CN207104857U - The total assembling platform of superposing type in aircraft cabin - Google Patents
The total assembling platform of superposing type in aircraft cabin Download PDFInfo
- Publication number
- CN207104857U CN207104857U CN201720486316.5U CN201720486316U CN207104857U CN 207104857 U CN207104857 U CN 207104857U CN 201720486316 U CN201720486316 U CN 201720486316U CN 207104857 U CN207104857 U CN 207104857U
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- platform
- aircraft cabin
- mounting plate
- superposing type
- total assembling
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Abstract
The utility model provides the total assembling platform of superposing type in a kind of aircraft cabin, lower platform is hung in inside nacelle by driving during use, lower platform is connected with 3 upper mounting plates with fastener, is connected upper mounting plate with upper support member with fastener.The total assembling platform up and down of the passage inside lower platform can be passed through, the operation in nacelle primary module can be realized when operating personnel are located at lower platform, the operation of nacelle inwall can be realized during positioned at upper mounting plate, solves the problems, such as that general assembly operation can not safe and reliable implementation in certain aircraft cabin.
Description
Technical field
It the utility model is related to the total assembling platform of superposing type in a kind of aircraft cabin.
Background technology
The below deck equipment of existing section structure and pipeline general assembly need total assembling platform in a kind of special cabin to be protected as production
Barrier, to ensure the reliability and safety of general assembly process, conventional ladder in the market can not meet requirements above.
Utility model content
In order to solve the below deck equipment of certain section structure and pipeline general assembly process safe operation process is ensured without dedicated platform
The problem of reliable, the purpose of this utility model are to provide the total assembling platform of superposing type in a kind of aircraft cabin, to ensure that general assembly is grasped
Make the safe and reliable of process.
The utility model discloses superposing type general assembly platform structure in a kind of aircraft cabin, including：Lower platform, upper mounting plate, on
Support member.
Wherein, lower platform is cylindrical structural, and structure bottom has 12 support feets, and support feet can realize leveling；In structure
Portion is platform, and axis position is entrance downwards in platform, and there is foot-operated ladder porch；Have the first of uniform one week on the outside of structure upper
Through hole, for being connected with upper mounting plate；There are 3 uniform suspension centres on the inside of structure upper, for lifting by crane.
Upper mounting plate is frame structure, and side upper end is welded with metal derby with side lower end, has uniform second logical on metal derby
Hole, through hole are used for the connection with lower platform and upper supporting piece；Different through hole connections may be selected, realize upper mounting plate and lower platform,
The relative position change of upper support member.
Upper supporting piece is triangle mount structure, two uniform third through-holes of rod member of side, for being connected with upper mounting plate.This reality
The total assembling platform of superposing type in a kind of aircraft cabin is provided with new, and lower platform, upper mounting plate, upper support member are passed through into screw during use
Connection, whole utilization driving lifting are put into cabin, have reached safe and reliable operating effect.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the total assembling platform of superposing type in aircraft cabin；
Fig. 2 is the structural representation of the lower platform of the utility model one embodiment；
Fig. 3 is the structural representation of the upper mounting plate of the utility model one embodiment；
Fig. 4 is the structural representation of the upper support member of the utility model one embodiment.
Embodiment
To enable above-mentioned purpose of the present utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings and tool
Body embodiment is described in further detail to the utility model.
As shown in figures 1-4, the total assembling platform of superposing type in a kind of aircraft cabin of the utility model offer, including lower platform 1,
Upper mounting plate 2 and upper support member 3, wherein,
The lower platform 2 is cylindrical structure, and the structure bottom has support feet, and support feet can realize leveling；
Be platform in the middle part of the structure, axis position be entrance downwards in the platform, porch be provided with ride it is terraced；
There is the first through hole of uniform one week on the outside of the structure upper, for being connected with the upper mounting plate；
The upper mounting plate 2 is frame structure, and side upper end is welded with metal derby with side lower end, there is uniform the on metal derby
Two through holes, second through hole are used to be connected with lower platform 1 and upper support member 3 respectively；
The upper support member 3 is triangle mount structure, two uniform third through-holes of rod member of the upper support member side, for
Platform connects.
In the aircraft cabin of the embodiment of the utility model one in the total assembling platform of superposing type, the quantity of the support feet is 12
It is individual.
In the aircraft cabin of the embodiment of the utility model one in the total assembling platform of superposing type, also set up on the inside of the structure upper
There are 3 uniform suspension centres, for lifting by crane.
In the aircraft cabin of the embodiment of the utility model one in the total assembling platform of superposing type, by select diverse location second
Through hole, the relative position change that adjustment upper mounting plate is connected with lower platform, upper support member.
