CN109436372A - A kind of box section towards different loads level is to connected components, interconnection method and application - Google Patents
A kind of box section towards different loads level is to connected components, interconnection method and application Download PDFInfo
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- CN109436372A CN109436372A CN201811426498.2A CN201811426498A CN109436372A CN 109436372 A CN109436372 A CN 109436372A CN 201811426498 A CN201811426498 A CN 201811426498A CN 109436372 A CN109436372 A CN 109436372A
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- box section
- box
- docking
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- siding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
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- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The invention belongs to airframe experimental design fields, and in particular to a kind of box section towards different loads level is to connected components, interconnection method and application；The box section interconnection method is to be docked the siding of ontology and bogusware, spar partial cross-section using interfacing part connection self-box section and bogusware box section, and spar docking uses double shear form, and siding docking inside is connected using cornual plate.Box section interconnection method of the present invention assembles simply, is convenient for operation, in addition, it is more stable, safe when can make the test of box section to use double shear structure in docking, and reduces the risk of Failure Analysis of Composite Materials.
Description
Technical field
The invention belongs to airframe experimental design fields, and in particular to a kind of box section docking towards different loads level
Component, interconnection method and application.
Background technique
Currently, composite material application on civil aircraft need to pass through comprehensive building block system verification experimental verification, including it is typical box section grade, big
Type section grade test etc., such testpieces often design a bogusware box section, the equivalent application of external load on the outside of examination box section
In the bogusware box section, to guarantee the authenticity of examination box section borne load.Bogusware box section structure is generally divided into two kinds: first is that
Examination section composite material parts are directly extended as bogusware box section；Another kind is one can section of manufacture, even using machinery
Form is connect to dock with examination section.The former reduces assembly difficulty, but multiple material die cost, material cost are higher, and bogusware
Box section must be designed sufficiently strong, and composite Materials Design manufacture difficulty is larger；Cost is relatively low by the latter, but assembles complicated, test
Part integrally increases weight larger.By taking the test of the typical box section of composite wing as an example, test objective is verifying wing root structure
Bearing capacity, bogusware box section bear equivalent load it is higher, be typically designed as can section, docked with multiple material box section.
For existing box section testpieces docking concept as shown in Figure of description 1, Fig. 2 and Fig. 3, testpieces examines box section and bogusware
Box section is connected using interior outside jointing strip plate, tandem docking side plate, carries out whole docking to the rib position close to wing tip in exhibition.
Siding is mechanically connected using interior outside jointing strip plate, wherein interior docking band plate design overlap joint slot is last to connect examination box segment length purlin
End；Front and back spar carries out simple shear connection using opposed side panel；Rib and siding are mechanically connected at docking.Examine box section siding, the wing
Liang Jun is truncated at rib section and connect with bogusware box section；As shown in figure 3, testpieces two sides are clamped, apply among box section and carry
Lotus.For bogusware box section without applying additional equivalent load, docking area load level is relatively low.And for similar examination wing root area
Load-transfer mechanism on the outside of box section to bogusware box section, docking area need to be born load-carrying water by the wing-box cantilever design testpieces of structure
It puts down relatively high.Existing docking design is unsatisfactory for big load test requirements document.It is specific as follows:
1) box section docking area siding, spar dock at same rib section, and stiffness variation is excessive, and stress is concentrated tight at section
Weight；
2) spar docking uses simple shear form, and in the case where bearing larger shear loads, the type of attachment is on the weak side；
3) siding uses band card slot type monoblock type to dock, and assembles location difficulty, under big load effect, compatibility of deformation is difficult.
Summary of the invention
To solve the above problems, the present invention proposes a kind of box section towards different loads level to connected components, interconnection method
And application；For the box section interconnection method when box section is docked, siding, the docking of spar partial cross-section, spar docking use double shear form,
Siding docking inside uses piecemeal corner strip type connection scheme, and this method assembly is simple, and it is horizontal especially to can be adapted for different loads
It is the box section test of big load level, reduces assembly difficulty and empirical risk.
The present invention is achieved by the following technical solutions:
A kind of box section towards different loads level to connected components, it is described to connected components for different loads in airframe
Horizontal box section tests field, described to include: to connected components
Several sectional type angle boxes for being used to connect adjacent docking stringer；
One with the inside and outside band plate for realizing double shear structure of several sectional type angle boxes；
Several cornual plates for connecting inside self-box section spar and bogusware box section spar；And
Several lateral angle boxes with the inside and outside realization double shear structure of the cornual plate.
