CN106441392A - Satellite detector - Google Patents

Satellite detector Download PDF

Info

Publication number
CN106441392A
CN106441392A CN201610909031.8A CN201610909031A CN106441392A CN 106441392 A CN106441392 A CN 106441392A CN 201610909031 A CN201610909031 A CN 201610909031A CN 106441392 A CN106441392 A CN 106441392A
Authority
CN
China
Prior art keywords
detector
seat
circular cross
satellite
sensor
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.)
Pending
Application number
CN201610909031.8A
Other languages
Chinese (zh)
Inventor
周末
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201610909031.8A priority Critical patent/CN106441392A/en
Publication of CN106441392A publication Critical patent/CN106441392A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D11/00Component parts of measuring arrangements not specially adapted for a specific variable
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D11/00Component parts of measuring arrangements not specially adapted for a specific variable
    • G01D11/30Supports specially adapted for an instrument; Supports specially adapted for a set of instruments

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

The invention relates to a satellite detector, which comprises a spherical ultrasonic detector capsule. The right end of the spherical ultrasonic detector capsule is equipped with a circular cross section component base; the lower side of the circular cross section component base is equipped with an LED indication lamp; the upper side of the circular cross section component base is equipped with a sensor sleeve and a power line connector; the left side of the sensor sleeve is provided with a fixation side ear; the power line connector is arranged at the right end of the sensor sleeve; and the right end of the circular cross section component base is equipped with a detector base. The satellite detector is provided with the spherical ultrasonic detector capsule, the circular cross section component base, the detector base and the LED indication lamp, thereby facilitating classification installation of different types of detectors and installation of auxiliary components and realizing a light indication function; and through the arrangement of the power line connector, the LED indication lamp, the sensor sleeve and the fixation side ear, connection of a power line, installation of the LED lamp and the sensor can be realized favorably, and the function of installation and fixation of the whole device body is realized.

Description

A kind of satellite sensor
Technical field
The present invention relates to space equipment device design technical field, more particularly, to a kind of satellite sensor.
Background technology
In recent years, international space industry starts a new round and explores upsurge it is desirable to grasp " secret " and the money of space further 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 " ancestor one Step " conquers space, and none is not " without a stop ".Except obtaining important strategic interests and economic benefit, various countries are to boat The input in its field, also increasingly shows " Megrez processed " significance for national security and development.Spacecraft has many Plant sorting technique, you can be classified according to its Path Properties, scientific and technological feature, quality size, application.Spacecraft according to Application 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 divides 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 satellite sensor on existing market and contributing to classification, inhomogeneity is installed The detector of type, the device installing and realizing light referential function of accessory, satellite sensor also lack and help In connecting power line, mounted LED lamp tool and sensor and realize the device of overall the installations fixing function of device it is impossible to meet in fact The demand of border situation.
Content of the invention
The invention aims to overcoming the deficiencies in the prior art, there is provided a kind of satellite sensor.
The present invention is to be achieved through the following technical solutions:
A kind of satellite sensor, including spherical ultrasonic detector capsule, the right-hand member peace of described spherical ultrasonic detector capsule Equipped with circular cross-section element seat, the downside of described circular cross-section element seat is provided with LED light, circular cross-section element seat upper Side is provided with sensor sleeve and power cord connector, and the left side of described sensor sleeve is provided with fixation and picks up the ears, described power cord connector position In the right-hand member of sensor sleeve, the right-hand member of circular cross-section element seat is provided with detector seat, the upper end of described detector seat and detection The lower end of device seat is equipped with LED marking light.
As the preferred technical solution of the present invention, described circular cross-section element seat is arranged on the left end of detector seat, described The lower end of detector seat is provided with laser lamp cylinder, and detector seat is provided with LED display.
As the preferred technical solution of the present invention, described sensor sleeve is also located at the middle part of circular cross-section element seat.
As the preferred technical solution of the present invention, described detector seat is bolted on the right side of circular cross-section element seat End.
During onsite application, device integral installation at correct position, then device is integrally fixed by operator, you can Carry out satellite sounding operation work.
Compared with prior art, the invention has the beneficial effects as follows:The present invention be provided with spherical ultrasonic detector capsule, Circular cross-section element seat, detector seat and LED marking light contribute to classification and install different types of detector, the peace of accessory Fill and realize light referential function, pick up the ears to contribute to even by arranging power cord connector, LED light, sensor sleeve and fixation Connect power line, mounted LED lamp tool and sensor and realize the overall installation fixing function of device, and structure is simple, easy to operate, Economical and practical.
Brief description
Fig. 1 is the structural representation of the present invention.
In figure:1st, spherical ultrasonic detector capsule;2nd, circular cross-section element seat;21st, LED light;22nd, sensor sleeve; 221st, fixation is picked up the ears;23rd, power cord connector;24th, detector seat;241st, LED marking light;242nd, laser lamp cylinder;243rd, LED shows Screen.
Specific embodiment
In order that the objects, technical solutions and advantages of the present invention become more apparent, below in conjunction with drawings and Examples, right The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only in order to explain the present invention, and It is not used in the restriction present invention.
Refer to Fig. 1, Fig. 1 is the structural representation of the present invention.
A kind of described satellite sensor, including spherical ultrasonic detector capsule 1, described spherical ultrasonic detector capsule 1 Right-hand member is provided with circular cross-section element seat 2, and the downside of described circular cross-section element seat 2 is provided with LED light 21, spherical ultrasonic It is different types of that wave detector capsule 1, circular cross-section element seat 2, detector seat 24 and LED marking light 241 contribute to classification installation Detector, the installing and realize light referential function of accessory.
Described LED light 21 contributes to circular cross-section element seat 2 laser diode attachment auxiliary, circular cross-section element seat 2 upper Side is provided with sensor sleeve 22 and power cord connector 23, power cord connector 23, LED light 21, sensor sleeve 22 and affixed side Ear 221 contributes to connecting power line, mounted LED lamp tool and sensor and realizing the overall installation fixing function of device, described biography The middle parts that sensor set 22 is also located at circular cross-section element seat 2, the left side of sensor sleeve 22 is provided with fixation and picks up the ears 221.
Described power cord connector 23 is located at the right-hand member of sensor sleeve 22, and the right-hand member of circular cross-section element seat 2 is provided with detection Device seat 24, circular cross-section element seat 2 is also arranged on the left end of detector seat 24, and described detector seat 24 is bolted to be justified The right-hand member of tee section element seat 2, the lower end of the upper end of detector seat 24 and detector seat 24 is equipped with LED marking light 241, detects The lower end of device seat 24 is provided with laser lamp cylinder 242, and laser lamp cylinder 242 contributes to installing laser lamp, and detector seat 24 is provided with LED display 243.
During onsite application, device integral installation at correct position, then device is integrally fixed by operator, you can Carry out satellite sounding operation work.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention Any modification, equivalent and improvement made within god and principle etc., should be included within the scope of the present invention.

Claims (4)

1. a kind of satellite sensor it is characterised in that:Including spherical ultrasonic detector capsule (1), described spherical ultrasonic detects The right-hand member of device capsule (1) is provided with circular cross-section element seat (2), and the downside of described circular cross-section element seat (2) is provided with LED instruction Lamp (21), the upside of circular cross-section element seat (2) is provided with sensor sleeve (22) and power cord connector (23), described sensor sleeve (22) left side is provided with fixation and picks up the ears (221), and described power cord connector (23) is located at the right-hand member of sensor sleeve (22), circular cross-section The right-hand member of element seat (2) is provided with detector seat (24), the upper end of described detector seat (24) and the lower end of detector seat (24) It is equipped with LED marking light (241).
2. a kind of satellite sensor according to claim 1 it is characterised in that:Described circular cross-section element seat (2) is installed In the left end of detector seat (24), the lower end of described detector seat (24) is provided with laser lamp cylinder (242), on detector seat (24) LED display (243) is installed.
3. a kind of satellite sensor according to claim 1 it is characterised in that:Described sensor sleeve (22) is also located at circle The middle part of section members seat (2).
4. a kind of satellite sensor according to claim 1 it is characterised in that:Described detector seat (24) is by bolt even It is connected on the right-hand member of circular cross-section element seat (2).
CN201610909031.8A 2016-10-18 2016-10-18 Satellite detector Pending CN106441392A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610909031.8A CN106441392A (en) 2016-10-18 2016-10-18 Satellite detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610909031.8A CN106441392A (en) 2016-10-18 2016-10-18 Satellite detector

Publications (1)

Publication Number Publication Date
CN106441392A true CN106441392A (en) 2017-02-22

Family

ID=58175462

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610909031.8A Pending CN106441392A (en) 2016-10-18 2016-10-18 Satellite detector

