CN109606619A - A kind of cargo deck stringer posting structure - Google Patents
A kind of cargo deck stringer posting structure Download PDFInfo
- Publication number
- CN109606619A CN109606619A CN201811319521.8A CN201811319521A CN109606619A CN 109606619 A CN109606619 A CN 109606619A CN 201811319521 A CN201811319521 A CN 201811319521A CN 109606619 A CN109606619 A CN 109606619A
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- CN
- China
- Prior art keywords
- stringer
- cargo deck
- brace
- jointing
- deck stringer
- 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.)
- Pending
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- 230000002787 reinforcement Effects 0.000 abstract description 3
- 230000015572 biosynthetic process Effects 0.000 abstract description 2
- 238000005452 bending Methods 0.000 description 4
- 230000003014 reinforcing effect Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/18—Floors
- B64C1/20—Floors specially adapted for freight
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Joining Of Building Structures In Genera (AREA)
Abstract
The present invention relates to field of airplane structure, specially a kind of cargo deck stringer posting structure.It include: cargo deck stringer, brace, jointing, diffuser, frame and stringer；Cargo deck stringer one end is connect with frame, and intermediate position is hinged by bolt and brace, and the brace other end is hinged by bolt and jointing, and jointing facade is vertical with frame to be fixed, and bottom surface is fixed with diffuser, and the diffuser is fixed with stringer vertical elevation.The formation of triangle robust structure and brace only by the application of axial load so that cargo deck stringer reinforcement structure is simple, light-weight, good manufacturability, it is at low cost, be readily produced and assemble.
Description
Technical field
The present invention relates to field of airplane structure, specially a kind of cargo deck stringer posting structure.
Background technique
Cargo deck stringer receiving longitudinal loading ability is poor, need to disperse be transmitted on airframe structure by longitudinal loading.It is existing
The most longitudinal loading of aircraft is transmitted by sidewall paneling, and posting path is remote, low efficiency, and adopts mostly with lower wall panels connection reinforcing structure
With fixed connection, structure is complicated, weight weight.The present invention is directed to the longitudinal loading of cargo deck stringer is transmitted to underbelly
In structure.There are difference in height between cargo deck stringer and underbelly, load is transmitted in underbelly structure in parallel and is easy
Additional bending moment is generated, increases the complexity of underbelly structural bearing, and structural strengthening is made due to the increase of load
Weight increases.Therefore it is required that it is direct, high-efficient to make every effort to power transmission when load transmission, and it is simple and reliable for structure, additional bending moment is not transmitted, into
And influence the arrangement of original structure.
Summary of the invention
The present invention is directed to which the longitudinal loading of cargo deck stringer to be transmitted in fuselage stringer structure, while making every effort to posting road
Diameter is short, high-efficient.The characteristics of two power rod structures only pass axial force is taken full advantage of, both ensure that cargo deck stringer longitudinal loading
It can be transmitted on airframe structure, in turn avoid the generation of additional bending moment, simplify posting form and structure, alleviate aircaft configuration
Weight.
Technical solution
A kind of cargo deck stringer posting structure, include: cargo deck stringer [1], brace [2], jointing [3],
Diffuser [4], frame [5] and stringer [6]；Cargo deck stringer [1] one end is connect with frame [5], intermediate position by bolt with
Hingedly, brace [2] other end passes through bolt and jointing [3] hingedly to brace [2], jointing [3] facade and frame [5]
Vertical fixed, bottom surface and diffuser [4] are fixed, and the diffuser [4] is fixed with stringer [6] vertical elevation.
Brace [2] both ends are the aperture of monaural list.Structure is simple, guarantees axial load transmitting, the not production of additional bending moment
It is raw.
The jointing [3] is set as L-type Intermediate Gray stud.While guaranteeing to connect with brace [2], and also and frame
[4] and lower wall panels [5] are fixed.
The diffuser [4] is set as spill.Ensure load dispersion be transmitted to stringer [6] on.
Stud is arranged in the back side of the frame [5].Ensure brace [2] it is vertical it is discrete by stud pass through tension and compression bear.
Brace [2] and stringer [6] are formed by angle and should be less than 45 °.Ensure that cargo deck stringer [1] longitudinal loading is big
Decomposed is longitudinal Tensile or Compressive Loading of stringer [6].
Technical effect
Compared with traditional fixed connection structure, this invention simplifies cargo deck longitudinal beam structure and connection structure by
Power situation, so that cargo deck stringer, brace, jointing, diffuser, frame form a firm triangular structure.Goods
Cabin longitudinal floor beam longitudinal loading is transmitted on jointing by brace, is transmitted to stringer by diffuser, and brace axis
It is born to power in vertical component by mount structure.The formation of triangle robust structure and brace are only answered by axial load
With so that cargo deck stringer reinforcement structure is simple, light-weight, good manufacturability, it is at low cost, be readily produced and assemble.
Detailed description of the invention
Fig. 1 is the longitudinally reinforced structure chart of cargo deck stringer
Fig. 2 is the longitudinally reinforced structure rearview of cargo deck stringer
Wherein: 1- cargo deck stringer 2- brace 3- jointing 4- diffuser 5- frame 6- stringer
Specific embodiment
Cargo deck stringer reinforcement structure passes through cargo deck stringer [1], brace [2], jointing [3], diffuser
[4], frame [5], stringer [6] form firm triangular structure.
