CN204868703U - Switching frock of carrier rocket supporting cabin installation - Google Patents
Switching frock of carrier rocket supporting cabin installation Download PDFInfo
- Publication number
- CN204868703U CN204868703U CN201520262285.6U CN201520262285U CN204868703U CN 204868703 U CN204868703 U CN 204868703U CN 201520262285 U CN201520262285 U CN 201520262285U CN 204868703 U CN204868703 U CN 204868703U
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- China
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- tenon
- carrier rocket
- supporting cabin
- switching tooling
- connecting rod
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Abstract
The utility model relates to a switching frock of carrier rocket supporting cabin installation can simplify the butt joint procedure that the star covers assembly and rocket powder level, is convenient for support the moment of deciding of installing in the cabin and implements, optimizes carrier rocket launching site work flow.
Description
Technical field
The utility model relate to one be applied to carrier rocket supporting cabin install, by with existing assembly wrench with the use of, can installation be simplified, be convenient to simultaneously moment implement, be applicable to carrier rocket supporting cabin install.
Background technology
At present, domestic carrier rocket generally adopts satellite and satellite fairing assembly to dock with rocket powder level.Concrete docking operation is: first carry out supporting cabin and dock with rocket powder level, then carries out satellite fairing lower end frame, supporting cabin, the docking of rocket powder level.Wherein supporting cabin and rocket powder level docking operation operate in satellite fairing, and because supporting cabin is pyramidal structure, limit by satellite fairing sidewall, operating space is very limited, causes installing more difficult (installing and using spanner 4), and the set-up time is longer; Meanwhile, each connecting portion of carrier rocket all has determines moment installation requirement, and the handle of spanner is interferenceed current assembly wrench 4 and implemented very difficult with supporting cabin conical surface stringer, and scheme of installation as shown in Figure 1.
Therefore, the utility model provides a kind of switching tooling supporting cabin and install in satellite fairing, is convenient to the installation in supporting cabin and determines moment enforcement.
Summary of the invention
The purpose of this utility model is to provide the switching tooling that a kind of carrier rocket supporting cabin is installed, the docking procedure of star cover assembly and rocket powder level can be simplified, the difficult problem that the handle solving spanner is interferenceed with supporting cabin conical surface stringer is convenient to support the enforcement of installing and determining moment in cabin, optimizes launch-vehicle site workflow.
For achieving the above object, the utility model provides a kind of switching tooling, comprises foreign side's tenon, connecting rod and Nei Fang tenon; The spanner that the size of described foreign side tenon is connected by it or sleeve are determined; The bottle opener chieftain that the size of described interior side's tenon is connected by it determines.Described foreign side tenon, connecting rod and Nei Fang tenon are in turn connected into switching tooling, and described switching tooling is higher than radome fairing sidewall middle boxes and lower than satellite bottom.Wherein, connecting rod is generally cylindrical.
The switching tooling that a kind of carrier rocket supporting cabin that the utility model provides is installed and existing assembly wrench with the use of, for supporting the installation in cabin and determining moment enforcement, solve narrow space between satellite fairing with supporting cabin limit and operate and handle and the difficult problem supporting cabin conical surface stringer and interference, shorten the docking time of carrier rocket at launching site.
Accompanying drawing explanation
Fig. 1 is scheme of installation of the prior art, and wherein 4 is spanner;
Fig. 2 is the switching tooling schematic diagram in the utility model; Wherein, 1 is foreign side's tenon; 2 is connecting rod; 3 is interior side's tenon;
Fig. 3 is the scheme of installation in the utility model.
Detailed description of the invention
The utility model provides a kind of switching tooling, comprises foreign side's tenon 1, connecting rod 2 and Nei Fang tenon 3, and the size of foreign side's tenon 1 and Nei Fang tenon 3 is all adjustable; Described foreign side tenon 1 regulates size according to the spanner connected or sleeve; Described interior side's tenon 3 regulates size according to the bottle opener connected.Described foreign side tenon 1, connecting rod 2 and Nei Fang tenon 3 are in turn connected into switching tooling, and described switching tooling is higher than radome fairing sidewall middle boxes and lower than satellite bottom.Wherein, connecting rod 2 is generally cylindrical.
Below in conjunction with Fig. 1 ~ 3, describe a preferred case study on implementation of the present utility model in detail.
As shown in Fig. 1 ~ 3, because supporting cabin is pyramidal structure, limits simultaneously, need carry out during installation in narrow space by satellite fairing sidewall, operating personnel's working strength is large, and the set-up time is long.
Preferably, a kind of length that the utility model is preferred is the switching tooling of 300mm, described switching tooling comprises foreign side's tenon 1, connecting rod 2 and Nei Fang tenon 3, foreign side's tenon 1 connects external key or sleeve, its size and spanner or sleeve match, and interior side's tenon 3 connects outside bottle opener, and its size and bottle opener match, described foreign side tenon 1, connecting rod 2 and Nei Fang tenon 3 are in turn connected into switching tooling, and described switching tooling is higher than radome fairing sidewall middle boxes and lower than satellite bottom.So, as shown in Figure 3, operating personnel need not bend over to carry out, and avoid the difficult problem that the space of supporting cabin lower narrow and handle are interferenceed with supporting cabin conical surface stringer, greatly reduce working strength, the set-up time is reduced therefore efficiency significantly and is greatly improved; Meanwhile, because space is discharged, the moment of determining being convenient to each connecting portion is implemented, and ensure that the reliability of connecting portion to a certain extent.
Although content of the present utility model be have been introduced by above preferred embodiment, will be appreciated that above-mentioned description should not be considered to restriction of the present utility model.After those skilled in the art have read foregoing, for multiple amendment of the present utility model and substitute will be all apparent.Therefore, protection domain of the present utility model should be limited to the appended claims.
Claims (3)
1. the switching tooling of a carrier rocket supporting cabin installation, comprise foreign side's tenon [1], connecting rod [2] and interior side's tenon [3], it is characterized in that, described foreign side tenon [1], connecting rod [2] and interior side's tenon [3] are in turn connected into switching tooling, and described switching tooling is higher than radome fairing sidewall middle boxes and lower than satellite bottom.
2. the switching tooling of a kind of carrier rocket supporting cabin installation according to claim 1, it is characterized in that, described connecting rod [2] is for cylindrical.
3. the switching tooling installed of a kind of carrier rocket supporting cabin according to claim 1, is characterized in that, the spanner that the size of described foreign side tenon [1] is connected by it or sleeve are determined; The bottle opener that the size of described interior side's tenon [3] is connected by it is determined.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520262285.6U CN204868703U (en) | 2015-04-28 | 2015-04-28 | Switching frock of carrier rocket supporting cabin installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520262285.6U CN204868703U (en) | 2015-04-28 | 2015-04-28 | Switching frock of carrier rocket supporting cabin installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204868703U true CN204868703U (en) | 2015-12-16 |
Family
ID=54813124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520262285.6U Active CN204868703U (en) | 2015-04-28 | 2015-04-28 | Switching frock of carrier rocket supporting cabin installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204868703U (en) |
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2015
- 2015-04-28 CN CN201520262285.6U patent/CN204868703U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |