CN103991649B - The collapsible pallet for transporting of large-scale main body section section - Google Patents
The collapsible pallet for transporting of large-scale main body section section Download PDFInfo
- Publication number
- CN103991649B CN103991649B CN201410259923.9A CN201410259923A CN103991649B CN 103991649 B CN103991649 B CN 103991649B CN 201410259923 A CN201410259923 A CN 201410259923A CN 103991649 B CN103991649 B CN 103991649B
- Authority
- CN
- China
- Prior art keywords
- girder
- section
- bar
- fixed
- transporting
- 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.)
- Active
Links
Abstract
The invention provides the collapsible pallet for transporting of a kind of large-scale main body section section, overall in " basket " formula structure, end angle fence upright and girder removably connect, former and later two protection faces adopt termination horizontal bar bar to removably connect with end angle fence upright and are formed, two, left and right protection face adopts side guard bar to removably connect with end angle fence upright and is formed, bucket section brace supporting plate is fixed with between corresponding two ends before and after girder, the bucket section fastening straps for fixed main body is provided with above bucket section brace supporting plate, girder is fixed with and turnoverly stacks post, alighting gear hinge steady arm and lifting arm <b>, the keel bar of </b> between two girders is fixed chain and is connected with the keysets on fuselage keel bar.The present invention adopts collapsible mode, reduces bracket taking up room in freight container on the one hand, reduces the traffic cost of fuselage sections of aircraft section, and the time and the pallet for transporting that reduce pallet for transporting dismounting vanning on the other hand recover the multiplexing time.
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, pallet for transporting for using in main body section section transportation also can be generally the instrument of super large, and traditional pallet for transporting all adopts overall backhauling, the position of a freight container is taken to I haven't seen you for ages, when pallet for transporting is larger, then need the case position taken 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 and take up room, reduce traffic cost.
Technical scheme of the present invention: the collapsible pallet for transporting of large-scale main body section section, overall in groove-like, two girders are provided with along fore-and-aft direction is parallel bottom it, carrying tankette fagging is connected with between two girders, and carrying tankette fagging is positioned at two ends before and after girder, end angle fence upright is separately installed with in groove four corners, end angle fence upright and girder removably connect, former and later two protection faces of groove are formed by adopting termination horizontal bar bar and end angle fence upright to removably connect, two, the left and right protection face of groove is formed by adopting side guard bar and end angle fence upright to removably connect, the guardrail strut for strengthening connection and guardrail pole is distributed with between side guard bar and girder, bucket section brace supporting plate is fixed with between corresponding two ends before and after girder, the bucket section fastening straps for fixed main body is provided with above bucket section brace supporting plate, girder is fixed with fuselage lifting head pillar, fuselage lifting head pillar is provided with lifting head fastening straps, girder is fixed with and turnoverly stacks post, alighting gear hinge steady arm and lifting arm, lifting arm to be fixedly connected with girder by bolt and lifting arm plays certain supporting role to side guard bar, keel bar between two girders is fixed chain and is connected with the keysets on fuselage keel bar, the longitudinal travel of restriction fuselage bucket section.
The side, two, left and right of described groove adopts two side guard bar respectively, two side guard bar 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 guard bar being 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 bracket taking up room in freight container on the one hand, reduce the traffic cost of fuselage sections of aircraft section, the time and the pallet for transporting that reduce pallet for transporting dismounting vanning on the other hand recover the multiplexing time.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the view after the present invention decomposes the rear also folding onto itself of dismounting.
Detailed description of the invention
As shown in Figure 1, the collapsible pallet for transporting of large-scale main body section section, overall in groove-like, two girders 15 are provided with along fore-and-aft direction is parallel bottom it, carrying tankette fagging 03 is connected with between two girders 15, 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 groove four corners, end angle fence upright 05 removably connects with girder 15.Former and later two protection faces of groove are formed by adopting termination horizontal bar bar 04 and end angle fence upright 05 to removably connect, and two, the left and right protection face of groove is formed by adopting side guard bar 06 and end angle fence upright 05 to removably connect.The guardrail strut 10 for strengthening connection and guardrail pole 07 is distributed with between side guard bar 06 and girder 15, bucket section brace supporting plate 14 is fixed with between corresponding two ends before and after girder 15, the bucket section fastening straps 02 for fixed main body is provided with above bucket section brace supporting plate 14, girder 15 is fixed with fuselage lifting head pillar 08, fuselage lifting head pillar 08 is provided with lifting head fastening straps 13.
Girder 15 is fixed with and turnoverly stacks post 11, alighting gear hinge steady arm 12 and lifting arm 09, stack post 11 to keep flat under normal conditions, upright in use, object is that in making two brackets be stacked together to pack into the container when backhauling, alighting gear hinge steady arm 12 is for retraining fuselage bucket section along the displacement in Z-direction and displacement transversely.Lifting arm 09 to be fixedly connected with girder 15 by bolt and lifting arm plays certain supporting role to side guard bar, and lifting arm 09 is used to hang oneself toward truck rise shelving aircraft components.Keel bar between two girders 15 is fixed chain 01 and is connected with the keysets on fuselage keel bar, for retraining the displacement of fuselage bucket section along front and back (indulging) direction.
