CN214729714U - Helicopter engine combined bracket - Google Patents
Helicopter engine combined bracket Download PDFInfo
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- CN214729714U CN214729714U CN202120359791.2U CN202120359791U CN214729714U CN 214729714 U CN214729714 U CN 214729714U CN 202120359791 U CN202120359791 U CN 202120359791U CN 214729714 U CN214729714 U CN 214729714U
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Abstract
The utility model relates to an aviation maintenance auxiliary assembly technical field especially relates to helicopter engine combination bracket, which comprises a supporting rack, support frame surface mounting has supporting component, supporting component installs on the support frame surface adjustably, supporting component includes first bracket component, the second bracket component, the third bracket component, fourth bracket component and fifth bracket component, first bracket component, the second bracket component, the third bracket component, fourth bracket component and fifth bracket component install on the support frame replaceably respectively, supporting component has collected five kinds of series of engine brackets and has installed on the support frame in an organic whole, comprehensive properties is stronger, and can be according to demand detachably dismouting, make things convenient for the field rush-repair to use, the very big packing demand that satisfies of size after the dismantlement, be convenient for the transportation, moreover, the steam generator is simple in structure, and convenient for operation.
Description
Technical Field
The utility model relates to an aviation maintenance auxiliary assembly technical field especially relates to helicopter engine combination bracket.
Background
The models corresponding to the engine brackets of the original series of Z-8, Z-9, Z-10, AN9B and M171 are all single integers, and the single integers are generally large in size and heavy, consume a large amount of transportation resources when being transported, and need high cost.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a helicopter engine combination bracket to prior art's not enough.
In order to achieve the above purpose, the technical scheme of the utility model is as follows:
helicopter engine combination bracket, including the support frame, support frame surface mounting has supporting component, and supporting component adjustably installs at the support frame surface, and supporting component includes first bracket component, second bracket component, third bracket component, fourth bracket component and fifth bracket component, and first bracket component, second bracket component, third bracket component, fourth bracket component and fifth bracket component are installed on the support frame replaceably respectively.
Further: the support frame includes two chassis, and two chassis mutually perpendicular set up splices into T shape frame, and every chassis surface is followed its length direction shaping and is had the installation guide rail, and the embedding of supporting component adjustable, replaceability is in the installation guide rail, and the hand lever is installed to one of them base tip.
Further: the first bracket component is a Z-8 series engine bracket and comprises at least two first front brackets and at least two first rear brackets, the two first front brackets are symmetrically arranged on one underframe, and the first rear brackets are arranged on the other underframe.
Further: the second bracket component is a Z-9 series engine bracket and comprises a second front bracket and a second rear bracket which are coaxially arranged, auxiliary hooks are respectively arranged on two sides of the second front bracket, the second front bracket and the second rear bracket are installed on one of the underframe, and the two auxiliary hooks are installed on the other underframe.
Further: the third bracket assembly is a Z-10 series engine bracket and comprises a third front bracket and a third rear bracket which are different in height, the number of the third front brackets is at least two, the two third front brackets are simultaneously installed on one underframe, and the third rear bracket is installed on the other underframe.
Further: the fourth bracket component is an M-171 series engine bracket, the fourth bracket component comprises a fourth front bracket and a fourth rear bracket, the fourth front bracket comprises at least two front brackets, the top of the fourth front bracket is provided with a forked auxiliary supporting rod, the two fourth front brackets are simultaneously installed on one of the underframe, and the fourth rear bracket is installed on the other underframe.
Further: the fifth bracket component is AN AN9B series engine bracket, the fifth bracket component comprises a fifth bracket component which comprises a fifth front bracket and a fifth rear bracket with different heights, the number of the fifth front bracket is at least two, the top of the fifth front bracket is formed with a forked auxiliary supporting column, the two fifth front brackets are simultaneously installed on one underframe, and the fifth rear bracket is installed on the other underframe.
The utility model has the advantages that: the utility model discloses a helicopter engine sectional shelf-unit, supporting component have collected five kinds of series's engine bracket and have installed on the support frame in an organic whole, and comprehensive properties is stronger to can make things convenient for the field to salvage the use according to demand detachably dismouting, the very big vanning demand that satisfies of size after the dismantlement, the transportation of being convenient for, simple structure moreover, convenient operation.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural diagram of the first bracket assembly of the present invention.
Fig. 3 is a schematic structural diagram of the second bracket assembly of the present invention.
Fig. 4 is a schematic structural diagram of the third bracket assembly of the present invention.
Fig. 5 is a schematic structural diagram of a fourth bracket assembly according to the present invention.
Fig. 6 is a schematic structural diagram of a fifth bracket assembly according to the present invention.
