CN208080709U - A kind of flight case inner support skeleton structure - Google Patents

A kind of flight case inner support skeleton structure Download PDF

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Publication number
CN208080709U
CN208080709U CN201820367582.0U CN201820367582U CN208080709U CN 208080709 U CN208080709 U CN 208080709U CN 201820367582 U CN201820367582 U CN 201820367582U CN 208080709 U CN208080709 U CN 208080709U
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China
Prior art keywords
former
telescopic lever
section telescopic
section
flight case
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CN201820367582.0U
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Chinese (zh)
Inventor
廖银才
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Fujian Jinjiang Taixiang Technology Co Ltd
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Adimaner Lerther Article & Dress Decoration Co Ltd
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Priority to CN201820367582.0U priority Critical patent/CN208080709U/en
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Abstract

The utility model discloses a kind of flight case inner support skeleton structures, including upper former, lower former and two three section telescopic levers, three section telescopic lever lower ends are connect with lower former inner bottom surface, upper former is equipped with upper vacancy section, lower former is equipped with lower vacancy section, and upper former and lower former are all made of rigid plastics and are made;Middle part is equipped with collecting part on rear side of upper former, and three section telescopic lever upper ends pass through collecting part, three section telescopic lever upper ends to be equipped with handle, storage position is equipped with above upper former, and Middle face is equipped with button latch on handle, and upper former is connected with lower former by four supporting rods;Handgrip is equipped with above upper former, upper former inner top surface is equipped with inner bolt hole and solid slug;Lower former following four corners is equipped with mounting base, and mounting base lower end is equipped with universal single-wheel.The device is the skeleton structure for including upper former and lower former, is connected with supporting rod between upper former and lower former, can meet moulding and support function, reduce the usage amount of raw material, reduces the overall weight of flight case.

