CN205292452U - Aircraft wing box transportation trailer's multi -functional pull formula supporter - Google Patents

Aircraft wing box transportation trailer's multi -functional pull formula supporter Download PDF

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Publication number
CN205292452U
CN205292452U CN201520972863.5U CN201520972863U CN205292452U CN 205292452 U CN205292452 U CN 205292452U CN 201520972863 U CN201520972863 U CN 201520972863U CN 205292452 U CN205292452 U CN 205292452U
Authority
CN
China
Prior art keywords
bending
fixed
stull
vertical support
crossbeam
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
Application number
CN201520972863.5U
Other languages
Chinese (zh)
Inventor
张书斌
安蓉
邱晞
高建武
陈尚普
王礼春
李士保
王旺根
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC Aircraft Corp Xian Aircraft Branch
Anhui Kaile Special Vehicles Co Ltd
Original Assignee
AVIC Aircraft Corp Xian Aircraft Branch
Anhui Kaile Special Vehicles Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AVIC Aircraft Corp Xian Aircraft Branch, Anhui Kaile Special Vehicles Co Ltd filed Critical AVIC Aircraft Corp Xian Aircraft Branch
Priority to CN201520972863.5U priority Critical patent/CN205292452U/en
Application granted granted Critical
Publication of CN205292452U publication Critical patent/CN205292452U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an aircraft wing box transportation trailer's multi -functional pull formula supporter, including top part under with, top including two vertical support no. 1 and stull no. 1, the lower part divide including two vertical support no. 2 and stull no. 2 vertical support no. 1 and vertical support's no. 2 lateral surface on the even a plurality of round pins axle no. 1 of installing, the both ends of stull no. 1 are fixed respectively in two vertical support's no. 1 upper end, the lower extreme at two vertical support no. 2 is fixed respectively at the both ends of stull no. 2, all installs the axle with spring washers and deep groove ball bearing at the outer end tip of every round pin axle no. 1, cooperation rotation connection through round pin axle no. 2, plain washer, split pin, connecting plate and backing pin between two vertical support's no. 1 lower extreme and two vertical support's no. 2 the upper end. The utility model discloses the pull formula is put the roof truss and is placed at vehicle body back portion, can place the multiple structure irregularity body simultaneously, has effectively saved the space, and this configuration operation is convenient, and is simply easy -to -use.

Description

A kind of Multifunctional drawer type rack of aircraft wing box transtainer
Technical field
This utility model relates to aircraft wing box transtainer technical field, particularly relates to the Multifunctional drawer type rack of a kind of aircraft wing box transtainer.
Background technology
Aircraft wing box transtainer adopts tenon riveting trailer, and vehicle frame bottom is liftoff, and minimum clearance only has 150mm; Car load adopts seal case structure, and seal request is particularly harsh, and complete vehicle structure is arranged comparatively compact, and space need to be effectively utilized.
Utility model content
This utility model purpose is contemplated to make up the defect of prior art, it is provided that the Multifunctional drawer type rack of a kind of aircraft wing box transtainer.
This utility model is achieved through the following technical solutions:
A kind of Multifunctional drawer type rack of aircraft wing box transtainer, include upper and bottom section, described upper part includes two perpendicular supports one and stull one, described lower part includes two perpendicular supports two and stull two, the lateral surface of described perpendicular support one and perpendicular support two is provided with multiple bearing pin one uniformly, the two ends of stull one are separately fixed at the upper end of two perpendicular supports one, the two ends of stull two are separately fixed at the lower end of two perpendicular supports two, it is mounted on axle elastic washer and deep groove ball bearing in the end, outer end of each bearing pin one, by bearing pin two between the upper end of the lower end of two perpendicular supports one and two perpendicular supports two, plain washer, split pin, the cooperation of connecting plate and backing pin is rotationally connected, equidistant between two perpendicular supports two it is fixed with five bending crossbeams, first bending crossbeam is fixed with the bending transverse slat one of the outer end upwards bending of downside, second, three, four bending crossbeams are respectively and fixedly provided with the outer end of upper side and downside separately down and the bending transverse slat two of upwards bending, the bending transverse slat three of bending under the outer end being fixed with upper side on the 5th bending crossbeam, it is positioned between two perpendicular supports two and equidistant below the 5th bending crossbeam is fixed with two horizontal supporting plates, it is fixed with jacking bracket crossbeam between first horizontal supporting plate and the 5th bending crossbeam, jacking bracket crossbeam is fixed with jacking bracket, it is fixed with backing plate bearing between first horizontal supporting plate and second horizontal supporting plate, backing plate bearing is provided with screw rod, at the top of screw rod, small handwheel is installed.
1, pull pull bar, by deep groove ball bearing, rack is pulled out from guide rail, guide rail arranges baffle plate, when moving to baffle position, by bearing pin two, rack is folded, and one end is placed on the ground, reach the state of mounting.
2, the construction features according to object, is divided into several little space at rack, and designs suitable construction placement object and fixed structure;
3, after object installation, rack is advanced railway carriage and fixes.
The utility model has the advantages that: this utility model drawing and pulling type is put roof truss and is placed on rear vehicle, can place various structures irregularly shaped object simultaneously, effectively save space, this structure operation is convenient, easy to use.
Accompanying drawing explanation
Fig. 1 is top view of the present utility model.
Fig. 2 is left view of the present utility model.
Fig. 3 is the perpendicular support one of this utility model and perpendicular support two junction partial enlarged drawings.
Detailed description of the invention
Such as Fig. 1, 2, shown in 3, a kind of Multifunctional drawer type rack of aircraft wing box transtainer, include upper and bottom section, described upper part includes two perpendicular supports 1 and stull 1, described lower part includes two perpendicular supports 23 and stull 24, the lateral surface of described perpendicular support 1 and perpendicular support 23 is provided with multiple bearing pin 1 uniformly, the two ends of stull 1 are separately fixed at the upper end of two perpendicular supports 1, the two ends of stull 24 are separately fixed at the lower end of two perpendicular supports 23, axle elastic washer 6 and deep groove ball bearing 7 it is mounted in the end, outer end of each bearing pin 1, by bearing pin 28 between the upper end of the lower end of two perpendicular supports 1 and two perpendicular supports 23, plain washer 9, split pin 10, the cooperation of connecting plate 11 and backing pin 12 is rotationally connected, equidistant between two perpendicular supports 23 it is fixed with five bending crossbeams 13, first bending crossbeam is fixed with the bending transverse slat 1 of the outer end upwards bending of downside, second, three, four bending crossbeams are respectively and fixedly provided with the outer end of upper side and downside separately down and the bending transverse slat 2 15 of upwards bending, the bending transverse slat 3 16 of bending under the outer end being fixed with upper side on the 5th bending crossbeam, it is positioned between two perpendicular supports 23 and equidistant below the 5th bending crossbeam 13 is fixed with two horizontal supporting plates 17, it is fixed with jacking bracket crossbeam 18 between first horizontal supporting plate and the 5th bending crossbeam, jacking bracket crossbeam 18 is fixed with jacking bracket 19, it is fixed with backing plate bearing 20 between first horizontal supporting plate and second horizontal supporting plate, backing plate bearing 20 is provided with screw rod 21, at the top of screw rod 21, small handwheel 22 is installed.