The reference numerals include:
1-support frame 10-support component 11-bottom frame 12-inclined support frame 13-installation guide rail 14-hand lever 15-roller
2-first bracket assembly 21-first front bracket 22-first rear bracket
3-second bracket component 31-second front bracket 32-second rear bracket 33-auxiliary hook 34-support column 35-fastening ring
4-third bracket Assembly 41-third front cradle 42-third rear cradle
5-fourth bracket assembly 51-fourth front bracket 52-fourth rear bracket 53-auxiliary support rod
6-fifth bracket assembly 61-fifth front bracket 62-fifth rear bracket 63-auxiliary support post.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings.
As shown in figure 1, the helicopter engine combined bracket comprises a supporting frame 1, wherein a supporting component 10 is installed on the surface of the supporting frame 1 in a surface mounting mode, the supporting component 10 is installed on the surface of the supporting frame 1 in an adjustable mode, the supporting component 10 comprises a first bracket component 2, a second bracket component 3, a third bracket component 4, a fourth bracket component 5 and a fifth bracket component 6, the first bracket component 2, the second bracket component 3, the third bracket component 4, the fourth bracket component 5 and the fifth bracket component 6 are installed on the supporting frame 1 in a replaceable mode respectively, the supporting component 10 integrates five series of engine brackets and is installed on the supporting frame 1 integrally, the comprehensive performance is high, and can make things convenient for the field to salvage the use according to demand detachably dismouting, the very big vanning demand that satisfies of size after the dismantlement, the transportation of being convenient for, simple structure moreover, convenient operation.
Further refer to fig. 1-6, the support frame 1 includes two underframe 11, two underframe 11 mutually perpendicular set up and splice into T-shaped frame, and be provided with bracing frame 12 between support frame 1 and be used for the reinforcement, improve the steadiness of support frame 1, every underframe 11 surface is along its length direction shaping has installation guide rail 13, support assembly 10 is adjustable, the gomphosis in installation guide rail 13 of replaceability, hand lever 14 is installed to one of them base tip, support frame 1 bottom is provided with gyro wheel 15, can pull hand lever 14 and pull support frame 1 and slide in the bottom surface, improve conveying efficiency.
Further: the first bracket assembly 2 is a Z-8 series engine bracket, the first bracket assembly 2 comprises a first front bracket 21 and a first rear bracket 22, the number of the first front brackets 21 is at least two, the two first front brackets 21 are symmetrically arranged on one underframe 11, the first rear bracket 22 is arranged on the other underframe 11, the roller 15 at the bottom of the support frame 1 is firstly locked, the Z-8 series engine is arranged on the first front bracket 21 and the first rear bracket 22 to fix the Z-8 series engine, and the tops of the first front bracket 21 and the first rear bracket 22 are fixedly connected with the engine through pins.
Further: the second bracket component 3 is a Z-9 series engine bracket, the second bracket component 3 comprises a second front bracket 31 and a second rear bracket 32 which are coaxially arranged, auxiliary hooks 33 are respectively arranged on two sides of the second front bracket 31, the auxiliary hooks 33 are embedded on the mounting guide rail 13 through support pillars 34, the second front bracket 31 and the second rear bracket 32 are mounted on one of the base frames 11, the two auxiliary hooks 33 are mounted on the other base frame 11, the Z-9 engine special second bracket component 3 is placed at a proper position of the mounting guide rail 13 on the support frame 1 and fastened through bolts, wherein the second front bracket 31 and the second rear bracket 32 support the engine, a fastening ring 35 on the second rear bracket 32 assists in fastening the engine, the auxiliary hooks 33 penetrate through ear holes of the engine, and adjusting nuts tighten the hooks.
Further: the third bracket assembly 4 is a Z-10 series engine bracket, the third bracket assembly 4 comprises a third front bracket 41 and a third rear bracket 42 which are different in height, the number of the third front brackets 41 is at least two, two third front brackets 41 are simultaneously installed on one underframe 11, the third front bracket 41 is adjustably installed on the installation guide rail 13 through a support pillar 34, the third rear bracket 42 is installed on the other underframe 11, the third bracket assembly 4 special for the Z-10 engine is placed in a proper position of the installation guide rail 13 on the support frame 1 and is fastened through a bolt, the Z-10 engine is placed in a proper position and is connected through a pin, and the two third front brackets 41 and the third rear bracket 42 simultaneously support the engine.
Further: the fourth bracket assembly 5 is an M-171 series engine bracket, the fourth bracket assembly 5 comprises a fourth bracket assembly 5 including a fourth front bracket 51 and a fourth rear bracket 52 with different heights, the number of the fourth front brackets 51 is at least two, a forked auxiliary support rod 53 is formed on the top of the fourth front bracket 51, the two fourth front brackets 51 are simultaneously installed on one of the base frames 11, the fourth rear bracket 52 is installed on the other base frame 11, the M-171 engine-specific fourth bracket assembly 5 is placed on the proper position of the installation guide rail 13 on the support frame 1 and is fastened through bolts, and the forked angle of the auxiliary support rod 53 can be adjusted to adjust the bearing capacity of the fourth bracket assembly 5 on the engine.