Brace [2] both ends and longitudinal floor beam [1], jointing [3] are subjected only to axial load by single bolted splice
Lotus；Jointing [3] is affixed with frame [4] diffuser [5], and diffuser [5] and stringer [6] are affixed.Frame [4] back side cloth
Reinforcing rib is set, the transmitting for vertical load.Cargo deck stringer [1] longitudinal loading is transmitted to connection by brace [2] and connects
It on head [3], is then passed on diffuser [4], is finally born by stringer [6], and brace [2] axial load is on vertical
Component is then born by the reinforcing rib in frame [4] structure.
Claims (6)
1. a kind of cargo deck stringer posting structure includes: cargo deck stringer [1], brace [2], jointing [3], expands
Loose mail [4], frame [5] and stringer [6]；It is characterized by: cargo deck stringer [1] one end is connect with frame [5], intermediate position is logical
Cross bolt and brace [2] hingedly, brace [2] other end passes through bolt and jointing [3] hingedly, and jointing [3] is vertical
Face is vertical with frame [5] fixed, and bottom surface and diffuser [4] are fixed, and the diffuser [4] is fixed with stringer [6] vertical elevation.
2. a kind of cargo deck stringer posting structure according to claim 1, it is characterised in that: brace [2] both ends are
Monaural list aperture.
3. a kind of cargo deck stringer posting structure according to claim 1, it is characterised in that: the jointing [3]
It is set as L-type Intermediate Gray stud.
4. a kind of cargo deck stringer posting structure according to claim 1, it is characterised in that: the diffuser [4] sets
It is set to spill.
5. a kind of cargo deck stringer posting structure according to claim 1, it is characterised in that: the back side of the frame [5]
Stud is set.
6. a kind of cargo deck stringer posting structure according to claim 1, it is characterised in that: brace [2] and stringer
[6] being formed by angle should be less than 45 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811319521.8A CN109606619A (en) | 2018-11-07 | 2018-11-07 | A kind of cargo deck stringer posting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811319521.8A CN109606619A (en) | 2018-11-07 | 2018-11-07 | A kind of cargo deck stringer posting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109606619A true CN109606619A (en) | 2019-04-12 |
Family
ID=66003125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811319521.8A Pending CN109606619A (en) | 2018-11-07 | 2018-11-07 | A kind of cargo deck stringer posting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109606619A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017188A (en) * | 2019-12-24 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft floor longeron course passes carries structure |
| CN111232181A (en) * | 2020-03-09 | 2020-06-05 | 中国商用飞机有限责任公司 | Load transfer mechanism for cargo hold of civil passenger plane |
| US20210237878A1 (en) * | 2018-04-23 | 2021-08-05 | Moose Manufacturing Llc | System and Method for Mounting Items to an Aircraft Floor |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101952167A (en) * | 2008-02-07 | 2011-01-19 | 空中客车运营有限公司 | Floor system for a fuselage section of an aircraft |
| CN105836155A (en) * | 2016-03-18 | 2016-08-10 | 中国飞机强度研究所 | Double-layer floor beam loading device for aircraft structural strength test |
| CN106672197A (en) * | 2016-12-26 | 2017-05-17 | 中国航空工业集团公司西安飞机设计研究所 | Cargo hold floor longitudinal beam and blocking wall connecting structure |
| US20180065728A1 (en) * | 2016-07-08 | 2018-03-08 | Creative Solutions, Inc. | Protective covers for use with aircraft cargo holds |
| CN207631469U (en) * | 2017-12-20 | 2018-07-20 | 成都正通航空设备有限责任公司 | A kind of narrow body aircraft cargo bay floor component |
-
2018
- 2018-11-07 CN CN201811319521.8A patent/CN109606619A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101952167A (en) * | 2008-02-07 | 2011-01-19 | 空中客车运营有限公司 | Floor system for a fuselage section of an aircraft |
| CN105836155A (en) * | 2016-03-18 | 2016-08-10 | 中国飞机强度研究所 | Double-layer floor beam loading device for aircraft structural strength test |
| US20180065728A1 (en) * | 2016-07-08 | 2018-03-08 | Creative Solutions, Inc. | Protective covers for use with aircraft cargo holds |
| CN106672197A (en) * | 2016-12-26 | 2017-05-17 | 中国航空工业集团公司西安飞机设计研究所 | Cargo hold floor longitudinal beam and blocking wall connecting structure |
| CN207631469U (en) * | 2017-12-20 | 2018-07-20 | 成都正通航空设备有限责任公司 | A kind of narrow body aircraft cargo bay floor component |
Non-Patent Citations (2)
| Title |
|---|
| 孙洁琼: "民用飞机客舱地板横梁结构研究", 《民用飞机设计与研究》 * |
| 张卫文等: "飞机地板常用结构设计与传力分析", 《中国科技信息》 * |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210237878A1 (en) * | 2018-04-23 | 2021-08-05 | Moose Manufacturing Llc | System and Method for Mounting Items to an Aircraft Floor |
| US11772796B2 (en) * | 2018-04-23 | 2023-10-03 | Moose Manufacturing Llc | System and method for mounting items to an aircraft floor |
| CN111017188A (en) * | 2019-12-24 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft floor longeron course passes carries structure |
| CN111232181A (en) * | 2020-03-09 | 2020-06-05 | 中国商用飞机有限责任公司 | Load transfer mechanism for cargo hold of civil passenger plane |
| CN111232181B (en) * | 2020-03-09 | 2021-09-28 | 中国商用飞机有限责任公司 | Load transfer mechanism for cargo hold of civil passenger plane |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190412 |