CN205045770U - Aircraft is stopped nave boss and is hung commentaries on classics equipment - Google Patents
Aircraft is stopped nave boss and is hung commentaries on classics equipment Download PDFInfo
- Publication number
- CN205045770U CN205045770U CN201520644596.9U CN201520644596U CN205045770U CN 205045770 U CN205045770 U CN 205045770U CN 201520644596 U CN201520644596 U CN 201520644596U CN 205045770 U CN205045770 U CN 205045770U
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- China
- Prior art keywords
- actuating cylinder
- brake hub
- aircraft brake
- hydraulic actuating
- aircraft
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Abstract
The utility model discloses an aircraft is stopped nave boss and is hung commentaries on classics equipment, including braced frame, the carriage that can follow braced frame up -and -down motion is provided with in braced frame's inboard, the below of carriage is provided with first pneumatic cylinder being vertical, the piston rod and the carriage of first pneumatic cylinder are connected, be provided with the horizontal support arm on the carriage, at the articulated aircraft of the tip of the horizontal support arm nave boss holder of stopping, top at the horizontal support arm is provided with the second pneumatic cylinder along its length direction, the piston rod and the aircraft of second pneumatic cylinder are stopped the nave boss holder and are connected, can drive the aircraft during piston rod concertina movement of second pneumatic cylinder stops the nave boss holder and rotates between level and vertical position. The utility model discloses can realize easily that it slings and transport to the relevant position to stop nave boss with the aircraft, convenient operation, labour saving and time saving, the very big human cost of having saved has improved work efficiency, simple structure, it is convenient, with low costs to make, and the facilitate promotion is used.
Description
Technical field
The utility model relates to a kind of aircraft brake hub and hangs and turn equipment.
Background technology
Aircraft brake hub is very heavy, is all when mounted at present to use a large amount of manpower to go to lift, and require great effort very much, and workman's risk when lifting or carry aircraft brake hub is also larger, easily injured.
Summary of the invention
In order to solve the problems of the technologies described above, the utility model provides a kind of aircraft brake hub to hang to turn equipment.
The technical solution that the utility model adopts is:
A kind of aircraft brake hub hangs and turns equipment, comprise support frame, being provided with in the inner side of support frame can along the sliding rack of support frame up-and-down movement, the first hydraulic actuating cylinder is vertically provided with in the below of sliding rack, the piston rod of the first hydraulic actuating cylinder is connected with sliding rack, sliding rack is provided with horizontal support arms, at the end of horizontal support arms hinged aircraft brake hub holder, the second hydraulic actuating cylinder is provided with along its length above horizontal support arms, the piston rod of the second hydraulic actuating cylinder is connected with aircraft brake hub holder, aircraft brake hub holder can be driven to rotate between level and vertical position during the piston rod fore and aft motion of the second hydraulic actuating cylinder.
Preferably, the bottom of described support frame is provided with the first stretcher for manipulating the first hydraulic actuating cylinder, and for manipulating the crus secunda pedal of the second hydraulic actuating cylinder; Between the first stretcher and the first hydraulic actuating cylinder, be provided with the first hydraulic oil transfer line, the first hydraulic oil transfer line is provided with the first blowdown valve; Between crus secunda pedal and the second hydraulic actuating cylinder, be provided with the second hydraulic oil transfer line, the second hydraulic oil transfer line is provided with the second blowdown valve.
Preferably, the inner side of support frame is provided with sliding rail, be provided with in the both sides of sliding rack with sliding rail with the use of slide block.
Preferably, the piston rod end of described first hydraulic actuating cylinder connects a horizontal support bar, the two ends of horizontal support bar is provided with sprocket wheel, sprocket wheel is arranged with chain, and one end of described chain is connected with support frame, and the other end of chain is connected with sliding rack.
Preferably, described aircraft brake hub holder comprises U-shaped frame, the two ends of U-shaped frame are provided with movable jaw, the insertion termination inserting perforate on aircraft brake hub is provided with in the inner side of U-shaped frame, contiguous block is had in the middle part arranged outside of U-shaped frame, the end of the piston rod of described contiguous block and the second hydraulic actuating cylinder is hinged, and contiguous block is provided with the locating dowel pin of locating for U-shaped frame.
Preferably, the side of described support frame is provided with grille guard.
Preferably, the bottom of described support frame is provided with roller.
Advantageous Effects of the present utility model is:
The utility model can easily realize being sling by aircraft brake hub and being transported to relevant position, easy to operate, time saving and energy saving, save human cost greatly, improve work efficiency, reduce the risk probability that workman is injured in transport process, structure is simple, easily manufactured, cost is low, easy to utilize.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and detailed description of the invention, the utility model is described in further detail:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the front view of Fig. 1;
Fig. 3 is the rear view of Fig. 2;
Fig. 4 is the lateral plan of Fig. 1.
Detailed description of the invention
By reference to the accompanying drawings, a kind of aircraft brake hub hangs and turns equipment, comprises support frame 1, and being provided with in the inner side of support frame 1 can along the sliding rack 2 of support frame 1 up-and-down movement.The piston rod being vertically provided with the first hydraulic actuating cylinder 3, first hydraulic actuating cylinder 3 in the below of sliding rack 2 is connected with sliding rack 2, and sliding rack 2 is provided with horizontal support arms 4, at the end of horizontal support arms 4 hinged aircraft brake hub holder 5.The second hydraulic actuating cylinder 6 is provided with along its length above horizontal support arms 4, the piston rod of the second hydraulic actuating cylinder is connected with aircraft brake hub holder 5, aircraft brake hub holder 5 can be driven to rotate between level and vertical position during the piston rod fore and aft motion of the second hydraulic actuating cylinder 6.