Further, the sectional type angle angle He WeiUXing box.
Further, the material of U-shaped angle box is the metal materials such as aluminium alloy, steel, titanium alloy.
Further, the material of the band plate is the metal materials such as aluminium alloy, steel, titanium alloy.
Further, the material of the covering is composite material or aluminium alloy.
Further, the material of the cornual plate is the metal materials such as aluminium alloy, steel, titanium alloy.
Further, the metal materials such as aluminium alloy, steel, titanium alloy of the lateral angle box.
Further, the docking stringer be self-box segment length purlin and bogusware box segment length purlin docking after obtain.
Further, it is respectively provided on sectional type angle box, band plate, cornual plate and lateral angle box affixed convenient for screw accordingly
Through-hole.
A kind of box section interconnection method towards different loads level, the box section interconnection method are using described to connected components
Self-box section and bogusware box section are connected, the siding of ontology and bogusware, spar partial cross-section are docked, spar docking uses double shear shape
Formula, siding docking inside are connected using cornual plate.
Further, the box section interconnection method specifically comprises the following steps:
S1, self-box section siding dock in advance with bogusware box section siding；
S2, self-box section siding stringer of docking adjacent with bogusware box section siding docking area use internal sectional type angle box,
And it is affixed to cooperate the band plate in outside to carry out, the band plate and sectional type angle box realize double shear structure；
S3, self-box section spar and bogusware box section spar dock at rib, and internal jointing and lateral angle box make the wing
Web realizes double shear structure；It is connected inside spar flange using cornual plate, it is external to be shared with the band plate, it is same to realize double shear knot
Structure.
Further, self-box section siding described in the step S2 and bogusware box section siding docking area use internal piecemeal
The specific connection method of formula angle box is as follows:
After the self-box section siding and bogusware box section siding docking, at this point, the stringer of two box sections is also accordingly docked
Docking stringer is formed, then is connected the inside of the adjacent long case bay of docking using sectional type angle box.
Further, the docking stringer edge strip and web are arranged fastener, reduce Assembly part quantity, reduce fastening
Part arrangement difficulty.
Further, the double shear structure refers to three part connections, and there are two contact surfaces, is two for bolt
Shear surface；The box section interconnection method of the invention is for the horizontal box section test of big load, in box section docking location, loaded feelings
Condition is complicated, load is larger, and it is more stable when testing, safe to make box section using double shear structure, and reduces the wind of Failure Analysis of Composite Materials
Danger.
Further, it is known in the art that having covering, similarly, the bogusware box section on the outside of the stringer of the self-box section
Stringer on the outside of with one layer of covering.
Another object of the present invention is to provide a kind of box section interconnection methods towards different loads level to be applied to difference
The box section test of load level especially big load level reduces assembly difficulty and empirical risk.
Of the invention at least has following advantageous effects:
(1) a kind of box section interconnection method towards different loads level of the invention can be made using double shear structure when docking
Box section is more stable when testing, safe, and reduces the risk of Failure Analysis of Composite Materials.
(2) a kind of box section interconnection method assembly towards different loads level of the invention is simple, convenient for operation.
(3) a kind of box section docking area siding of box section interconnection method towards different loads level of the invention, spar be not
It is docked at same rib section, stiffness variation is small, and stress disperses at section.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of existing box section testpieces interconnection method changeover portion.
Fig. 2 is the structural schematic diagram of existing box section testpieces interconnection method testpieces connecting pin.
Fig. 3 is the scheme of installation of existing box section testpieces interconnection method testpieces changeover portion.
Fig. 4 is box section docking area position view in the embodiment of the present invention.
Fig. 5 is docking area structural schematic diagram in the embodiment of the present invention.
Fig. 6 is siding docking structure schematic diagram in the embodiment of the present invention.
Fig. 7 is central spar of embodiment of the present invention docking structure schematic diagram.
Fig. 8 is lateral angle box structure schematic diagram in the embodiment of the present invention.
Description of symbols: 1- wall, 2- self-box section, 3- bogusware box section, the docking area 4-, 5- self-box section siding, 6-
Bogusware box section siding, 7- bogusware box section spar, 8- self-box section spar, 9- self-box segment length purlin, 10- bogusware box segment length purlin, 11-
At rib, 12- covering, 13- band plate, the self-box segment length purlin 14- and bogusware box segment length purlin docking, 15-U shape angle box, 16- cornual plate,
Connector inside 17-, 18- lateral angle box.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to embodiments and specification
The present invention is explained in further detail in attached drawing.It should be appreciated that specific embodiment described herein is used only for explaining this
Invention, is not intended to limit the present invention.
