CN107877199A - A kind of space shuttle undercarriage processes clamper - Google Patents
A kind of space shuttle undercarriage processes clamper Download PDFInfo
- Publication number
- CN107877199A CN107877199A CN201711074233.6A CN201711074233A CN107877199A CN 107877199 A CN107877199 A CN 107877199A CN 201711074233 A CN201711074233 A CN 201711074233A CN 107877199 A CN107877199 A CN 107877199A
- Authority
- CN
- China
- Prior art keywords
- guide cylinder
- clamp assemblies
- undercarriage
- arc holder
- space shuttle
- Prior art date
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
- B23Q3/06—Work-clamping means
- B23Q3/062—Work-clamping means adapted for holding workpieces having a special form or being made from a special material
Abstract
A kind of space shuttle undercarriage processes clamper, mainly include clamp assemblies, the lower end of the clamp assemblies is provided with thread bush, connecting bolt is installed on the clamp assemblies, the clamp assemblies include left half and half, the right side, the upper end of the clamp assemblies is provided with arc holder, deformation block is provided with the arc holder, the upper end of the arc holder is provided with guide cylinder, the upper end of the arc holder is arranged on the downside of guide cylinder, the guide cylinder is provided with locating piece, and the left side of the guide cylinder is provided with L-shaped positive stop strip.By setting clamp assemblies, arc holder and guide cylinder not only to contribute to, undercarriage base clamps the present invention and its middle part position clamps and increases to grip effect but also contribute to undercarriage to be oriented to and installs, and simple in construction, easy to operate, economical and practical.
Description
Technical field
The present invention relates to space equipment device design technical field, more particularly to a kind of processing clamping of space shuttle undercarriage
Device.
Background technology
In recent years, international space industry starts a new round and explores upsurge, it is desirable to further grasps " secret " and money of space
Source.Various countries hurry in research and development rocket, satellite, Developing Manned Space Shuttles technology, formulate and explore the moon, Mars program, it is desirable to which " ancestor one
Step " conquers space, and none is not " without a stop ".Except that can obtain important strategic interests and economic benefit, various countries are to boat
The input in its field, also increasingly show " Megrez processed " for national security and the significance of development.Spacecraft has more
Kind sorting technique, you can be classified according to its Path Properties, scientific and technological feature, quality size, application field.Spacecraft according to
Application field carries out classification and is divided into military spacecraft, civil spacecraft and dual-use spacecraft, and these three spacecrafts can
It is divided into unmanned spacecraft and manned spacecraft.Scientific satellite is divided into space physics detection satellite and astronomical satellite.Applied satellite point
For telecommunication satellite, meteorological satellite, aeronautical satellite, geodetic satellite, earth resources satellite, reconnaissance satellite, early warning satellite, marine surveillance
Satellite, interceptor satellite and multipurpose satellite etc..Space probe is divided into lunar orbiter, planet and its satellite sensor, planet
Border detector and ASTEREX device.However, lacking on existing space shuttle undercarriage processing clamper both contributes to rise and fall
The clamping of frame base and its middle part position, which clamp and increased, grips the device that effect contributes to undercarriage to be oriented to installation again, it is impossible to
Meets the needs of actual conditions.
The content of the invention
The purpose of the present invention is：A kind of undercarriage base clamping is provided and undercarriage is oriented to the space shuttle undercarriage of installation
Process clamper.
The technical scheme is that：A kind of space shuttle undercarriage processes clamper, described mainly including clamp assemblies
The lower end of clamp assemblies is provided with thread bush, and connecting bolt, the upper end peace of the clamp assemblies are provided with the clamp assemblies
Equipped with arc holder, deformation block is provided with the arc holder, the upper end of the arc holder is provided with guide cylinder, the arc
The upper end of holder is arranged on the downside of guide cylinder, and the guide cylinder is provided with locating piece, and the left side of the guide cylinder limits provided with L-shaped
Position bar.
The arc holder is structure as a whole with guide cylinder.
The clamp assemblies include left half and half, the right side.
Shoulder hole is provided with the guide cylinder.
Beneficial effect is：
1. by setting clamp assemblies, arc holder and guide cylinder both to contribute to the clamping of undercarriage base and its middle part position
Clamp and increase and grip effect and contribute to undercarriage to be oriented to installation again, it is and simple in construction, it is easy to operate, it is economical and practical.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Embodiment
As shown in figure 1, a kind of space shuttle undercarriage processing clamper, mainly includes clamp assemblies 1, the clamp assemblies
1 lower end is provided with thread bush, and connecting bolt is provided with the clamp assemblies 1, and the clamp assemblies 1 include left half and the right side
Half, clamp assemblies 1, arc holder 2 and guide cylinder 3 had both contributed to the clamping of undercarriage base and its middle part position to clamp and increase
Grip effect contributes to undercarriage to be oriented to installation again, and the upper end of the clamp assemblies 1 is provided with arc holder 2, the arc
The lower end of clevis seat 2 is provided with thread bush.
The upper end of the arc holder 2 is provided with guide cylinder 3, and the upper end of the arc holder 2 is arranged under guide cylinder 3
Side, the guide cylinder 3 are provided with locating piece, and the left side of the guide cylinder 3 is provided with L-shaped positive stop strip, and L-shaped positive stop strip helps to be oriented to
The positioning of 3 positions of cylinder, the guide cylinder 3 is interior to be provided with shoulder hole, and the arc holder 2 is structure as a whole with guide cylinder 3.
During onsite application, device is integrally suitably positioned by operating personnel, then device is integrally fixed, you can is carried out
Space shuttle undercarriage processing clamping processing work
Above-described embodiment is intended merely to the purposes of the interpretation present invention, and is not limitation of the present invention, this technology
The those of ordinary skill in field, in the essential scope of the present invention, make a variety of changes or substitute, should also belong to the guarantor of the present invention
Protect category.
Claims (4)
1. a kind of space shuttle undercarriage processes clamper, it is characterised in that：Mainly include clamp assemblies (1), the clamping group
The lower end of part (1) is provided with thread bush, and connecting bolt, the upper end of the clamp assemblies (1) are provided with the clamp assemblies (1)
Arc holder (2) is installed, is provided with deformation block in the arc holder (2), the upper end of the arc holder (2) is provided with guiding
Cylinder (3), the upper end of the arc holder (2) are arranged on the downside of guide cylinder (3), and the guide cylinder (3) is provided with locating piece, institute
The left side for stating guide cylinder (3) is provided with L-shaped positive stop strip.
A kind of 2. space shuttle undercarriage processing clamper according to claim 1, it is characterised in that：The arc holder
(2) it is structure as a whole with guide cylinder (3).
A kind of 3. space shuttle undercarriage processing clamper according to claim 1, it is characterised in that：The clamp assemblies
(1) left half and half, the right side are included.
A kind of 4. space shuttle undercarriage processing clamper according to claim 1, it is characterised in that：The guide cylinder
(3) shoulder hole is provided with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711074233.6A CN107877199A (en) | 2017-11-05 | 2017-11-05 | A kind of space shuttle undercarriage processes clamper |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711074233.6A CN107877199A (en) | 2017-11-05 | 2017-11-05 | A kind of space shuttle undercarriage processes clamper |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107877199A true CN107877199A (en) | 2018-04-06 |
Family
ID=61778579
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711074233.6A Withdrawn CN107877199A (en) | 2017-11-05 | 2017-11-05 | A kind of space shuttle undercarriage processes clamper |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107877199A (en) |
-
2017
- 2017-11-05 CN CN201711074233.6A patent/CN107877199A/en not_active Withdrawn
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180406 |