Description

A kind of flight case inner support skeleton structure
Technical field
The utility model is specifically related to a kind of flight case inner support skeleton structure.
Background technology
Flight case, also known as trolley case, luggage case, suitcase are entrained to place the chest of article when going out, it is The one of which type of luggage.Usual flight case is for placing required clothing, personal-care supplies and souvenir on journey Product.The flight case of early stage is made of with timber or other heavier materials, and with popularizing for air travel, the material of flight case becomes To more light hard plastic or cloth.Flight case inner support currently on the market is a monoblock plank of unification, is used for babinet Moulding and support, including it is connected as the upper former, lower former and rear former of an entirety so that flight case overall weight is larger.
Utility model content
The shortcomings that the purpose of the utility model is to overcome the prior arts provides a kind of flight case inner support skeleton structure, with Solve the problems, such as that existing flight case overall weight is larger.
To achieve the above object, technical solution adopted in the utility model is:A kind of flight case inner support skeleton knot is provided Structure includes the three section telescopic levers of upper former, lower former and two side by side, and three section telescopic lever lower ends connect with lower former inner bottom surface It connects, upper former is equipped with upper vacancy section, and lower former is equipped with lower vacancy section, and upper former and lower former are all made of rigid plastics system At;Middle part is equipped with collecting part on rear side of the upper former, and three section telescopic lever upper ends pass through collecting part, three section telescopic lever upper ends to set There is handle, storage position recessed and that handle can be accommodated is equipped with above upper former, is stretched respectively with one three section on the downside of handle both ends Contracting pull rod upper end connects, and Middle face is equipped with the button latch for fixing three section telescopic lever collapsing lengths on handle;
The upper former is connected with lower former by four supporting rods parallel to each other, and four supporting rods press rectanglar arrangement, Post upper is connect with upper former inner top surface, and supporting rod lower end is connect with lower former inner bottom surface;It is equipped with above the upper former Handgrip, upper former inner top surface be equipped with multiple inner bolt holes, inner bolt hole side be equipped with solid slug, inner bolt hole or solid slug by screw with Handgrip connects, and inner bolt hole and solid slug are respectively positioned in vacancy section;
The lower former following four corners is equipped with dismountable mounting base, and mounting base lower end is equipped with dismountable universal list Wheel, mounting base upper end are equipped with the backplate being located on rear side of lower former, are flushed on rear side of collecting part and backplate;After the lower former inner bottom surface Middle side part is equipped with solid seat, and solid seat both ends are equipped with hollow connecting pole, and one three section telescopic lever lower end is located at a company It connects inside column, three section telescopic lever lower ends are connect by screw with solid seat, and solid seat is located in lower vacancy section.
It is upturned and the arc bound edge Jing Guo solid processing preferably, the lower former edge is equipped with.
Preferably, the mounting base is connect by screw with lower former.
Preferably, the three sections telescopic lever is aluminum alloy material.
Preferably, the supporting rod is made of glass fiber rod.
The beneficial effects of the utility model are:
1. existing flight case inner support is reduced to the skeleton structure of only upper former and lower former, upper former by the utility model It is connected with supporting rod between lower former, moulding and support function can be met, while the usage amount of raw material can also be reduced, Effectively reduce the overall weight of flight case.
2. the inner bolt hole on the utility model in vacancy section is with solid slug together with, inner bolt hole or solid slug pass through spiral shell Nail is connect with the handgrip above upper former, can avoid the error during manual operation mould assembling, handgrip is enable to be more prone to Be fixed on above former.
3. mainly wheel, the universal single-wheel of the device and the peace of serious wear during the utility model flight case use It is all dismountable to fill seat, is replaced convenient for the universal single-wheel to damage, effectively extends the service life of flight case.
4. being flushed on rear side of the utility model collecting part and the backplate of mounting base upper end, make two backplates of collecting part and rear side The firm support construction of a triangle is formed, being in direct contact with ground when flight case can be avoided to keep flat causes to wear.
5. the solid seat of former inner bottom surface is located in lower vacancy section under the utility model, one three section telescopic lever lower end is solid It is scheduled in the connecting pole of solid seat one end, to reduce using the impact to lower former during pull rod, keeps lower former stress opposite Uniformly, preventing strength from excessively concentrating makes lower former damage.
6. the arc bound edge at former edge is upturned and passes through solid processing under the utility model, lower former can be enhanced The intensity at edge, in case lower former edge stress is damaged.
7. the utility model is conducive to ensureing skeleton stability using supporting rod made of glass fiber rod, that is, light and secured Under the premise of reduce its weight.
Description of the drawings
Fig. 1 is the structural schematic diagram one of flight case inner support skeleton structure;
Fig. 2 is the structural schematic diagram two of flight case inner support skeleton structure.
Wherein:1, collecting part;2, position is stored;3, backplate;4, mounting base;5, universal single-wheel;6, lower vacancy section;7, solid Seat;8, connecting pole;9, lower former;10, arc bound edge;11, supporting rod;12, upper former;13, upper vacancy section;14, three sections are flexible Pull rod;15, button latch;16, handle;17, inner bolt hole;18, solid slug.
Specific implementation mode
It is specific below in conjunction with the utility model to keep the purpose of this utility model, technical solution and advantage clearer Technical solutions of the utility model are clearly and completely described in embodiment and corresponding attached drawing.
With reference to figure 1,2, the present embodiment provides a kind of flight case inner support skeleton structures, including upper former, lower former 9 and two Three section telescopic levers 14 side by side, three section 14 lower ends of telescopic lever are connect with lower 9 inner bottom surface of former, and upper former is equipped with upper hollow out Area 13, lower former are equipped with lower vacancy section 6, and upper former and lower former 9 are all made of rigid plastics and are made;In on rear side of the upper former Portion is equipped with collecting part 1, and three 14 upper ends of section telescopic lever pass through collecting part 1, three 14 upper ends of section telescopic lever to be equipped with handle 16, upper width It is equipped with storage position 2 recessed and that handle 16 can be accommodated above plate, telescopic lever is saved with one three respectively on the downside of 16 both ends of handle 14 upper ends connect, and Middle face is equipped with the button latch 15 for fixing three section telescopic levers, 14 collapsing length on handle 16.
The upper former and lower former 9 are connected by four supporting rods 11 parallel to each other, and four supporting rods 11 press rectangle Arrangement, 11 upper end of supporting rod are connect with upper former inner top surface, and 11 lower end of supporting rod is connect with lower former inner bottom surface;The upper former 12 are equipped with handgrip above, and 12 inner top surface of upper former is equipped with multiple inner bolt holes 17, and 17 side of inner bolt hole is equipped with solid slug 18, inner bolt hole 17 or solid slug 18 connect with handgrip by screw, inner bolt hole 17 and solid slug 18 are respectively positioned in vacancy section 13.
9 following four corners of lower former is equipped with dismountable mounting base 4, and 4 lower end of mounting base is equipped with dismountable universal Single-wheel 5,4 upper end of mounting base are equipped with the backplate 3 for being located at 9 rear side of lower former, and collecting part 1 and 3 rear side of backplate flush;The lower former Middle part is equipped with solid seat 7 on rear side of 9 inner bottom surfaces, and 7 both ends of solid seat are equipped with hollow connecting pole 8, one three section telescopic lever 14 Lower end is located inside a connecting pole 8, and three section 14 lower ends of telescopic lever are connect by screw with solid seat 7, under solid seat 7 is located at In vacancy section 6.
9 edge of lower former is equipped with and is upturned and the arc bound edge 10 Jing Guo solid processing.
The mounting base 4 is connect by screw with lower former 9.
The three sections telescopic lever 14 is aluminum alloy material.
The supporting rod 11 is made of glass fiber rod.
In implementation process, which is reduced to existing flight case inner support on the skeleton of only upper former 12 and lower former 9 Structure is connected with supporting rod 11 between upper former 12 and lower former 9, can meet moulding and support function, while can also reduce The usage amount of raw material, effectively reduces the overall weight of flight case.In use, the button latch on handle 16 is pressed 15 can be adjusted the length of three section telescopic levers 14, and adjusting rear release button lock 15 can stretching three section telescopic levers 14 Long status is fixed.
For inner bolt hole 17 in upper vacancy section 13 with solid slug 18 together with, inner bolt hole 17 or solid slug 18 pass through screw It is connect with the handgrip above upper former 12, the error during manual operation mould assembling can be avoided, handgrip is enable to be more prone to Be fixed on above former 12.
The mainly wheel of serious wear during flight case use, the universal single-wheel 5 of the device and mounting base 4 are all can Dismounting, it is replaced convenient for the universal single-wheel 5 to damage, effectively extends the service life of flight case.
3 rear side of backplate of 4 upper end of collecting part 1 and mounting base flushes, and collecting part 1 and two backplates 3 of rear side is made to form one The firm support construction of a triangle, being in direct contact with ground when flight case can be avoided to keep flat causes to wear.
The solid seat 7 of lower 9 inner bottom surface of former is located in lower vacancy section 6, and one three 14 lower end of section telescopic lever is fixed on reality In the connecting pole 8 of 7 one end of heart seat, to reduce using the impact to lower former 9 during pull rod, keep 9 stress of lower former relatively equal Even, preventing strength from excessively concentrating makes lower former 9 damage.
The arc bound edge 10 at lower 9 edge of former is upturned and passes through solid processing, can enhance the strong of 9 edge of lower former Degree, in case 9 edge stress of lower former is damaged.
It is light and secured using supporting rod made of glass fiber rod 11, is conducive to drop under the premise of ensureing skeleton stability Its low weight.
The above embodiment is used for illustrating the utility model, rather than limits the utility model, in this reality With in novel spirit and scope of the claims, to any modifications and changes that the utility model is made, this is both fallen within The protection domain of utility model.