Further: the fifth bracket assembly 6 is AN9B series engine bracket, the fifth bracket assembly 6 comprises a fifth bracket assembly 6 including a fifth front bracket 61 and a fifth rear bracket 62 with different heights, the number of the fifth front bracket 61 is at least two, a forked auxiliary support post 63 is formed on the top of the fifth front bracket 61, the two fifth front brackets 61 are simultaneously mounted on one of the chassis 11, the fifth rear bracket 62 is mounted on the other chassis 11, the fifth bracket assembly 6 special for AN9B engine is placed on a proper position of a mounting rail 13 on the support frame 1 and is fastened through bolts, the angle between the auxiliary support posts 63 on the fifth rear bracket 62 can be adjusted, the forked angle thereof is adjusted, and the engine is fixedly mounted on the fifth bracket assembly 6.
In conclusion, the present invention has the above-mentioned excellent characteristics, so that it can be used to enhance the effectiveness of the prior art and has practicability, and thus it is a product with practical value.
The above description is only for the preferred embodiment of the present invention, and for those skilled in the art, there are variations on the detailed description and the application scope according to the idea of the present invention, and the content of the description should not be construed as a limitation to the present invention.
Claims (7)
1. Helicopter engine combination bracket, including the support frame, its characterized in that: the supporting frame surface mounting has the supporting component, and the supporting component is installed on the supporting frame surface adjustably, and the supporting component includes first bracket component, second bracket component, third bracket component, fourth bracket component and fifth bracket component, and first bracket component, second bracket component, third bracket component, fourth bracket component and fifth bracket component are installed on the supporting frame replaceably respectively.
2. A helicopter engine assembling bracket according to claim 1, characterized in that: the support frame includes two chassis, and two chassis mutually perpendicular set up splices into T shape frame, and every chassis surface is followed its length direction shaping and is had the installation guide rail, and the embedding of supporting component adjustable, replaceability is in the installation guide rail, and the hand lever is installed to one of them base tip.
3. A helicopter engine assembling bracket according to claim 1, characterized in that: the first bracket component is a Z-8 series engine bracket and comprises at least two first front brackets and at least two first rear brackets, the two first front brackets are symmetrically arranged on one underframe, and the first rear brackets are arranged on the other underframe.
4. A helicopter engine assembling bracket according to claim 1, characterized in that: the second bracket component is a Z-9 series engine bracket and comprises a second front bracket and a second rear bracket which are coaxially arranged, auxiliary hooks are respectively arranged on two sides of the second front bracket, the second front bracket and the second rear bracket are installed on one of the underframe, and the two auxiliary hooks are installed on the other underframe.
5. A helicopter engine assembling bracket according to claim 1, characterized in that: the third bracket assembly is a Z-10 series engine bracket and comprises a third front bracket and a third rear bracket which are different in height, the number of the third front brackets is at least two, the two third front brackets are simultaneously installed on one underframe, and the third rear bracket is installed on the other underframe.
6. A helicopter engine assembling bracket according to claim 1, characterized in that: the fourth bracket component is an M-171 series engine bracket, the fourth bracket component comprises a fourth front bracket and a fourth rear bracket, the fourth front bracket comprises at least two front brackets, the top of the fourth front bracket is provided with a forked auxiliary supporting rod, the two fourth front brackets are simultaneously installed on one of the underframe, and the fourth rear bracket is installed on the other underframe.
7. A helicopter engine assembling bracket according to claim 1, characterized in that: the fifth bracket component is AN AN9B series engine bracket, the fifth bracket component comprises a fifth bracket component which comprises a fifth front bracket and a fifth rear bracket with different heights, the number of the fifth front bracket is at least two, the top of the fifth front bracket is formed with a forked auxiliary supporting column, the two fifth front brackets are simultaneously installed on one underframe, and the fifth rear bracket is installed on the other underframe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120359791.2U CN214729714U (en) | 2021-02-07 | 2021-02-07 | Helicopter engine combined bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120359791.2U CN214729714U (en) | 2021-02-07 | 2021-02-07 | Helicopter engine combined bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214729714U true CN214729714U (en) | 2021-11-16 |
Family
ID=78588420
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120359791.2U Active CN214729714U (en) | 2021-02-07 | 2021-02-07 | Helicopter engine combined bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214729714U (en) |
-
2021
- 2021-02-07 CN CN202120359791.2U patent/CN214729714U/en active Active
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