In the aircraft cabin of the embodiment of utility model one in the total assembling platform of superposing type, the quantity of the upper mounting plate is 3.
Specifically, as shown in figure 1, lower platform 1 is hung in inside nacelle by driving using when, with fastener by lower platform
1 and 3 upper mounting plate 2 connects at b, is connected upper mounting plate 2 and upper support member 3 at a with fastener.Can be by lower platform 1
The passage in portion total assembling platform up and down, the operation in nacelle primary module can be realized when operating personnel are located at lower platform 1, positioned at upper flat
The operation of nacelle inwall can be realized during platform 2, is solved
In certain aircraft cabin general assembly operation can not safe and reliable implementation the problem of.
The utility model provides the total assembling platform of superposing type in a kind of aircraft cabin, during use by lower platform, upper mounting plate, on
Support member is connected by screw, and whole utilization driving lifting is put into cabin, has reached safe and reliable operating effect.
In order to solve the below deck equipment of certain section structure and pipeline general assembly process safe operation process is ensured without dedicated platform
The problem of reliable, the purpose of this utility model are to provide the total assembling platform of superposing type in a kind of aircraft cabin, to ensure that general assembly is grasped
Make the safe and reliable of process.
The utility model provides the total assembling platform of superposing type in a kind of aircraft cabin, during use by lower platform, upper mounting plate, on
Support member is connected by screw, and whole utilization driving lifting is put into cabin, has reached safe and reliable operating effect.
Each embodiment is described by the way of progressive in this specification, what each embodiment stressed be and other
The difference of embodiment, between each embodiment identical similar portion mutually referring to.
Obviously, it is new without departing from this practicality can to carry out various changes and modification to utility model by those skilled in the art
The spirit and scope of type.So, if these modifications and variations of the present utility model belong to the utility model claims and its
Within the scope of equivalent technologies, then the utility model is also intended to include these changes and modification.
Claims (6)
- A kind of 1. total assembling platform of superposing type in aircraft cabin, it is characterised in that including lower platform, upper mounting plate and upper support member, wherein, The lower platform is cylindrical structure, and the structure bottom has support feet, and support feet can realize leveling；Be platform in the middle part of the structure, axis position be entrance downwards in the platform, porch be provided with ride it is terraced；There is the first through hole of uniform one week on the outside of the structure upper, for being connected with the upper mounting plate；The upper mounting plate is frame structure, and side upper end is welded with metal derby with side lower end, has uniform second logical on metal derby Hole, second through hole are used to be connected with lower platform (1) and upper support member (3) respectively；The upper support member is triangle mount structure, two uniform third through-holes of rod member of the upper support member side, is used for and upper mounting plate Connection.
- 2. the total assembling platform of superposing type in aircraft cabin as claimed in claim 1, it is characterised in that the quantity of the support feet is 12.
- 3. the total assembling platform of superposing type in aircraft cabin as claimed in claim 1, it is characterised in that on the inside of the structure upper also It is provided with uniform suspension centre.
- 4. the total assembling platform of superposing type in aircraft cabin as claimed in claim 3, it is characterised in that the quantity of the suspension centre is 3 It is individual.
- 5. the total assembling platform of superposing type in aircraft cabin as claimed in claim 1, it is characterised in that by selecting diverse location Second through hole, the relative position change that adjustment upper mounting plate is connected with lower platform, upper support member.
- 6. the total assembling platform of superposing type in the aircraft cabin as described in any one of claim 1 to 5, it is characterised in that described flat The quantity of platform is 3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720486316.5U CN207104857U (en) | 2017-05-04 | 2017-05-04 | The total assembling platform of superposing type in aircraft cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720486316.5U CN207104857U (en) | 2017-05-04 | 2017-05-04 | The total assembling platform of superposing type in aircraft cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207104857U true CN207104857U (en) | 2018-03-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720486316.5U Active CN207104857U (en) | 2017-05-04 | 2017-05-04 | The total assembling platform of superposing type in aircraft cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207104857U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110803294A (en) * | 2019-11-08 | 2020-02-18 | 上海航天设备制造总厂有限公司 | Enclosed cylinder type aircraft structure cabin body general assembly operating platform |
-
2017
- 2017-05-04 CN CN201720486316.5U patent/CN207104857U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110803294A (en) * | 2019-11-08 | 2020-02-18 | 上海航天设备制造总厂有限公司 | Enclosed cylinder type aircraft structure cabin body general assembly operating platform |
| CN110803294B (en) * | 2019-11-08 | 2023-02-10 | 上海航天设备制造总厂有限公司 | Enclosed cylinder type aircraft structure cabin body general assembly operating platform |
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