CN202171471U - Device for inspecting superfluous objects in spacecraft cabin body - Google Patents

Device for inspecting superfluous objects in spacecraft cabin body Download PDF

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Publication number
CN202171471U
CN202171471U CN2011203120933U CN201120312093U CN202171471U CN 202171471 U CN202171471 U CN 202171471U CN 2011203120933 U CN2011203120933 U CN 2011203120933U CN 201120312093 U CN201120312093 U CN 201120312093U CN 202171471 U CN202171471 U CN 202171471U
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CN
China
Prior art keywords
spacecraft cabin
rotating shaft
rotating disk
spacecraft
wheel
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Withdrawn - After Issue
Application number
CN2011203120933U
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Chinese (zh)
Inventor
程国栋
樊章芸
吴红英
杨秀富
田华
陈畅
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.)
Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Original Assignee
Guizhou Aerospace Fenghua Precision Equipment 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 Guizhou Aerospace Fenghua Precision Equipment Co Ltd filed Critical Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Priority to CN2011203120933U priority Critical patent/CN202171471U/en
Application granted granted Critical
Publication of CN202171471U publication Critical patent/CN202171471U/en
Anticipated expiration legal-status Critical
Withdrawn - After Issue legal-status Critical Current

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Abstract

The utility model discloses a device for inspecting superfluous objects in a spacecraft cabin body. The device comprises a frame (1), wherein the frame (1) is provided with a rotating shaft (2), a front end of the rotating shaft (2) is provided with a connecting rotating disk (3) used for connecting the spacecraft cabin body (5), a tail end of the rotating shaft (2) is provided with a crank handle (4), and an end face of the connecting rotating disk (3) is provided with at least one viewing port (3.4). The device of the utility model has the advantages of high inspection efficiency, good reliability, low inspection cost, simple structure, easy manufacture, convenient use, etc.

Description

The testing fixture of fifth wheel in a kind of spacecraft cabin
Technical field
the utility model relates to the testing fixture of fifth wheel in a kind of spacecraft cabin, belongs to spacecraft cabin detection technique field.
Background technology
are present, when relating to the spacecraft general assembly, the inspection method of fifth wheel in the spacecraft cabin mainly contained observation and internal imaging method.Wherein observation is more direct, but inspection is very coarse, and the place that can't see naked eyes in the spacecraft cabin is easy to omission, thereby causes quality accident.And the internal imaging method; It mainly is that high-end imaging technique of application and device are shot with video-corder, scanned fifth wheel in the spacecraft cabin, observes and analyzes through external connection display equipment, adopts this method that fifth wheel is checked; Though effect is better; But it is high but to exist the inspection cost, and the complex structure that checks the equipment is unfavorable for improving shortcomings such as spacecraft general assembly production efficiency.Therefore the test mode of fifth wheel still is not ideal enough in the existing spacecraft cabin.
Summary of the invention
The purpose of the utility model is: the testing fixture of fifth wheel in a kind of detection efficiency height, good reliability and the detection cost spacecraft cabin low, easy to use is provided, to overcome the deficiency of prior art.
the utility model is achieved in that the testing fixture of the interior fifth wheel of a kind of spacecraft cabin of the utility model is: this device comprises frame; On frame, be provided with the rotating shaft that to rotate; Front end in rotating shaft is equipped with the connection rotating disk that is used to connect spacecraft cabin; Tail end in rotating shaft is provided with crank handle, on the end face that connects rotating disk, is provided with at least one observation panel.
are fixed with on above-mentioned connection rotating disk and are used for the axle sleeve of sleeve in rotating shaft; And be connected with floor between the rotating disk with being connected at axle sleeve; Connecting rotating disk is installed in the rotating shaft through axle sleeve; On the connection rotating disk, be provided with the bolt hole that is used for connecting spacecraft cabin, on the end face that connects rotating disk, be provided with at least one observation panel through bolt.
are owing to adopted technique scheme; The utility model is installed in one with spacecraft cabin and can drives on the device that this spacecraft cabin rotates; Making this device drive spacecraft cabin then rotates; Through rotating the fifth wheel in the spacecraft cabin is moved; Can make things convenient for so exactly through the observation panel on the device and observe the motion of fifth wheel in the spacecraft cabin or the situation of being scattered, and can clearly listen in the spacecraft cabin of rotation whether send the sound, thus convenient, judge effectively or check out whether fifth wheel is arranged in the spacecraft module body.When the device through the utility model rotates spacecraft cabin; If in case hear the sound; Just explanation has fifth wheel to exist in spacecraft cabin; And can examine the position of being scattered of fifth wheel through observation panel, can stop rotation immediately like this, and fifth wheel taken out through observation panel to spacecraft cabin; So circulation can make things convenient for, efficiently, reliably the fifth wheel complete inspection in the spacecraft cabin is come out.So, the utility model compared with prior art, the utility model not only has detection efficiency height, good reliability, advantage that the detection cost is low, but also have simple in structure, make advantages such as easy, easy to use.
Description of drawings
Fig. 1 is the structural representation of the utility model;
Fig. 2 is that the connection rotating disk of the utility model is installed in the structural representation in the rotating shaft;
Fig. 3 is the left TV structure synoptic diagram of Fig. 2.
Being labeled as in accompanying drawing: the 1-frame, the 2-rotating shaft, 3-connects rotating disk, 3.1-axle sleeve, 3.2-floor, 3.3-bolt hole, 3.4-observation panel, 4-crank handle, 5-spacecraft cabin.
Embodiment
Below , the utility model is further described in conjunction with accompanying drawing and embodiment.
The embodiment of the utility model: the utility model be used for the method that fifth wheel in the spacecraft cabin is checked be; Promptly earlier spacecraft cabin being installed in one can drive on the device that this spacecraft cabin rotates; And setting can be observed the observation panel in the spacecraft cabin on this device; Making this device drive spacecraft cabin then rotates; Through rotating the fifth wheel in the spacecraft cabin is moved; Like this can be when rotating observe the motion or the situation of being scattered of fifth wheel in the spacecraft cabin, and listen in the spacecraft cabin of rotation whether send the sound, thereby judge or check out whether fifth wheel is arranged in the spacecraft module body through the observation panel on the device.
The testing fixture that are used for fifth wheel in a kind of spacecraft cabin of the utility model of said method is: the structure of this device is shown in Fig. 1~3; Comprise frame 1; Frame 1 can adopt steel to be welded; During making, a horizontally disposed rotating shaft 2 is installed on frame 1, a connection rotating disk 3 that is used to connect spacecraft cabin 5 is installed at the front end of rotating shaft 2; Tail end in rotating shaft 2 is installed a crank handle 4, and on the end face that connects rotating disk 3, produces 2~4 observation panels 3.4; The structure of this device is stable more and reliable in order to work; Connect on the rotating disk 3 fixing one can the axle sleeve 3.1 of sleeve in rotating shaft 2; And axle sleeve 3.1 be connected between the rotating disk 3 by 4 floors 3.2 of welding that distribute symmetrically; To connect rotating disk 3 and be installed in the rotating shaft 2, and rotating shaft 2 can be driven connect rotating disk 3 and rotate together through axle sleeve 3.1; For connection spacecraft cabin 5 convenience, produce 4~8 bolts hole 3.3 that can connect spacecraft cabin 5 on the rotating disk 3 connecting through bolt.