Claims (1)

1. the Multifunctional drawer type rack of an aircraft wing box transtainer, it is characterized in that: include upper and bottom section, described upper part includes two perpendicular supports one and stull one, described lower part includes two perpendicular supports two and stull two, the lateral surface of described perpendicular support one and perpendicular support two is provided with multiple bearing pin one uniformly, the two ends of stull one are separately fixed at the upper end of two perpendicular supports one, the two ends of stull two are separately fixed at the lower end of two perpendicular supports two, it is mounted on axle elastic washer and deep groove ball bearing in the end, outer end of each bearing pin one, by bearing pin two between the upper end of the lower end of two perpendicular supports one and two perpendicular supports two, plain washer, split pin, the cooperation of connecting plate and backing pin is rotationally connected, equidistant between two perpendicular supports two it is fixed with five bending crossbeams, first bending crossbeam is fixed with the bending transverse slat one of the outer end upwards bending of downside, second, three, four bending crossbeams are respectively and fixedly provided with the outer end of upper side and downside separately down and the bending transverse slat two of upwards bending, the bending transverse slat three of bending under the outer end being fixed with upper side on the 5th bending crossbeam, it is positioned between two perpendicular supports two and equidistant below the 5th bending crossbeam is fixed with two horizontal supporting plates, it is fixed with jacking bracket crossbeam between first horizontal supporting plate and the 5th bending crossbeam, jacking bracket crossbeam is fixed with jacking bracket, it is fixed with backing plate bearing between first horizontal supporting plate and second horizontal supporting plate, backing plate bearing is provided with screw rod, at the top of screw rod, small handwheel is installed.
CN201520972863.5U 2015-11-26 2015-11-26 Aircraft wing box transportation trailer's multi -functional pull formula supporter Expired - Fee Related CN205292452U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520972863.5U CN205292452U (en) 2015-11-26 2015-11-26 Aircraft wing box transportation trailer's multi -functional pull formula supporter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520972863.5U CN205292452U (en) 2015-11-26 2015-11-26 Aircraft wing box transportation trailer's multi -functional pull formula supporter

Publications (1)

Publication Number Publication Date
CN205292452U true CN205292452U (en) 2016-06-08

Family

ID=56436220

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520972863.5U Expired - Fee Related CN205292452U (en) 2015-11-26 2015-11-26 Aircraft wing box transportation trailer's multi -functional pull formula supporter

Country Status (1)

Country Link
CN (1) CN205292452U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108263632A (en) * 2018-03-13 2018-07-10 江苏捷诚车载电子信息工程有限公司 Unmanned plane transports and launch vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108263632A (en) * 2018-03-13 2018-07-10 江苏捷诚车载电子信息工程有限公司 Unmanned plane transports and launch vehicle
CN108263632B (en) * 2018-03-13 2024-03-19 江苏捷诚车载电子信息工程有限公司 Unmanned aerial vehicle transportation and launching galloping

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160608

Termination date: 20211126

CF01 Termination of patent right due to non-payment of annual fee