Country Status (1)

Country Link
CN (1) CN106441392A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2718517Y (en) * 2004-04-29 2005-08-17 陈新 Sea level buoy detector based on satellite positioning system
CN101915924A (en) * 2010-04-14 2010-12-15 清华大学 Normal-temperature infrared inner satellite imaging detector
CN202711490U (en) * 2012-07-03 2013-01-30 厦门科拓通讯技术股份有限公司 Multi-probe integrated supersonic wave parking stall detector
CN103033834A (en) * 2012-12-17 2013-04-10 清华大学 Global position system (GPS) indoor positioning system based on visible light light-emitting diode (LED)
CN103197187A (en) * 2013-04-15 2013-07-10 北京空间飞行器总体设计部 Verifying equipment for detector power supply and distribution test system
CN203311648U (en) * 2013-07-05 2013-11-27 黄淮学院 Ultrasonic wave detector of parking space
CN203849407U (en) * 2014-04-17 2014-09-24 北京金景科技有限公司 Support device mounting each assembly of mobile laser radar equipment
CN105570640A (en) * 2015-11-18 2016-05-11 青岛理工大学琴岛学院 Detector shelf

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2718517Y (en) * 2004-04-29 2005-08-17 陈新 Sea level buoy detector based on satellite positioning system
CN101915924A (en) * 2010-04-14 2010-12-15 清华大学 Normal-temperature infrared inner satellite imaging detector
CN202711490U (en) * 2012-07-03 2013-01-30 厦门科拓通讯技术股份有限公司 Multi-probe integrated supersonic wave parking stall detector
CN103033834A (en) * 2012-12-17 2013-04-10 清华大学 Global position system (GPS) indoor positioning system based on visible light light-emitting diode (LED)
CN103197187A (en) * 2013-04-15 2013-07-10 北京空间飞行器总体设计部 Verifying equipment for detector power supply and distribution test system
CN203311648U (en) * 2013-07-05 2013-11-27 黄淮学院 Ultrasonic wave detector of parking space
CN203849407U (en) * 2014-04-17 2014-09-24 北京金景科技有限公司 Support device mounting each assembly of mobile laser radar equipment
CN105570640A (en) * 2015-11-18 2016-05-11 青岛理工大学琴岛学院 Detector shelf

Similar Documents

Publication Publication Date Title
RU2358294C2 (en) Helicopter system for electromagnetic survey
Paul et al. The Chinese–French SVOM mission for gamma-ray burst studies
Østgaard et al. Evolution of auroral asymmetries in the conjugate hemispheres during two substorms
Němec et al. Quasiperiodic emissions observed by the Cluster spacecraft and their association with ULF magnetic pulsations
Flatley Spacecube: A family of reconfigurable hybrid on-board science data processors
CN106441392A (en) Satellite detector
Akhavan‐Tafti et al. Cross‐scale quantification of storm‐time dayside magnetospheric magnetic flux content
Nakazawa et al. The hard x-ray imager (HXI) onboard ASTRO-H
Baglioni et al. The Mars exploration plans of ESA
Pareschi et al. The mini-array of ASTRI SST-2M telescopes, precursors for the Cherenkov Telescope Array
Gershman et al. Ion‐scale structure in Mercury's magnetopause reconnection diffusion region
Kauristie et al. Study on the ionospheric signatures of the plasma sheet bubbles
Ubertini et al. The INTErnational Gamma Ray Astrophysics Laboratory: INTEGRAL Highlights
Owen et al. High-cadence measurements of electron pitch-angle distributions from Solar Orbiter SWA-EAS burst mode operations
Sol et al. Observing the sky at extremely high energies with the Cherenkov Telescope Array: Status of the GCT project
CN107877199A (en) A kind of space shuttle undercarriage processes clamper
CN106312628A (en) Aero-engine machining instrument
CN108001710A (en) A kind of grapefruit satellite transmitter
CN205030047U (en) A shield cover for on multiaxis aircraft
den Herder et al. The search for decaying Dark Matter
CN107983843A (en) A kind of aerospace parts processing apparatus
Braden et al. Human exploration of the Gruithuisen Domes
CN108032140A (en) A kind of space shuttle component produces instruments
Jørgensen et al. The interplanetary dust population as measured by the MAG investigation on the Juno mission.
CN107879014A (en) A kind of space flight equipment processes conveyer

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20170222