CN103991649A - Folding transportation bracket for large fuselage part section - Google Patents
Folding transportation bracket for large fuselage part section Download PDFInfo
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- CN103991649A CN103991649A CN201410259923.9A CN201410259923A CN103991649A CN 103991649 A CN103991649 A CN 103991649A CN 201410259923 A CN201410259923 A CN 201410259923A CN 103991649 A CN103991649 A CN 103991649A
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Abstract
The invention provides a folding transportation bracket for a large fuselage part section. The overall folding transportation bracket is of a basketstructure. End corner guard bar stand columns are detachably connected to main beams. A front protection surface and a rear protection surface are formed by connecting end head transverse handrails to the end corner guard bar stand columns in a detachable mode. A left protection surface and a right protection surface are formed by connecting side protection handrails to the end corner guard bar stand columns in a detachable mode. Barrel section supporting wood pallets are fixed between the corresponding front ends of the main beams and between the corresponding rear ends of the main beams. A barrel section fastening strap is arranged above each barrel section supporting wood pallet and used for fixing a fuselage. A turnable staking pillar, an undercarriage hinge point locator and lifting arms are fixed to each main beam. A keel beam fixing chain located between the two main beams is connected with an adapter plate on a keel beam of the fuselage. According to the folding transportation bracket for the large fuselage part section, the folding mode is adopted, the space occupied by the bracket inside a container is reduced, the transportation cost of the fuselage part section of a plane is reduced, and the time for disassembling and boxing the folding transportation bracket and the time for restoring the usage of the folding transportation bracket are shortened.
Description
Technical field
The present invention relates to the collapsible pallet for transporting of a kind of large-scale main body section section, belong to airframe transportation engineering technical field.
Background technology
Concerning planemaker, the control of large aircraft main body section section traffic cost is an important content, the pallet for transporting using for main body section section transportation can be also generally the instrument of super large, and traditional pallet for transporting all adopts entirety to backhaul, take the position of a freight container to I haven't seen you for ages, when pallet for transporting is larger, need the case position taking will be more, therefore make to backhaul expense also larger.
Summary of the invention
For above deficiency, the invention provides the collapsible pallet for transporting of a kind of large-scale main body section section, adopt collapsible mode, reduce to take up room, reduce traffic cost.
Technical scheme of the present invention: the collapsible pallet for transporting of large-scale main body section section, entirety is " basket " formula structure, its bottom is provided with two girders along fore-and-aft direction is parallel, between two girders, be connected with carrying tankette fagging, and carrying tankette fagging is positioned at two ends before and after girder, be separately installed with end angle fence upright in four corners of " basket " formula structure, end angle fence upright and girder removably connect, former and later two protection faces of " basket " formula structure are by adopting the formation that removably connects of termination horizontal bar bar and end angle fence upright, two of the left and right protection face of " basket " formula structure is by adopting the formation that removably connects of side rail bar and end angle fence upright, between side rail bar and girder, be distributed with the guardrail strut and the guardrail pole that connect for strengthening, before and after girder, between corresponding two ends, be fixed with bucket section brace supporting plate, above bucket section brace supporting plate, be provided with the bucket section fastening straps for fixed main body, on girder, be fixed with a fuselage lifting pillar, on a fuselage lifting pillar, be provided with a lifting fastening straps, on girder, be fixed with the turnover post that stacks, alighting gear hinge steady arm and lifting arm, lifting arm is fixedly connected with girder by bolt and lifting arm offside guard rail rod plays certain supporting role, be connected with the keysets on fuselage keel bar at the fixing chain of the keel bar between two girders, the longitudinal travel of restriction fuselage bucket section.
The side, two of left and right of described " basket " formula structure adopts respectively two side rail bars, two side rail bars are arranged above and below, described guardrail strut and guardrail pole are L-type, set up an oblique pole and surround three point arbitrage in L corner, and the side rail bar that is arranged in below is through at above-mentioned three point arbitrage and is fixed.
Beneficial effect of the present invention: the present invention adopts collapsible mode, reduce on the one hand bracket taking up room in freight container, reduced the traffic cost of fuselage sections of aircraft section, the time and the pallet for transporting that have reduced on the other hand pallet for transporting dismounting vanning recover the multiplexing time.
Brief description of the drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is the view after the present invention decomposes dismounting and after self folding.
Detailed description of the invention
As shown in Figure 1, the collapsible pallet for transporting of large-scale main body section section, entirety is " basket " formula structure, its bottom is provided with two girders 15 along fore-and-aft direction is parallel, between two girders 15, be connected with carrying tankette fagging 03, and carrying tankette fagging 03 is positioned at two ends of girder 15 front and back, be separately installed with end angle fence upright 05 in four corners of " basket " formula structure, end angle fence upright 05 removably connects with girder 15.Former and later two protection faces of " basket " formula structure are by adopting formations that removably connects of termination horizontal bar bar 04 and end angle fence upright 05, and two of the left and right protection face of " basket " formula structure is by adopting side rail bar 06 and holding angle fence upright 05 formation that removably connects.Between side rail bar 06 and girder 15, be distributed with the guardrail strut 10 and the guardrail pole 07 that connect for strengthening, between corresponding two ends, girder 15 front and back, be fixed with bucket section brace supporting plate 14, above bucket section brace supporting plate 14, be provided with the bucket section fastening straps 02 for fixed main body, on girder 15, be fixed with a fuselage lifting pillar 08, on a fuselage lifting pillar 08, be provided with a lifting fastening straps 13.
On girder 15, be fixed with turnover post 11, alighting gear hinge steady arm 12 and the lifting arm 09 of stacking, stacking post 11 keeps flat under normal conditions, upright in use, object is that in making two brackets be stacked together in the time backhauling to pack into the container, alighting gear hinge steady arm 12 is for retraining fuselage bucket section along the displacement in Z-direction and displacement transversely.Lifting arm 09 is fixedly connected with girder 15 by bolt and lifting arm offside guard rail rod plays certain supporting role, and lifting arm 09 is used for hanging oneself and rising toward truck shelving aircraft components.Be connected with the keysets on fuselage keel bar at the fixing chain 01 of the keel bar between two girders 15, (indulge) displacement of direction for retraining fuselage bucket section along front and back.
The side, two of left and right of described " basket " formula structure adopts respectively two side rail bars 06, two side rail bars 06 are arranged above and below, described guardrail strut 10 and guardrail pole 07 are L-type, set up an oblique pole and surround three point arbitrage in L corner, the side rail bar 06 that is arranged in below is through at above-mentioned three point arbitrage and is fixed.
The present invention is before backhauling, first the termination horizontal bar bar 04 in Fig. 1, end angle fence upright 05, side rail bar 06, guardrail pole 07, guardrail strut 10 to be dismantled and decomposed from integral bracket, and the part after tie bolt and the decomposition of decomposing after dismounting is included into tool box, large decomposition part is positioned over bracket middle part; Then by keep flat to stack post 11 upright, as shown in Figure 2, carry out self folding of fuselage lifting a pillar 08, lifting arm 09 and front and back end extendible portion 16,17 simultaneously, now two can be completed and disassembled the bracket folding with self and be stacked together by stacking post 11, and the hook carrying with bracket is fixed together two brackets, last backhauls with sending into freight container.