On the contrary, the present invention covers any substitution done on the essence and scope of the present invention being defined by the claims, repairs
Change, equivalent method and scheme.Further, in order to make the public have a better understanding the present invention, below to of the invention thin
It is detailed to describe some specific detail sections in section description.Part without these details for a person skilled in the art
The present invention can also be understood completely in description.
Embodiment 1
The present embodiment propose a kind of box section towards different loads level to connected components, it is described right as shown in Fig. 4~Fig. 8
Connected components test field for the box section of different loads level in airframe, described to include: to connected components
Several sectional type angle boxes for being used to connect adjacent docking stringer；
One with the inside and outside band plate 13 for realizing double shear structure of several sectional type angle boxes；
Several cornual plates 16 for connecting inside self-box section spar 8 and bogusware box section spar 7；And
Several lateral angle boxes 18 with the inside and outside realization double shear structure of the cornual plate 16.
The sectional type angle angle He WeiUXing box 15.
The docking stringer be self-box segment length purlin 9 and bogusware box segment length purlin docking after obtain.
It is respectively provided on sectional type angle box, band plate 13, cornual plate 16 and lateral angle box 18 affixed convenient for screw accordingly
Through-hole.
The present embodiment also proposes that a kind of box section interconnection method towards different loads level, the box section interconnection method are specific
Include the following steps:
S1, self-box section siding 5 dock in advance with bogusware box section siding 6；
S2, the stringer of docking adjacent with 6 docking area 4 of bogusware box section siding of self-box section siding 5 is using internal sectional type angle
Box, and it is affixed to cooperate the band plate 13 in outside to carry out, the band plate 13 realizes double shear structure with sectional type angle box；
S3, self-box section spar 8 and bogusware box section spar 7 dock at rib 11, internal jointing and lateral angle box
18 make spar web realize double shear structure；It is connected inside spar flange using cornual plate 16, it is external to be shared with the band plate 13, equally
Realize double shear structure.
Self-box section siding 5 described in the step S2 and 6 docking area 4 of bogusware box section siding use internal sectional type angle box
Specific connection method it is as follows:
After the self-box section siding 5 and the bogusware box section siding 6 docking, at this point, the stringer of two box sections is also mutually coped with
It connects to form docking stringer, then is connected the inside of the adjacent long case bay of docking using sectional type angle box.
The double shear structure refers to three part connections, and there are two contact surfaces, is two shear surfaces for bolt；This
The box section interconnection method of invention is for the horizontal box section test of big load, and in box section docking location, loading conditions are complicated, carry
Lotus is larger, and it is more stable when testing, safe to make box section using double shear structure, and reduces the risk of Failure Analysis of Composite Materials.
A kind of box section interconnection method towards different loads level of the present embodiment can make box using double shear structure when docking
More stable, safety when section test, and reduce the risk of Failure Analysis of Composite Materials.
Box section interconnection method assembly is simple, convenient for operation.
In addition, box section docking area siding, spar dock not at same rib section, stiffness variation is small, stress point at section
It dissipates.
Embodiment 2
The present embodiment provides a kind of application of the box section interconnection method towards different loads level as described in Example 1,
The box section interconnection method is applied to the box section test of different loads level especially big load level, reduces assembly difficulty and examination
Test risk.
Claims (9)
1. a kind of box section towards different loads level is to connected components, described to be used for different loads water in airframe to connected components
Flat box section tests field, which is characterized in that described to include: to connected components
Several sectional type angle boxes for being used to connect adjacent docking stringer；
One with the inside and outside band plate for realizing double shear structure of several sectional type angle boxes；
Several cornual plates for connecting inside self-box section spar and bogusware box section spar；And
Several lateral angle boxes with the inside and outside realization double shear structure of the cornual plate.
2. a kind of box section towards different loads level according to claim 1 is to connected components, which is characterized in that described point
The block formula angle angle He WeiUXing box.
3. a kind of box section towards different loads level according to claim 1 is to connected components, which is characterized in that described right
Spreading purlin be self-box segment length purlin and bogusware box segment length purlin docking after obtain.
4. a kind of box section towards different loads level according to claim 1 is to connected components, which is characterized in that described point
The corresponding through-hole affixed convenient for screw is respectively provided on block formula angle box, band plate, cornual plate and lateral angle box.