Claims (5)

1. a kind of flight case inner support skeleton structure, it is characterised in that:Three sections including upper former, lower former and two side by side are flexible Pull rod, three section telescopic lever lower ends are connect with lower former inner bottom surface, and upper former is equipped with upper vacancy section, and lower former, which is equipped with down, to be engraved Dead zone, upper former and lower former are all made of rigid plastics and are made;Middle part is equipped with collecting part on rear side of the upper former, and three sections are flexible to be drawn Bar upper end passes through collecting part, three section telescopic lever upper ends to be equipped with handle, is equipped with recessed above upper former and can accommodate handle Position is stored, is connect respectively with one three section telescopic lever upper end on the downside of handle both ends, Middle face is equipped with for fixing three on handle Save the button latch of telescopic lever collapsing length;
The upper former is connected with lower former by four supporting rods parallel to each other, and four supporting rods press rectanglar arrangement, support Bar upper end is connect with upper former inner top surface, and supporting rod lower end is connect with lower former inner bottom surface;Handgrip is equipped with above the upper former, Upper former inner top surface is equipped with multiple inner bolt holes, and inner bolt hole side is equipped with solid slug, and inner bolt hole or solid slug pass through screw and handgrip Connection, inner bolt hole and solid slug are respectively positioned in vacancy section;
The lower former following four corners is equipped with dismountable mounting base, and mounting base lower end is equipped with dismountable universal single-wheel, peace It fills seat upper end and is equipped with the backplate being located on rear side of lower former, flushed on rear side of collecting part and backplate;In on rear side of the lower former inner bottom surface Portion is equipped with solid seat, and solid seat both ends are equipped with hollow connecting pole, and one three section telescopic lever lower end is located at a connecting pole Inside, three section telescopic lever lower ends are connect by screw with solid seat, and solid seat is located in lower vacancy section.
2. flight case inner support skeleton structure according to claim 1, it is characterised in that:The lower former edge is equipped with upward Tilting and the arc bound edge Jing Guo solid processing.
3. flight case inner support skeleton structure according to claim 1, it is characterised in that:The mounting base is by screw under Former connects.
4. flight case inner support skeleton structure according to claim 1, it is characterised in that:The three section telescopic lever closes for aluminium Golden material.
5. flight case inner support skeleton structure according to claim 1, it is characterised in that:The supporting rod uses glass fiber rod system At.
CN201820367582.0U 2018-03-19 2018-03-19 A kind of flight case inner support skeleton structure Active CN208080709U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820367582.0U CN208080709U (en) 2018-03-19 2018-03-19 A kind of flight case inner support skeleton structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820367582.0U CN208080709U (en) 2018-03-19 2018-03-19 A kind of flight case inner support skeleton structure

Publications (1)

Publication Number Publication Date
CN208080709U true CN208080709U (en) 2018-11-13

Family

ID=64059135

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820367582.0U Active CN208080709U (en) 2018-03-19 2018-03-19 A kind of flight case inner support skeleton structure

Country Status (1)

Country Link
CN (1) CN208080709U (en)

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Effective date of registration: 20220810

Address after: No. 55, Jinshan Road, Xiaowutang, Lingyuan Street, Jinjiang City, Quanzhou City, Fujian Province, 362200

Patentee after: Fujian Jinjiang Taixiang Technology Co., Ltd.

Address before: No. 48, Tengfei 3rd Road, Southwest Airport Economic Development Zone, Shuangliu, Chengdu, Sichuan 610207

Patentee before: SICHUAN ADMIRE LEATHER & FASHION CO.,LTD.