As to further improvement of the utility model, the bottom of described support frame 1 is provided with the first stretcher 7 for manipulating the first hydraulic actuating cylinder, and for manipulating the crus secunda pedal 8 of the second hydraulic actuating cylinder.Between the first stretcher 7 and the first hydraulic actuating cylinder 3, be provided with the first hydraulic oil transfer line 9, the first hydraulic oil transfer line 9 is provided with the first blowdown valve 10.Between crus secunda pedal 8 and the second hydraulic actuating cylinder 6, be provided with the second hydraulic oil transfer line 11, the second hydraulic oil transfer line 11 is provided with the second blowdown valve 12.
Further, the inner side of support frame 1 is provided with sliding rail, be provided with in the both sides of sliding rack 2 with sliding rail with the use of slide block.
Further, the piston rod end of described first hydraulic actuating cylinder connects a horizontal support bar 13, the two ends of horizontal support bar is provided with sprocket wheel 14, sprocket wheel is arranged with chain 15.One end of described chain 15 is connected with support frame 1, and the other end of chain 15 is connected with sliding rack 2.
Further, described aircraft brake hub holder 5 comprises U-shaped frame 501, the two ends of U-shaped frame 501 are provided with movable jaw 502, the insertion termination 503 inserting perforate on aircraft brake hub is provided with in the inner side of U-shaped frame, contiguous block 504 is had in the middle part arranged outside of U-shaped frame, the end of the piston rod of described contiguous block and the second hydraulic actuating cylinder is hinged, and contiguous block is provided with the locating dowel pin 505 of locating for U-shaped frame.
Further, the side of described support frame 1 is provided with grille guard 16.
Further, the bottom of described support frame 1 is provided with roller 17.
The part do not addressed in aforesaid way is taked or uses for reference prior art to realize.
Above embodiment is only in order to illustrate the technical solution of the utility model and unrestricted, although be described in detail the utility model with reference to preferred embodiment, those of ordinary skill in the art is to be understood that, can modify to the technical solution of the utility model or equivalent replacement, and not departing from aim and the scope of the technical program, it all should be encompassed in the middle of right of the present utility model.
Claims (7)
1. an aircraft brake hub hangs and turns equipment, it is characterized in that: comprise support frame, being provided with in the inner side of support frame can along the sliding rack of support frame up-and-down movement, the first hydraulic actuating cylinder is vertically provided with in the below of sliding rack, the piston rod of the first hydraulic actuating cylinder is connected with sliding rack, sliding rack is provided with horizontal support arms, at the end of horizontal support arms hinged aircraft brake hub holder, the second hydraulic actuating cylinder is provided with along its length above horizontal support arms, the piston rod of the second hydraulic actuating cylinder is connected with aircraft brake hub holder, aircraft brake hub holder can be driven to rotate between level and vertical position during the piston rod fore and aft motion of the second hydraulic actuating cylinder.
2. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: the bottom of described support frame is provided with the first stretcher for manipulating the first hydraulic actuating cylinder, and for manipulating the crus secunda pedal of the second hydraulic actuating cylinder; Between the first stretcher and the first hydraulic actuating cylinder, be provided with the first hydraulic oil transfer line, the first hydraulic oil transfer line is provided with the first blowdown valve; Between crus secunda pedal and the second hydraulic actuating cylinder, be provided with the second hydraulic oil transfer line, the second hydraulic oil transfer line is provided with the second blowdown valve.
3. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: the inner side of support frame is provided with sliding rail, be provided with in the both sides of sliding rack with sliding rail with the use of slide block.
4. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: the piston rod end of described first hydraulic actuating cylinder connects a horizontal support bar, the two ends of horizontal support bar are provided with sprocket wheel, sprocket wheel is arranged with chain, one end of described chain is connected with support frame, and the other end of chain is connected with sliding rack.
5. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: described aircraft brake hub holder comprises U-shaped frame, the two ends of U-shaped frame are provided with movable jaw, the insertion termination inserting perforate on aircraft brake hub is provided with in the inner side of U-shaped frame, contiguous block is had in the middle part arranged outside of U-shaped frame, the end of the piston rod of described contiguous block and the second hydraulic actuating cylinder is hinged, and contiguous block is provided with the locating dowel pin of locating for U-shaped frame.
6. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: the side of described support frame is provided with grille guard.
7. a kind of aircraft brake hub according to claim 1 hangs and turns equipment, it is characterized in that: the bottom of described support frame is provided with roller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520644596.9U CN205045770U (en) | 2015-08-25 | 2015-08-25 | Aircraft is stopped nave boss and is hung commentaries on classics equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520644596.9U CN205045770U (en) | 2015-08-25 | 2015-08-25 | Aircraft is stopped nave boss and is hung commentaries on classics equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205045770U true CN205045770U (en) | 2016-02-24 |
Family
ID=55339368
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520644596.9U Active CN205045770U (en) | 2015-08-25 | 2015-08-25 | Aircraft is stopped nave boss and is hung commentaries on classics equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205045770U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108689158A (en) * | 2018-06-22 | 2018-10-23 | 张蔡超 | One kind embracing folder centralising device |
| CN111891377A (en) * | 2020-06-15 | 2020-11-06 | 成都飞机工业（集团）有限责任公司 | Movable aircraft owner wheel erection equipment |
-
2015
- 2015-08-25 CN CN201520644596.9U patent/CN205045770U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108689158A (en) * | 2018-06-22 | 2018-10-23 | 张蔡超 | One kind embracing folder centralising device |
| CN111891377A (en) * | 2020-06-15 | 2020-11-06 | 成都飞机工业（集团）有限责任公司 | Movable aircraft owner wheel erection equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |