CN207454465U - A kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib - Google Patents
A kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib Download PDFInfo
- Publication number
- CN207454465U CN207454465U CN201721276745.6U CN201721276745U CN207454465U CN 207454465 U CN207454465 U CN 207454465U CN 201721276745 U CN201721276745 U CN 201721276745U CN 207454465 U CN207454465 U CN 207454465U
- Authority
- CN
- China
- Prior art keywords
- reinforcing rib
- multiple material
- limit chamber
- bonding tool
- aircraft machine
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including the limit chamber being fixed on tooling base and multiple reinforcing rib pressing devices arranged on limit chamber periphery；The reinforcing rib pressing device includes housing screw, the compression beam perpendicular to the supporting rack of pedestal and on supporting rack, and the compression beam is equipped with multiple through holes perpendicular to the limit chamber, and the housing screw is connected with the through hole whorl.It is accurate that the positioning of the utility model reinforcing rib facilitates, and shaping pressurization is reliable, and it is good to be glued forming quality for material panel surfaces and reinforcing rib again.
Description
Technical field
The utility model is related to frock technical fields, particularly the bonding work of a kind of multiple material of aircraft machine beam and reinforcing rib
Dress.
Background technology
Multiple material is accounted for its height than performances such as strong, Gao Bimo, heat-resisting resistance to ablation, light and conductive and heat-conductives in field of aerospace
There is special status, multiple material is different from manufacturing process with its structure, shows different performances.As can not in aerospace field
Or scarce critical function section bar material, multiple the comprehensive of material performance, accurate characterization are to its development and production and using significant.
At present to answering the shaping of material siding with reinforcing rib, traditional beam is such as used, covering is each separately formed to be then glued,
Interfacial effect is also easy to produce being glued face, easy degumming, influences flight safety when being subject to big load, it is therefore desirable to multiple material siding
Monolithic molding cure.
Utility model content
For solve problems of the prior art, the purpose of this utility model be to provide a kind of multiple material of aircraft machine beam with
The bonding tool of reinforcing rib, it is accurate that the positioning of this frock reinforcing rib facilitates, and solves multiple material and reinforcing rib siding monolithic molding process
In, reinforcing rib shapes pressurization problem, improves the bonding effect of multiple material and reinforcing rib.
To achieve the above object, the technical solution adopted in the utility model is：The multiple material and reinforcing rib of a kind of aircraft machine beam
Bonding tool, compress dress including the limit chamber that is fixed on tooling base and multiple reinforcing ribs arranged on limit chamber periphery
It puts；The reinforcing rib pressing device includes housing screw, the compression beam perpendicular to the supporting rack of pedestal and on supporting rack, institute
Compression beam is stated equipped with multiple through holes perpendicular to the limit chamber, the housing screw is connected with the through hole whorl.
When installing reinforcing rib additional to the multiple material of aircraft machine beam, multiple material is sleeved on to the periphery of limit chamber, it would be desirable to bond with multiple material
Reinforcing rib be placed in the periphery of multiple material, specifically, aperture corresponding with housing screw position, assistant reinforcement can be set on reinforcing rib
The positioning of muscle makes the positioning of reinforcing rib facilitate accurate, is then applied to adhesive on the contact surface of multiple material and reinforcing rib, rotation pressure
Tight screw makes reinforcing rib sufficiently be contacted with multiple material；When multiple reinforcing rib pressing devices that reinforcing rib is limited chamber periphery are abundant
After fixation, the multiple material of aircraft machine beam is placed in together with the bonding tool of reinforcing rib and multiple material and reinforcing rib in vacuum tank and is carried out
Vacuum bonding.It is accurate that the positioning of the utility model reinforcing rib facilitates, and shaping pressurization is reliable, multiple material panel surfaces and reinforcing rib be glued into
Form quality amount is good.
As further improvement of the utility model, the compression beam includes horizontal beam and composite beam, the horizontal beam water
Flat to be arranged on support frame as described above, the composite beam is combined for a horizontal segment and the vertical section arranged on horizontal segment one end, described
The horizontal segment of composite beam is arranged on support frame as described above.Horizontal beam and composite beam are set, allow the reinforcement of multiple material and various shapes
Muscle bonds, and makes the multiple material intensity bigger after bonding.
As further improvement of the utility model, multiple /Vs are equipped with positioned at the periphery of limit chamber bottom on the pedestal
Block.Will answer material be sleeved on limit chamber periphery and reinforcing rib be fixed when, limited block can aid in limiting the position of multiple material, make operation
It is more convenient.