Claims (2)
1. the collapsible pallet for transporting of large-scale main body section section, it is characterized in that: entirety is " basket " formula structure, its bottom is along parallel two girders (15) that are provided with of fore-and-aft direction, between two girders (15), be connected with carrying tankette fagging (03), and carrying tankette fagging (03) is positioned at two ends before and after girder (15), be separately installed with end angle fence upright (05) in four corners of " basket " formula structure, end angle fence upright (05) removably connects with girder (15), former and later two protection faces of " basket " formula structure are by adopting termination horizontal bar bar (04) and end angle fence upright (05) formation that removably connects, two of the left and right protection face of " basket " formula structure is by adopting side rail bar (06) and end angle fence upright (05) formation that removably connects, between side rail bar (06) and girder (15), be distributed with the guardrail strut (10) and the guardrail pole (07) that connect for strengthening, before and after girder (15), between corresponding two ends, be fixed with bucket section brace supporting plate (14), be provided with the bucket section fastening straps (02) for fixed main body in the top of bucket section brace supporting plate (14), on girder (15), be fixed with a fuselage lifting pillar (08), on a fuselage lifting pillar (08), be provided with a lifting fastening straps (13), on girder (15), be fixed with the turnover post (11) that stacks, alighting gear hinge steady arm (12) and lifting arm (09), lifting arm (09) is fixedly connected with girder (15) by bolt and lifting arm (09) offside guard rail rod (06) plays a supportive role, the fixing chain (01) of keel bar being positioned between two girders (15) is connected with the keysets on fuselage keel bar, for limiting the longitudinal travel of fuselage bucket section.
2. the collapsible pallet for transporting of large-scale main body section section as claimed in claim 1, it is characterized in that: the side, two of left and right of described " basket " formula structure adopts respectively two side rail bars (06), two side rail bars (06) are arranged above and below, described guardrail strut (10) and guardrail pole (07) are L-type, set up an oblique pole and surround three point arbitrage in L corner, the side rail bar (06) that is arranged in below is through at above-mentioned three point arbitrage and is fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410259923.9A CN103991649B (en) | 2014-06-12 | 2014-06-12 | The collapsible pallet for transporting of large-scale main body section section |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410259923.9A CN103991649B (en) | 2014-06-12 | 2014-06-12 | The collapsible pallet for transporting of large-scale main body section section |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103991649A true CN103991649A (en) | 2014-08-20 |
| CN103991649B CN103991649B (en) | 2016-04-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410259923.9A Active CN103991649B (en) | 2014-06-12 | 2014-06-12 | The collapsible pallet for transporting of large-scale main body section section |
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| CN (1) | CN103991649B (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216684A (en) * | 2017-12-08 | 2018-06-29 | 西安飞机工业（集团）有限责任公司 | A kind of aircraft skin transport vehicle |
| CN109368021A (en) * | 2018-11-16 | 2019-02-22 | 芜湖新兴新材料产业园有限公司 | Bend pipe tools material frame |
| CN110002002A (en) * | 2019-04-24 | 2019-07-12 | 新乡市永安机械设备有限公司 | A kind of helicopter foldable bracket |
| CN110816951A (en) * | 2019-09-30 | 2020-02-21 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110979727A (en) * | 2019-12-09 | 2020-04-10 | 中航沈飞民用飞机有限责任公司 | Aircraft tail cone transportation bracket |
| CN113665819A (en) * | 2020-05-15 | 2021-11-19 | 中航西飞民用飞机有限责任公司 | Aircraft suspended structure |