Claims (2)

1. the testing fixture of fifth wheel in the spacecraft cabin; Comprise frame (1); It is characterized in that: on frame (1), be provided with rotating shaft (2); Front end in rotating shaft (2) is equipped with the connection rotating disk (3) that is used to connect spacecraft cabin (5), is provided with crank handle (4) at the tail end of rotating shaft (2), on the end face that connects rotating disk (3), is provided with at least one observation panel (3.4).
2. the testing fixture of fifth wheel in the spacecraft cabin according to claim 1; It is characterized in that: be used for the axle sleeve (3.1) of sleeve in rotating shaft (2) connecting to be fixed with on the rotating disk (3); And be connected with floor (3.2) between the rotating disk (3) with being connected at axle sleeve (3.1); Connect rotating disk (3) and be installed in the rotating shaft (2), on connection rotating disk (3), be provided with the bolt hole (3.3) that is used for connecting spacecraft cabin (5) through bolt through axle sleeve (3.1).
CN2011203120933U 2011-08-24 2011-08-24 Device for inspecting superfluous objects in spacecraft cabin body Withdrawn - After Issue CN202171471U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011203120933U CN202171471U (en) 2011-08-24 2011-08-24 Device for inspecting superfluous objects in spacecraft cabin body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011203120933U CN202171471U (en) 2011-08-24 2011-08-24 Device for inspecting superfluous objects in spacecraft cabin body

Publications (1)

Publication Number Publication Date
CN202171471U true CN202171471U (en) 2012-03-21

Family

ID=45829666

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011203120933U Withdrawn - After Issue CN202171471U (en) 2011-08-24 2011-08-24 Device for inspecting superfluous objects in spacecraft cabin body

Country Status (1)

Country Link
CN (1) CN202171471U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102955178A (en) * 2011-08-24 2013-03-06 贵州航天风华精密设备有限公司 Method and device for checking remnant in spacecraft cabin
CN103472196A (en) * 2013-10-08 2013-12-25 上海航天测控通信研究所 Redundancy detecting device
CN108910075A (en) * 2018-07-06 2018-11-30 江西洪都航空工业集团有限责任公司 A kind of universal fifth wheel removing equipment
CN111025419A (en) * 2019-11-22 2020-04-17 中国电子产品可靠性与环境试验研究所((工业和信息化部电子第五研究所)(中国赛宝实验室)) Cavity device detection equipment and system
CN114106712A (en) * 2021-12-06 2022-03-01 扬州海科电子科技有限公司 Cavity filter conductive adhesive bonding process

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102955178A (en) * 2011-08-24 2013-03-06 贵州航天风华精密设备有限公司 Method and device for checking remnant in spacecraft cabin
CN102955178B (en) * 2011-08-24 2016-04-13 贵州航天风华精密设备有限公司 The testing fixture of fifth wheel in a kind of spacecraft cabin
CN103472196A (en) * 2013-10-08 2013-12-25 上海航天测控通信研究所 Redundancy detecting device
CN103472196B (en) * 2013-10-08 2015-07-08 上海航天测控通信研究所 Redundancy detecting device
CN108910075A (en) * 2018-07-06 2018-11-30 江西洪都航空工业集团有限责任公司 A kind of universal fifth wheel removing equipment
CN111025419A (en) * 2019-11-22 2020-04-17 中国电子产品可靠性与环境试验研究所((工业和信息化部电子第五研究所)(中国赛宝实验室)) Cavity device detection equipment and system
CN111025419B (en) * 2019-11-22 2022-02-11 中国电子产品可靠性与环境试验研究所((工业和信息化部电子第五研究所)(中国赛宝实验室)) Cavity device detection equipment and system
CN114106712A (en) * 2021-12-06 2022-03-01 扬州海科电子科技有限公司 Cavity filter conductive adhesive bonding process
CN114106712B (en) * 2021-12-06 2023-10-13 扬州海科电子科技有限公司 Cavity filter conductive adhesive bonding process

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20120321

Effective date of abandoning: 20160413

C25 Abandonment of patent right or utility model to avoid double patenting