CN202689763U - Boarding gate hinge structure - Google Patents
Boarding gate hinge structure Download PDFInfo
- Publication number
- CN202689763U CN202689763U CN 201220086911 CN201220086911U CN202689763U CN 202689763 U CN202689763 U CN 202689763U CN 201220086911 CN201220086911 CN 201220086911 CN 201220086911 U CN201220086911 U CN 201220086911U CN 202689763 U CN202689763 U CN 202689763U
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- China
- Prior art keywords
- hinge
- door
- doorframe
- door frame
- hole
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- 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 - Lifetime
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Abstract
The utility model relates to the machinery field and provides a boarding gate hinge structure which comprises an upper doorframe hinge, a lower doorframe hinge and a door hinge between the two doorframe hinges, wherein through holes in the upper doorframe hinge and the lower doorframe hinge are designed to be round-shaped, a through hole in the door frame hinge are ellipse-shaped, and a door shaft of a cabin door penetrates through the through hole of the upper doorframe hinge, the through hole of the boarding door hinge and the through hole of the lower doorframe hinge sequentially in a vertical direction. Due to the fact that the through holes of the upper doorframe hinge and the lower doorframe hinge are designed to be round-shaped, the possibility that the door shaft tilts in the direction of a long shaft of the upper and lower ellipse through holes can be avoided, and the problem that poor assembly tightness of a boarding gate caused by the fall-down boarding gate can be solved.
Description
Technical field
The utility model relates to mechanical field, relates in particular to a kind of landing gate hinge arrangement.
Background technology
Existing airframe landing gate and doorframe hinge structure are as shown in Figure 1, door hinge is clipped in up and down between two door frame hinges, in order to guarantee between door and doorframe, to possess activity degree of exceeding, the via design ovalisation on the door frame hinge up and down, through hole on the door frame hinge is circular, the hatch door door-hinge passes upper door frame hinge vias, landing gate hinge vias, lower door frame hinge vias in the vertical direction successively, realizes rotating.
Shown in Fig. 2,3, when assembling, landing gate falls under an end occurring door under the Action of Gravity Field at (or in opening process) after the unlatching, the problem such as poor sealing when closing, thus affected landing gate erection quality.
The utility model content
The technical problems to be solved in the utility model: the utility model provides a kind of landing gate hinge arrangement, effectively overcomes the landing gate fitting tight problem of poor of falling to bring under the landing gate.
The technical solution of the utility model: a kind of landing gate hinge arrangement, comprise: up and down two door frame hinges and between a door hinge, wherein, via design on the door frame hinge is circular up and down, through hole on the door frame hinge is oval, and the hatch door door-hinge passes upper door frame hinge vias, landing gate hinge vias, lower door frame hinge vias in the vertical direction successively.
The beneficial effects of the utility model: the via design on the door frame hinge is circular up and down, avoided door-hinge elliptical hole long axis direction up and down occur tilting may, effectively overcome the landing gate fitting tight problem of poor of falling to bring under the landing gate.
Description of drawings
Fig. 1 disassembles schematic diagram for having airframe landing gate and doorframe hinge structure now.
Fig. 2 is for falling schematic diagram under the existing airframe landing gate.
Fig. 3 is combined schematic diagram for existing airframe landing gate with doorframe hinge structure.
Fig. 4 is that the utility model airframe landing gate is combined schematic diagram with doorframe hinge structure.
The specific embodiment
Landing gate hinge arrangement of the present utility model, comprise: up and down two door frame hinges and between a door hinge, wherein, via design on the door frame hinge is circular up and down, through hole on the door frame hinge is oval, and the hatch door door-hinge passes upper door frame hinge vias, landing gate hinge vias, lower door frame hinge vias in the vertical direction successively.
As shown in Figure 4, the landing gate hinge arrangement improves, make the landing gate width in the whole motion process of landing gate, be in mated condition (being about to the slotted hole design is changed in the door hinge top connection by doorframe) with slotted hole all the time, via design on the door frame hinge is circular up and down, avoided door-hinge elliptical hole long axis direction up and down occur tilting may, effectively overcome the landing gate fitting tight problem of poor of falling to bring under the landing gate.
Claims (1)
1. landing gate hinge arrangement, it is characterized in that, comprise: up and down two door frame hinges and between a door hinge, wherein, via design on the door frame hinge is circular up and down, through hole on the door frame hinge is oval, and the hatch door door-hinge passes upper door frame hinge vias, landing gate hinge vias, lower door frame hinge vias in the vertical direction successively.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220086911 CN202689763U (en) | 2012-03-09 | 2012-03-09 | Boarding gate hinge structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220086911 CN202689763U (en) | 2012-03-09 | 2012-03-09 | Boarding gate hinge structure |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202689763U true CN202689763U (en) | 2013-01-23 |
Family
ID=47545396
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201220086911 Expired - Lifetime CN202689763U (en) | 2012-03-09 | 2012-03-09 | Boarding gate hinge structure |
Country Status (1)
Country | Link |
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CN (1) | CN202689763U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105511258A (en) * | 2015-11-27 | 2016-04-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Boarding gate operating mechanism reliability test automatic control method and device |
-
2012
- 2012-03-09 CN CN 201220086911 patent/CN202689763U/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105511258A (en) * | 2015-11-27 | 2016-04-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Boarding gate operating mechanism reliability test automatic control method and device |
CN105511258B (en) * | 2015-11-27 | 2019-03-22 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of boarding gate operator reliability test autocontrol method and device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20130123 |