixedly connected to the two sides of the bottom of the limiting plate (901), a sliding rod (905) is fixedly connected to the bottom of the front side of the limiting rod (904), and the front side of the sliding rod (905) extends to the inner cavity of the third through hole (505).
4. An anti-drop aircraft maintenance support according to claim 2, wherein: one side that guard plate (3) is close to constant head tank (2) inner wall contacts with the inner wall of constant head tank (2), fourth through-hole (11) that use with fixed column (502) cooperation are all seted up to the both sides of activity groove (4) bottom.
5. An anti-drop aircraft maintenance support according to claim 2, wherein: both sides of the spring (501) are fixedly connected with a fixing column (502), one side, close to the inner wall of the first through hole (7), of the connecting column (503) is in contact with the inner wall of the first through hole (7), one side, close to the inner wall of the sliding groove (6), of the sliding block (504) is in contact with the inner wall of the sliding groove (6), and one side, close to the inner wall of the fixing groove (8), of the fixing column (502) is in contact with the inner wall of the fixing groove (8).
6. A drop-resistant aircraft maintenance support according to claim 3, wherein: the limiting plate (901) is close to the contact of one side of the inner wall of the movable groove (4) and the inner wall of the movable groove (4), the connecting block (902) is close to the contact of one side of the inner wall of the second through hole (10) and the inner wall of the second through hole (10), the pulling block (903) is close to the contact of one side of the protection plate (3) and the protection plate (3), and the sliding rod (905) is close to the contact of one side of the inner wall of the third through hole (505) and the inner wall of the third through hole (505).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022557531.4U CN213928215U (en) | 2020-11-08 | 2020-11-08 | Anti-falling aircraft maintenance support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022557531.4U CN213928215U (en) | 2020-11-08 | 2020-11-08 | Anti-falling aircraft maintenance support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213928215U true CN213928215U (en) | 2021-08-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022557531.4U Active CN213928215U (en) | 2020-11-08 | 2020-11-08 | Anti-falling aircraft maintenance support |
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| Country | Link |
|---|---|
| CN (1) | CN213928215U (en) |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211203 Address after: 300000 No. 314, unit 1, building 19, Ruihang Plaza, pilot free trade zone (Airport Economic Zone), Binhai New Area, Tianjin Patentee after: Liangjie Aviation Technology (Tianjin) Co.,Ltd. Address before: 300000 19-1-314 Ruihang Plaza, pilot free trade zone (Airport Economic Zone) of Binhai New Area, Tianjin Patentee before: LIGHTJET AVIATION TECHNOLOGY SERVICE Co.,Ltd. |