| CN113978909A (en) * | 2021-12-30 | 2022-01-28 | 四川腾盾科技有限公司 | Large unmanned aerial vehicle transportation fixing device and sedan type constraint method |
| CN114013786A (en) * | 2021-11-26 | 2022-02-08 | 昌河飞机工业（集团）有限责任公司 | Flexible supporting and placing device for helicopter frame |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6257522B1 (en) * | 1997-03-31 | 2001-07-10 | The Boeing Company | Multi-beam method and apparatus for removing and replacing major structural components while converting an airplane to efficiently carry freight |
| CN1432509A (en) * | 2002-01-14 | 2003-07-30 | 奥特玛尔·法里昂 | Maintenance mount unit for aeroplane, etc. |
| EP1905690A2 (en) * | 2006-09-27 | 2008-04-02 | Airbus Espana, S.L. | Mobile transport platform for the handling of aeronautical parts |
| CN102101531A (en) * | 2009-12-22 | 2011-06-22 | 尤洛考普特德国有限公司 | Lift device for replacing dynamic or static components of helicopter-type aircraft |
| CN102249006A (en) * | 2011-05-11 | 2011-11-23 | 西安飞机工业（集团）有限责任公司 | Movement butt joint device for large body part of airplane general assembly |
| CN102656089A (en) * | 2009-11-20 | 2012-09-05 | 斯奈克玛 | Carriage for the transport of an aircraft engine module |
| WO2014046783A1 (en) * | 2012-09-18 | 2014-03-27 | The Boeing Company | Transport, assembly, and edge stabilizing system and method for composite barrel segments |
-
2014
- 2014-06-12 CN CN201410259923.9A patent/CN103991649B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6257522B1 (en) * | 1997-03-31 | 2001-07-10 | The Boeing Company | Multi-beam method and apparatus for removing and replacing major structural components while converting an airplane to efficiently carry freight |
| CN1432509A (en) * | 2002-01-14 | 2003-07-30 | 奥特玛尔·法里昂 | Maintenance mount unit for aeroplane, etc. |
| EP1905690A2 (en) * | 2006-09-27 | 2008-04-02 | Airbus Espana, S.L. | Mobile transport platform for the handling of aeronautical parts |
| CN102656089A (en) * | 2009-11-20 | 2012-09-05 | 斯奈克玛 | Carriage for the transport of an aircraft engine module |
| CN102101531A (en) * | 2009-12-22 | 2011-06-22 | 尤洛考普特德国有限公司 | Lift device for replacing dynamic or static components of helicopter-type aircraft |
| CN102249006A (en) * | 2011-05-11 | 2011-11-23 | 西安飞机工业（集团）有限责任公司 | Movement butt joint device for large body part of airplane general assembly |
| WO2014046783A1 (en) * | 2012-09-18 | 2014-03-27 | The Boeing Company | Transport, assembly, and edge stabilizing system and method for composite barrel segments |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216684A (en) * | 2017-12-08 | 2018-06-29 | 西安飞机工业（集团）有限责任公司 | A kind of aircraft skin transport vehicle |
| CN109368021A (en) * | 2018-11-16 | 2019-02-22 | 芜湖新兴新材料产业园有限公司 | Bend pipe tools material frame |
| CN109368021B (en) * | 2018-11-16 | 2024-01-05 | 芜湖新兴新材料产业园有限公司 | Elbow pipe fitting work or material rest |
| CN110002002A (en) * | 2019-04-24 | 2019-07-12 | 新乡市永安机械设备有限公司 | A kind of helicopter foldable bracket |
| CN110002002B (en) * | 2019-04-24 | 2024-01-16 | 新乡市永安机械设备有限公司 | Folding bracket for helicopter |
| CN110816951A (en) * | 2019-09-30 | 2020-02-21 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110816951B (en) * | 2019-09-30 | 2022-07-12 | 中航成飞民用飞机有限责任公司 | Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts |
| CN110979727A (en) * | 2019-12-09 | 2020-04-10 | 中航沈飞民用飞机有限责任公司 | Aircraft tail cone transportation bracket |
| CN113665819A (en) * | 2020-05-15 | 2021-11-19 | 中航西飞民用飞机有限责任公司 | Aircraft suspended structure |
| CN114013786A (en) * | 2021-11-26 | 2022-02-08 | 昌河飞机工业（集团）有限责任公司 | Flexible supporting and placing device for helicopter frame |
| CN114013786B (en) * | 2021-11-26 | 2023-12-15 | 昌河飞机工业（集团）有限责任公司 | Helicopter frame-adding flexible supporting device |
| CN113978909A (en) * | 2021-12-30 | 2022-01-28 | 四川腾盾科技有限公司 | Large unmanned aerial vehicle transportation fixing device and sedan type constraint method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103991649B (en) | 2016-04-20 |
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