CN211336405U - Boarding gate - Google Patents
Boarding gate Download PDFInfo
- Publication number
- CN211336405U CN211336405U CN201921919501.4U CN201921919501U CN211336405U CN 211336405 U CN211336405 U CN 211336405U CN 201921919501 U CN201921919501 U CN 201921919501U CN 211336405 U CN211336405 U CN 211336405U
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- China
- Prior art keywords
- shaped piece
- inner basin
- gate
- outer skin
- basin
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Abstract
The utility model belongs to the small-size aircraft hatch door field, concretely relates to gate of boarding. The inner basin-shaped piece is provided with a reinforcing socket, the bottom surface of the reinforcing socket is tightly attached and fixed with the outer skin, the inner basin-shaped piece is provided with a plurality of through holes, and the thickness of the inner basin-shaped piece is gradually increased from the center to the periphery. In the technical scheme, the reinforcing pit is arranged on the inner basin-shaped piece, so that the outer skin and the inner basin-shaped piece are integrated, the rigidity of the boarding door is greatly improved, and the safety of the flight process is ensured.
Description
Technical Field
The utility model belongs to the small-size aircraft hatch door field, concretely relates to gate of boarding.
Background
In the flying process of the airplane, the special environment of the airplane has higher requirement on the strength resistance of the gate, however, at present, the gate of the small airplane consists of an outer skin and an inner basin-shaped part, and the inside of the gate is hollow, so that the outer skin is easily sunken or even damaged, and great potential safety hazard is brought to the flying process.
Disclosure of Invention
The utility model aims at: a gate is provided to overcome the above-mentioned deficiencies of the prior art.
The utility model discloses the technical solution who adopts is:
the utility model provides a gate, includes outer covering and interior basin piece, outer covering upper portion sets up ventilation window, its characterized in that: and the inner basin-shaped piece is provided with a reinforcing socket, and the bottom surface of the reinforcing socket is tightly attached and fixed with the outer skin.
Further, a plurality of through holes are formed in the inner basin.
Furthermore, the outer peripheral edge of the inner basin-shaped piece is provided with a sealing strip, and the sealing strip is made of sponge rubber materials.
Furthermore, an upper hinge and a lower hinge are arranged on the outer side of the edge of the outer skin, the upper hinge is close to the ventilation window, and the lower hinge is located near a round angle of the front lower portion of the outer skin.
Further, the thickness of the inner basin-shaped piece is gradually increased from the center to the periphery.
The utility model has the advantages that: in the technical scheme, the reinforcing pit is arranged on the inner basin-shaped piece, so that the outer skin and the inner basin-shaped piece are integrated, the rigidity of the boarding door is greatly improved, and the safety of the flight process is ensured.
Drawings
FIG. 1 is a schematic structural view of the outer side of a gate;
FIG. 2 is a schematic view of the inside side of the gate;
FIG. 3 is a schematic view of the positional relationship of the sealing band to the inner basin.
In the figure, 1-outer skin, 2-inner basin, 3-ventilation window, 4-upper hinge, 5-lower hinge, 6-sealing belt, 7-through hole, 8-reinforcing nest.
Detailed Description
The technical solution of the present invention will be clearly and completely described below with reference to the accompanying drawings of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1 to 3, the present embodiment provides a gate, which mainly comprises an outer skin 1, an inner basin-shaped member 2, a ventilation window 3, a hinge, a sealing tape 6, and the like.
The outer skin and the inner basin-shaped piece are frameworks of the gate, and as the lock mechanism is positioned between the inner basin-shaped piece and the outer skin, 3 through holes are formed in the inner basin-shaped piece to serve as passages for mechanism installation and maintenance, and meanwhile, the basin-shaped piece is also reinforced around the perforated area. In order to improve the rigidity of the door, a circular reinforcing socket is designed in the middle of the inner basin-shaped piece, and the bottom surface of the reinforcing socket is tightly attached to the outer skin and riveted with the outer skin to form a whole.
The appearance around the gate is relatively straight, so that the gate is suitable for adopting an external hinge. According to the size and the weight of the door, two hinges are arranged for the boarding door, the upper hinge 4 is close to the ventilation window, and the lower hinge 5 is located near a round angle at the front lower part of the outer skin. In order to further improve the stability of the boarding door, the hinge axis is close to the appearance of the machine body in front of the boarding door, the intersection point of the upper hinge plane and the hinge axis is 4.9 mm far away from the theoretical appearance of the machine body, and the intersection point of the lower hinge plane and the hinge axis is 9.5 mm far away from the theoretical appearance of the machine body. The hinge connected to one side of the cabin door is formed by bending a stainless steel plate, and the part connected to one side of the cabin body is a stainless steel machining part.
In order to prevent the entry of rainwater and to ensure that the boarding door is not ventilated all around during flight, sealing strips are arranged on the periphery of the door. The sealing tape is made of sponge rubber material, the material has larger compression deformation and good rebound resilience, and can effectively meet the sealing requirements of different parts of the circumference of the cabin door. The sealing strip is bonded at the round angle of the periphery of the basin-shaped piece through adhesive.
In order to reduce the processing cost of the inner basin-shaped part, the material is changed from aluminum alloy into composite material, the part thicknesses are different in different regions, the thickness of the central region is 0.964 mm, the thickness of the outermost ring region is 1.446 mm, and the thickness of a transition region sandwiched between the two regions is 1.205 mm.
The above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present invention, and the changes or substitutions should be covered within the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (3)
1. The utility model provides a gate, includes outer covering and interior basin piece, outer covering upper portion sets up ventilation window, its characterized in that: the inner basin-shaped piece is provided with a reinforcing socket, the bottom surface of the reinforcing socket is tightly attached and fixed with the outer skin, the inner basin-shaped piece is provided with a plurality of through holes, and the thickness of the inner basin-shaped piece is gradually increased from the center to the periphery.
2. The gate of claim 1, wherein: the outer periphery of the inner basin-shaped piece is provided with a sealing strip which is made of sponge rubber.
3. The gate of claim 1, wherein: and an upper hinge and a lower hinge are arranged on the outer side of the edge of the outer skin, the upper hinge is close to the ventilation window, and the lower hinge is positioned near a round angle of the front lower part of the outer skin.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921919501.4U CN211336405U (en) | 2019-11-08 | 2019-11-08 | Boarding gate |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921919501.4U CN211336405U (en) | 2019-11-08 | 2019-11-08 | Boarding gate |
Publications (1)
Publication Number | Publication Date |
---|---|
CN211336405U true CN211336405U (en) | 2020-08-25 |
Family
ID=72128145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201921919501.4U Active CN211336405U (en) | 2019-11-08 | 2019-11-08 | Boarding gate |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN211336405U (en) |
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2019
- 2019-11-08 CN CN201921919501.4U patent/CN211336405U/en active Active
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