As further improvement of the utility model, the reinforcing rib pressing device is 6-8.Multiple reinforcing rib pressures are set
Tight device enables multiple material panel surfaces to set multiple reinforcing ribs, makes multiple material intensity bigger.
As further improvement of the utility model, the multiple material of the aircraft machine beam and the bonding tool of reinforcing rib are steel
Matter.Using steel material, intensity is big, and service life is long.
The beneficial effects of the utility model are：
1st, the positioning of the utility model reinforcing rib facilitates accurate, and shaping pressurization is reliable, and multiple material panel surfaces and reinforcing rib are glued
Forming quality is good.
The 2nd, horizontal beam and composite beam are set, allow the reinforcing rib bonding of multiple material and various shapes, make the multiple material after bonding
Intensity bigger.
3rd, multiple limited blocks are set positioned at the periphery of limit chamber bottom on pedestal, are sleeved on limit chamber periphery material will be answered and add
When strengthening tendons is fixed, limited block can aid in limiting the position of multiple material, make operation more convenient.
The 4th, multiple reinforcing rib pressing devices are set, enable multiple material panel surfaces that multiple reinforcing ribs are set, make multiple material intensity more
Greatly.
5th, the bonding tool of the multiple material of the aircraft machine beam and reinforcing rib uses steel material, and intensity is big, and service life is long.
Description of the drawings
Fig. 1 is the structure diagram of the utility model embodiment；
Reference numeral：
10th, pedestal, 20, limit chamber, 30, reinforcing rib pressing device；
11st, limited block, 31, housing screw, 32, supporting rack, 33, compression beam, 33a, horizontal beam, 33b, composite beam, 34 is logical
Hole.
Specific embodiment
The embodiment of the utility model is described in detail below in conjunction with the accompanying drawings.
Embodiment 1
As shown in Figure 1, a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including being fixed at tooling base 10
On limit chamber 20 and multiple reinforcing rib pressing devices 30 arranged on the periphery of limit chamber 20；The reinforcing rib pressing device 30 includes
Housing screw 31, the compression beam 33 perpendicular to the supporting rack 32 of pedestal 10 and on supporting rack 32 are set in the compression beam 33
There are multiple through holes 34 perpendicular to the limit chamber 20, the housing screw 31 is threadedly coupled with the through hole 34.
Embodiment 2
As shown in Figure 1, a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including being fixed at tooling base 10
On limit chamber 20 and multiple reinforcing rib pressing devices 30 arranged on the periphery of limit chamber 20；The reinforcing rib pressing device 30 includes
Housing screw 31, the compression beam 33 perpendicular to the supporting rack 32 of pedestal 10 and on supporting rack 32 are set in the compression beam 33
There are multiple through holes 34 perpendicular to the limit chamber 20, the housing screw 31 is threadedly coupled with the through hole 34.
The compression beam 33 includes horizontal beam 33a and composite beam 33b, the horizontal beam 33a is horizontal arranged on support frame as described above
On 32, the composite beam 33b is combined for a horizontal segment and the vertical section arranged on horizontal segment one end, the composite beam 33b's
Horizontal segment is arranged on support frame as described above 32.
Embodiment 3
As shown in Figure 1, a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including being fixed at tooling base 10
On limit chamber 20 and multiple reinforcing rib pressing devices 30 arranged on the periphery of limit chamber 20；The reinforcing rib pressing device 30 includes
Housing screw 31, the compression beam 33 perpendicular to the supporting rack 32 of pedestal 10 and on supporting rack 32 are set in the compression beam 33
There are multiple through holes 34 perpendicular to the limit chamber 20, the housing screw 31 is threadedly coupled with the through hole 34.
The compression beam 33 includes horizontal beam 33a and composite beam 33b, the horizontal beam 33a is horizontal arranged on support frame as described above
On 32, the composite beam 33b is combined for a horizontal segment and the vertical section arranged on horizontal segment one end, the composite beam 33b's
Horizontal segment is arranged on support frame as described above 32.
On the pedestal 10 multiple limited blocks 11 are equipped with positioned at the periphery of 20 bottom of limit chamber.
Embodiment 4
As shown in Figure 1, a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including being fixed at tooling base 10
On limit chamber 20 and multiple reinforcing rib pressing devices 30 arranged on the periphery of limit chamber 20；The reinforcing rib pressing device 30 includes
Housing screw 31, the compression beam 33 perpendicular to the supporting rack 32 of pedestal 10 and on supporting rack 32 are set in the compression beam 33
There are multiple through holes 34 perpendicular to the limit chamber 20, the housing screw 31 is threadedly coupled with the through hole 34.