The side, two, left and right of described groove adopts two side guard bar 06 respectively, two side guard bar 06 are arranged above and below, described guardrail strut 10 and guardrail pole 07 are in L-type, set up an oblique pole in L corner and surround three point arbitrage, the side guard bar 06 being 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 guard bar 06, guardrail pole 07, guardrail strut 10 to be dismantled from integral bracket and decompose, and the part after decomposing the tie bolt after dismantling and decomposition is included into tool box, large decomposition part is positioned in the middle part of bracket; Then by keep flat to stack post 11 upright, as shown in Figure 2, carry out the folding onto itself of fuselage lifting head pillar 08, lifting arm 09 and front and back end extendible portion 16,17 simultaneously, now two can be completed to disassemble and be stacked together by stacking post 11 with the bracket of folding onto itself, and with the hook that bracket carries, two brackets are fixed together, 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: overall in groove-like, two girders (15) are provided with along fore-and-aft direction is parallel bottom it, carrying tankette fagging (03) is connected with between two girders (15), and carrying tankette fagging (03) is positioned at two ends before and after girder (15), end angle fence upright (05) is separately installed with in groove four corners, end angle fence upright (05) and girder (15) removably connect, former and later two protection faces of groove are formed by adopting termination horizontal bar bar (04) and end angle fence upright (05) to removably connect, two, the left and right protection face of groove is formed by adopting side guard bar (06) and end angle fence upright (05) to removably connect, the guardrail strut (10) for strengthening connection and guardrail pole (07) is distributed with between side guard bar (06) and girder (15), bucket section brace supporting plate (14) is fixed with between corresponding two ends before and after girder (15), the bucket section fastening straps (02) for fixed main body is provided with in the top of bucket section brace supporting plate (14), girder (15) is fixed with fuselage lifting head pillar (08), fuselage lifting head pillar (08) is provided with lifting head fastening straps (13), girder (15) is fixed with and turnoverly stacks post (11), alighting gear hinge steady arm (12) and lifting arm (09), lifting arm (09) to be fixedly connected with girder (15) by bolt and lifting arm (09) plays a supportive role to side guard bar (06), the keel bar be positioned between two girders (15) is fixed chain (01) and 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, left and right of described groove adopts two side guard bar (06) respectively, two side guard bar (06) are arranged above and below, described guardrail strut (10) and guardrail pole (07) are in L-type, set up an oblique pole in L corner and surround three point arbitrage, the side guard bar (06) being 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 CN103991649A (en) | 2014-08-20 |
| CN103991649B true CN103991649B (en) | 2016-04-20 |
Family
ID=51306046
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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103991649B (en) |
Families Citing this family (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 |
| 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 |
| 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 |
| 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 |
| CN110979727B (en) * | 2019-12-09 | 2023-05-05 | 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 |
| 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 |
| CN113978909B (en) * | 2021-12-30 | 2022-03-22 | 四川腾盾科技有限公司 | Large unmanned aerial vehicle transportation fixing device and sedan type constraint method |
Family Cites Families (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 |
| DE10201202B4 (en) * | 2002-01-14 | 2009-11-26 | Otmar Fahrion | Docking unit for servicing an aircraft or the like |
| ES2294947B1 (en) * | 2006-09-27 | 2009-02-16 | Airbus España, S.L. | MOBILE TRANSPORT PLATFORM FOR THE HANDLING OF AIRCRAFT PARTS. |
| FR2952921B1 (en) * | 2009-11-20 | 2012-05-25 | Snecma | TRANSPORT TROLLEY FOR AN AIRCRAFT ENGINE MODULE |
| EP2338794B1 (en) * | 2009-12-22 | 2018-08-29 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | 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 |
| US10160076B2 (en) * | 2012-09-18 | 2018-12-25 | The Boeing Company | Edge stabilizing system and method for composite barrel segments |
-
2014
- 2014-06-12 CN CN201410259923.9A patent/CN103991649B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN103991649A (en) | 2014-08-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103991649B (en) | The collapsible pallet for transporting of large-scale main body section section | |
| CN104088227A (en) | Rear pull rod | |
| CN103192882B (en) | Framework type frame structure and concrete pump truck | |
| CN203410480U (en) | Foldable type pull rod vehicle | |
| CN205531673U (en) | Flexible safety barrier | |
| CN203460888U (en) | Foldable draw bar trolley | |
| CN202788002U (en) | Assembled overhanging-type feed-receiving platform | |
| CN205168749U (en) | Tricycle freight car | |
| CN204920764U (en) | Folding single ladder | |
| CN203567906U (en) | Cargo hold ladder reinforcement structure | |
| CN204210906U (en) | A kind of section bar transportation frame | |
| CN203268127U (en) | Frame type car frame structure and concrete pump car | |
| CN202784099U (en) | Package and transportation framework | |
| CN202505624U (en) | First-aid stretcher cart | |
| CN202967192U (en) | Top corner piece and middle twist lock and container comprising the same | |
| CN105151519A (en) | Convenient-to-use profile placement frame | |
| CN203958220U (en) | A kind of Portable reinforcing steel bar transport trolley | |
| CN204701865U (en) | Gantry type manned solution bundle frame | |
| CN204917599U (en) | Staircase transportation support frame | |
| CN204173875U (en) | A kind of fork truck loads the auxiliary mould of glass casing | |
| CN203321321U (en) | Hydraulic power skid-mounted structure provided with fork holes | |
| CN204823777U (en) | Two roof beam hoists are with integrated monkey frame | |
| CN204750011U (en) | Portable tank wagon cat ladder | |
| CN205233295U (en) | A collapsible aircraft protection against rodents section of thick bamboo | |
| CN202744288U (en) | Cradle for loading and unloading goods |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |