CN108032140A - 一种航天飞机构件生产仪器 - Google Patents

一种航天飞机构件生产仪器 Download PDF

Info

Publication number
CN108032140A
CN108032140A CN201711488589.4A CN201711488589A CN108032140A CN 108032140 A CN108032140 A CN 108032140A CN 201711488589 A CN201711488589 A CN 201711488589A CN 108032140 A CN108032140 A CN 108032140A
Authority
CN
China
Prior art keywords
machine body
regulating arm
guide rail
allowance
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Withdrawn
Application number
CN201711488589.4A
Other languages
English (en)
Inventor
覃海莲
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dongguan Leidi 3d History Numerical Control Technology Co Ltd
Dongguan City Shileidi 3D Numerical Control Technology Co Ltd
Original Assignee
Dongguan Leidi 3d History Numerical Control Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dongguan Leidi 3d History Numerical Control Technology Co Ltd filed Critical Dongguan Leidi 3d History Numerical Control Technology Co Ltd
Priority to CN201711488589.4A priority Critical patent/CN108032140A/zh
Publication of CN108032140A publication Critical patent/CN108032140A/zh
Withdrawn legal-status Critical Current

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
    • B23Q11/00—Accessories fitted to machine tools for keeping tools or parts of the machine in good working condition or for cooling work; Safety devices specially combined with or arranged in, or specially adapted for use in connection with, machine tools
    • B23Q11/10—Arrangements for cooling or lubricating tools or work
    • 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
    • B23Q11/00—Accessories fitted to machine tools for keeping tools or parts of the machine in good working condition or for cooling work; Safety devices specially combined with or arranged in, or specially adapted for use in connection with, machine tools
    • B23Q11/12—Arrangements for cooling or lubricating parts of the machine
    • B23Q11/126—Arrangements for cooling or lubricating parts of the machine for cooling only
    • 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
    • B23Q17/00—Arrangements for observing, indicating or measuring on machine tools
    • B23Q17/20—Arrangements for observing, indicating or measuring on machine tools for indicating or measuring workpiece characteristics, e.g. contour, dimension, hardness

Abstract

本发明涉及一种航天飞机构件生产仪器，包括机床本体，所述机床本体上侧加工台上安装有加工余量检测器、导轨、调节臂和冷却液箱，所述加工余量检测器、导轨和调节臂均通过螺栓安装在机床本体，加工余量检测器的两端通过钢丝绳还安装在机床本体侧板上，所述加工余量检测器、导轨和调节臂与机床本体上均设有装饰涂层，所述机床本体上安装有支腿。本发明通过设置机床本体和冷却液箱有助于安装辅助生产器械及存储供给冷却液，通过设置加工余量检测器、导轨和调节臂有助于安装加工余量检测传感器、移动导向部件的位置并调节调节臂上辅助测量仪器的位置。

Description

一种航天飞机构件生产仪器
技术领域
本发明涉及航天设备器械设计技术领域，尤其涉及一种航天飞机构件生产仪器。
背景技术
近年来，国际航天领域掀起新一轮探索热潮，希望进一步掌握太空的 “机密”和资源。各国忙着研发火箭、卫星，发展载人航天技术，制定探索月球、火星计划，想要“先人一步”征服太空，无一不是“马不停蹄”。除了能够获取重要的战略利益和经济效益，各国对航天领域的投入，也越来越显示出“制天权”对于国家安全和发展的重要意义。航天器具有多种分类方法，即可以按照其轨道性质、科技特点、质量大小、应用领域进行分类。航天器按照应用领域进行分类分为军用航天器、民用航天器和军民两用航天器，这三种航天器都可以分为无人航天器和载人航天器。科学卫星分为空间物理探测卫星和天文卫星。应用卫星分为通信卫星、气象卫星、导航卫星、测地卫星、地球资源卫星、侦察卫星、预警卫星、海洋监视卫星、截击卫星和多用途卫星等。空间探测器分为月球探测器、行星及其卫星探测器、行星际探测器和小行星探测器。然而，现有的航天飞机构件生产仪器上缺少有助于安装辅助生产器械及存储供给冷却液的装置，有些航天飞机构件生产仪器上缺少有助于安装加工余量检测传感器、移动导向部件的位置并调节调节臂上辅助测量仪器的位置的装置，不能满足实际情况的需求。
发明内容
本发明的目的是为了克服现有技术的不足，提供了一种航天飞机构件生产仪器。
本发明是通过以下技术方案实现：
一种航天飞机构件生产仪器，包括机床本体，所述机床本体上侧加工台上安装有加工余量检测器、导轨、调节臂和冷却液箱，所述加工余量检测器、导轨和调节臂均通过螺栓安装在机床本体，加工余量检测器的两端通过钢丝绳还安装在机床本体侧板上。
作为本发明的优选技术方案，所述加工余量检测器、导轨和调节臂与机床本体上均设有装饰涂层。
作为本发明的优选技术方案，所述机床本体上安装有支腿。
作为本发明的优选技术方案，所述冷却液箱的下端安装有输入软管。
现场使用时，操作人员将装置整体放置到合适位置，再将装置整体固定，即可进行航天飞机构件生产工作。
与现有的技术相比，本发明的有益效果是：本发明通过设置机床本体和冷却液箱有助于安装辅助生产器械及存储供给冷却液，通过设置加工余量检测器、导轨和调节臂有助于安装加工余量检测传感器、移动导向部件的位置并调节调节臂上辅助测量仪器的位置，且结构简单，操作方便，经济实用。
附图说明
图1为本发明的结构示意图。
图中：1、机床本体；2、加工余量检测器；3、导轨；4、调节臂；5、冷却液箱。
具体实施方式
为了使本发明的目的、技术方案及优点更加清楚明白，以下结合附图及实施例，对本发明进行进一步详细说明。应当理解，此处所描述的具体实施例仅仅用以解释本发明，并不用于限定本发明。
请参阅图1，图1为本发明的结构示意图。
所述一种航天飞机构件生产仪器，包括机床本体1，所述机床本体1上安装有支腿，机床本体1和冷却液箱5有助于安装辅助生产器械及存储供给冷却液，所述机床本体1上侧加工台上安装有加工余量检测器2、导轨3、调节臂4和冷却液箱5。
所述加工余量检测器2、导轨3和调节臂4均通过螺栓安装在机床本体1，加工余量检测器2的两端通过钢丝绳还安装在机床本体1侧板上，加工余量检测器2、导轨3和调节臂4有助于安装加工余量检测传感器、移动导向部件的位置并调节调节臂4上辅助测量仪器的位置，所述加工余量检测器2、导轨3和调节臂4与机床本体1上均设有装饰涂层，所述冷却液箱5的下端安装有输入软管。
现场使用时，操作人员将装置整体放置到合适位置，再将装置整体固定，即可进行航天飞机构件生产工作。
以上所述仅为本发明的较佳实施例而已，并不用以限制本发明，凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等，均应包含在本发明的保护范围之内。

Claims (4)

1.一种航天飞机构件生产仪器，其特征在于：包括机床本体（1），所述机床本体（1）上侧加工台上安装有加工余量检测器（2）、导轨（3）、调节臂（4）和冷却液箱（5），所述加工余量检测器（2）、导轨（3）和调节臂（4）均通过螺栓安装在机床本体（1），加工余量检测器（2）的两端通过钢丝绳还安装在机床本体侧板（1）上。
2.根据权利要求1所述的一种航天飞机构件生产仪器，其特征在于：所述加工余量检测器（2）、导轨（3）和调节臂（4）与机床本体（1）上均设有装饰涂层。
3.根据权利要求1所述的一种航天飞机构件生产仪器，其特征在于：所述机床本体（1）上安装有支腿。
4.根据权利要求1所述的一种航天飞机构件生产仪器，其特征在于：所述冷却液箱（5）的下端安装有输入软管。
CN201711488589.4A 2017-12-29 2017-12-29 一种航天飞机构件生产仪器 Withdrawn CN108032140A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711488589.4A CN108032140A (zh) 2017-12-29 2017-12-29 一种航天飞机构件生产仪器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711488589.4A CN108032140A (zh) 2017-12-29 2017-12-29 一种航天飞机构件生产仪器

Publications (1)

Publication Number Publication Date
CN108032140A true CN108032140A (zh) 2018-05-15

Family

ID=62098087

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711488589.4A Withdrawn CN108032140A (zh) 2017-12-29 2017-12-29 一种航天飞机构件生产仪器

Country Status (1)

Country Link
CN (1) CN108032140A (zh)

Similar Documents

Publication Publication Date Title
Cao et al. MMS observations of whistler waves in electron diffusion region
Liu et al. On the current sheets surrounding dipolarizing flux bundles in the magnetotail: The case for wedgelets
Saikin et al. The dependence on geomagnetic conditions and solar wind dynamic pressure of the spatial distributions of EMIC waves observed by the Van Allen Probes
Eastwood et al. Evidence for collisionless magnetic reconnection at Mars
Asano et al. Electron acceleration signatures in the magnetotail associated with substorms
DiBraccio et al. MAVEN observations of tail current sheet flapping at Mars
Ionescu-Kruse An exact solution for geophysical edge waves in the β-plane approximation
Jarvinen et al. Hemispheric asymmetries of the Venus plasma environment
Poh et al. Coupling between Mercury and its nightside magnetosphere: Cross‐tail current sheet asymmetry and substorm current wedge formation
Imada et al. Favorable conditions for energetic electron acceleration during magnetic reconnection in the Earth's magnetotail
Omidi et al. Foreshock bubbles at Venus: Hybrid simulations and VEX observations
Usanova et al. MMS observations of harmonic electromagnetic ion cyclotron waves
Ranquist et al. Survey of Jupiter's dawn magnetosheath using Juno
Farrugia et al. An encounter with the ion and electron diffusion regions at a flapping and twisted tail current sheet
Slapak et al. Observations of oxygen ions in the dayside magnetosheath associated with southward IMF
CN108032140A (zh) 一种航天飞机构件生产仪器
CN207930397U (zh) 一种航天飞机构件生产仪器
Ala‐Lahti et al. Energy flux through the magnetopause during flux transfer events in hybrid‐Vlasov 2D simulations
Genestreti et al. An empirical model for the location and occurrence rate of near‐Earth magnetotail reconnection
Lundberg et al. Multi‐payload measurement of transverse velocity shears in the topside ionosphere
Yu et al. EMIC waves covering wide L shells: MMS and Van Allen Probes observations
Wang et al. The influence of IMF By on the bow shock: observation result
Liu et al. The geometry of an electron scale magnetic cavity in the plasma sheet
Wu et al. Current sheet flapping motions in the tailward flow of magnetic reconnection
Cao et al. Bidirectional electron conic observations for photoelectrons in the Martian ionosphere

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

Application publication date: 20180515

WW01 Invention patent application withdrawn after publication