The compression beam 33 includes horizontal beam 33a and composite beam 33b, the horizontal beam 33a is horizontal arranged on support frame as described above
On 32, the composite beam 33b is combined for a horizontal segment and the vertical section arranged on horizontal segment one end, the composite beam 33b's
Horizontal segment is arranged on support frame as described above 32.
On the pedestal 10 multiple limited blocks 11 are equipped with positioned at the periphery of 20 bottom of limit chamber.
The reinforcing rib pressing device 30 is 7.
Embodiment 5
The present embodiment is substantially the same manner as Example 4, is 6 difference lies in the reinforcing rib pressing device 30.
Embodiment 6
The present embodiment is substantially the same manner as Example 4, is 8 difference lies in the reinforcing rib pressing device 30.
Embodiment 7
As shown in Figure 1, a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, including being fixed at tooling base 10
On limit chamber 20 and multiple reinforcing rib pressing devices 30 arranged on the periphery of limit chamber 20；The reinforcing rib pressing device 30 includes
Housing screw 31, the compression beam 33 perpendicular to the supporting rack 32 of pedestal 10 and on supporting rack 32 are set in the compression beam 33
There are multiple through holes 34 perpendicular to the limit chamber 20, the housing screw 31 is threadedly coupled with the through hole 34.
The compression beam 33 includes horizontal beam 33a and composite beam 33b, the horizontal beam 33a is horizontal arranged on support frame as described above
On 32, the composite beam 33b is combined for a horizontal segment and the vertical section arranged on horizontal segment one end, the composite beam 33b's
Horizontal segment is arranged on support frame as described above 32.
On the pedestal 10 multiple limited blocks 11 are equipped with positioned at the periphery of 20 bottom of limit chamber.
The reinforcing rib pressing device 30 is 7.
The multiple material of the aircraft machine beam and the bonding tool of reinforcing rib are steel material.
Embodiment described above only expresses specific embodiment of the present utility model, and description is more specific and detailed,
But it should not be interpreted as limiting the scope of the present invention.It should be pointed out that for the common of this field
For technical staff, without departing from the concept of the premise utility, various modifications and improvements can be made, these all belong to
In the scope of protection of the utility model.
Claims (5)
1. a kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib, which is characterized in that including being fixed on tooling base
Limit chamber and multiple reinforcing rib pressing devices arranged on limit chamber periphery；The reinforcing rib pressing device include housing screw,
Compression beam perpendicular to the supporting rack of pedestal and on supporting rack, the compression beam are equipped with multiple perpendicular to the limit chamber
Through hole, the housing screw is connected with the through hole whorl.
2. the multiple material of aircraft machine beam according to claim 1 and the bonding tool of reinforcing rib, which is characterized in that the compression
Beam includes horizontal beam and composite beam, and the horizontal beam is horizontal to be arranged on support frame as described above, and the composite beam is a horizontal segment and sets
Vertical section in horizontal segment one end is combined, and the horizontal segment of the composite beam is arranged on support frame as described above.
3. the multiple material of aircraft machine beam according to claim 1 and the bonding tool of reinforcing rib, which is characterized in that the pedestal
It is upper to be equipped with multiple limited blocks positioned at the periphery of limit chamber bottom.
4. the multiple material of aircraft machine beam according to claim 1 and the bonding tool of reinforcing rib, which is characterized in that the reinforcement
Muscle pressing device is 6-8.
5. the multiple material of aircraft machine beam according to claim 1 and the bonding tool of reinforcing rib, which is characterized in that the aircraft machine
The multiple material of beam and the bonding tool of reinforcing rib are steel material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721276745.6U CN207454465U (en) | 2017-09-30 | 2017-09-30 | A kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721276745.6U CN207454465U (en) | 2017-09-30 | 2017-09-30 | A kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207454465U true CN207454465U (en) | 2018-06-05 |
Family
ID=62250188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721276745.6U Expired - Fee Related CN207454465U (en) | 2017-09-30 | 2017-09-30 | A kind of multiple material of aircraft machine beam and the bonding tool of reinforcing rib |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207454465U (en) |
-
2017
- 2017-09-30 CN CN201721276745.6U patent/CN207454465U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180605 Termination date: 20200930 |