5. a kind of box section interconnection method towards different loads level, which is characterized in that the box section interconnection method is using such as
Any one of Claims 1 to 4 is described to connect self-box section and bogusware box section to connected components, by the siding of ontology and bogusware, spar
Partial cross-section docking, spar docking use double shear form, and siding docking inside is connected using cornual plate.
6. a kind of box section interconnection method towards different loads level according to claim 5, which is characterized in that the box
Section interconnection method specifically comprises the following steps:
S1, self-box section siding dock in advance with bogusware box section siding；
S2, self-box section siding stringer of docking adjacent with bogusware box section siding docking area are matched using internal sectional type angle box
The band plate for closing outside carries out affixed, the band plate and sectional type angle box realization double shear structure；
S3, self-box section spar and bogusware box section spar dock at rib, and internal jointing and lateral angle box make spar web
Plate realizes double shear structure；It is connected inside spar flange using cornual plate, it is external to be shared with the band plate, it is same to realize double shear structure.
7. a kind of box section interconnection method towards different loads level according to claim 6, which is characterized in that the step
Self-box section siding described in rapid S2 and bogusware box section siding docking area use the specific connection method of internal sectional type angle box such as
Under:
After the self-box section siding and bogusware box section siding docking, at this point, also accordingly docking is formed the stringer of two box sections
Stringer is docked, then is connected the inside of the adjacent long case bay of docking using sectional type angle box.
8. a kind of box section interconnection method towards different loads level according to claim 7, which is characterized in that described right
Spreading purlin edge strip and web are arranged fastener, and Assembly part quantity is reduced, and are reduced fastener and are arranged difficulty.
9. being applied to not according to a kind of described in any item box section interconnection methods towards different loads level of claim 5~8
With the test of box section, reduction assembly difficulty and the empirical risk of load level especially big load level.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811426498.2A CN109436372A (en) | 2018-11-27 | 2018-11-27 | A kind of box section towards different loads level is to connected components, interconnection method and application |
| PCT/CN2018/120273 WO2020107530A1 (en) | 2018-11-27 | 2018-12-11 | Box section docking assembly and docking method and application therefor for different load levels |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811426498.2A CN109436372A (en) | 2018-11-27 | 2018-11-27 | A kind of box section towards different loads level is to connected components, interconnection method and application |
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| Publication Number | Publication Date |
|---|---|
| CN109436372A true CN109436372A (en) | 2019-03-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811426498.2A Pending CN109436372A (en) | 2018-11-27 | 2018-11-27 | A kind of box section towards different loads level is to connected components, interconnection method and application |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN109436372A (en) |
| WO (1) | WO2020107530A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406657A (en) * | 2019-07-31 | 2019-11-05 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Civil aircraft wing wainscot root joint angle box, connection structure and wing |
| CN110501467A (en) * | 2019-09-19 | 2019-11-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of connection structure of wing box specimen of plane |
| CN111003209A (en) * | 2019-12-26 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | Large-scale empennage deicing wind tunnel test device and method |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL221317A (en) * | 2012-08-06 | 2016-11-30 | Yochanan Giat | Ergonomic strategy and system for cast construction |
| CN205642963U (en) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | Combined material box section testpieces changeover portion |
| CN205633010U (en) * | 2016-05-16 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | Wing adds muscle box section testpieces |
| CN106314759A (en) * | 2016-09-06 | 2017-01-11 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Spar connecting structure of aircraft wing |
| CN206945287U (en) * | 2017-08-01 | 2018-01-30 | 中国航空工业集团公司西安飞机设计研究所 | A kind of joint test part structure for being used to examine rudder face metal joint |
-
2018
- 2018-11-27 CN CN201811426498.2A patent/CN109436372A/en active Pending
- 2018-12-11 WO PCT/CN2018/120273 patent/WO2020107530A1/en active Application Filing
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406657A (en) * | 2019-07-31 | 2019-11-05 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Civil aircraft wing wainscot root joint angle box, connection structure and wing |
| CN110406657B (en) * | 2019-07-31 | 2021-06-01 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Civil aircraft wing upper wall plate root connecting corner box, connecting structure and wing |
| CN110501467A (en) * | 2019-09-19 | 2019-11-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of connection structure of wing box specimen of plane |
| CN111003209A (en) * | 2019-12-26 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | Large-scale empennage deicing wind tunnel test device and method |
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| Publication number | Publication date |
|---|---|
| WO2020107530A1 (en) | 2020-06-04 |
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