CN107957595A - High-altitude air blast remote probe instrument - Google Patents
High-altitude air blast remote probe instrument Download PDFInfo
- Publication number
- CN107957595A CN107957595A CN201711272658.8A CN201711272658A CN107957595A CN 107957595 A CN107957595 A CN 107957595A CN 201711272658 A CN201711272658 A CN 201711272658A CN 107957595 A CN107957595 A CN 107957595A
- Authority
- CN
- China
- Prior art keywords
- electromagnetic wave
- ultrasonic electromagnetic
- ultrasonic
- air blast
- display screen
- 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.)
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V3/00—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
- G01V3/15—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat
- G01V3/16—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat specially adapted for use from aircraft
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V3/00—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
- G01V3/15—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat
- G01V3/17—Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat operating with electromagnetic waves
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- Life Sciences & Earth Sciences (AREA)
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Environmental & Geological Engineering (AREA)
- Geology (AREA)
- Remote Sensing (AREA)
- General Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- Geophysics (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
The present invention relates to a kind of equipment for being practically applicable to aircraft smooth flight, and in particular to a kind of high-altitude air blast remote probe instrument.The high-altitude air blast remote probe instrument is by ultrasonic electromagnetic wave transceiver, computing controller and display screen etc. form, the effect of ultrasonic electromagnetic wave is the air blast detected beyond 100 kilometers from aircraft on course line, ultrasonic electromagnetic wave transceiver connects computing controller, computing controller connects display screen, ultrasonic electromagnetic wave transceiver launches ultrasonic electromagnetic wave and receives the ultrasonic electromagnetic wave for running into air blast return, the ultrasonic electromagnetic wave that return receives is passed to computing controller by ultrasonic electromagnetic wave transceiver, display is reported out coming on a display screen after computing controller processing, for pilot with reference to whether change of flight course line, ultrasonic electromagnetic wave transceiver is installed on plane nose, display screen is installed on airplane operation console.
Description
Technical field
The present invention relates to a kind of equipment for being practically applicable to aircraft smooth flight, and in particular to a kind of high-altitude air blast remote probe
Instrument.
Background technology
Mood was nervous immediately when the people that carriage crosses aircraft run into lame top and vibration, and cabin has broadcast " aircraft immediately
Run into air blast ... ".The air blast that aircraft is awing run into fact can forecast and get around flight and take precautions against.
The content of the invention
In order to aircraft flight steadily without run lame and vibration the problems such as, the present invention provides a kind of high-altitude air blast remote probe
Instrument, the high-altitude air blast remote probe instrument are made of ultrasonic electromagnetic wave transceiver, computing controller and display screen etc., are surpassed
Acoustic-electric magnetic wave meets with high-altitude air blast causes ultrasonic electromagnetic wave to change, and the effect of ultrasonic electromagnetic wave is detected from aircraft
Air blast beyond 100 kilometers on course line, ultrasonic electromagnetic wave transceiver connection computing controller, computing controller connection are aobvious
Display screen, ultrasonic electromagnetic wave transceiver transmitting ultrasonic electromagnetic wave simultaneously receive the ultrasonic electromagnetic wave for running into air blast return, ultrasound
The ultrasonic electromagnetic wave that return receives is passed to computing controller by electromagnetic radiation receiver, aobvious after computing controller processing
Show screen display be reported out come, for pilot with reference to whether change of flight course line, ultrasonic electromagnetic wave transceiver be installed on fly
On machine head, display screen is installed on airplane operation console, as shown in the figure.The invention has the advantages that aircraft flight is steady
Without running, lame and vibration, effect simple in structure are good.
Brief description of the drawings
Fig. 1 is the structure diagram of high-altitude air blast remote probe instrument：Wherein 1 is ultrasonic electromagnetic wave transceiver, and 2 are
Computing controller, 3 be display screen.
Embodiment
In Fig. 1, high-altitude air blast remote probe instrument is by ultrasonic electromagnetic wave transceiver（1）, computing controller（2）And
Display screen（3）Formed Deng device, ultrasonic electromagnetic wave meets with high-altitude air blast causes ultrasonic electromagnetic wave to change, ultrasonic electromagnetism
The effect of ripple is to detect 100 kilometers from the aircraft air blasts on course line in addition, ultrasonic electromagnetic wave transceiver（1）Connection calculates
Controller（2）, computing controller（2）Connect display screen（3）, ultrasonic electromagnetic wave transceiver（1）Launch ultrasonic electromagnetic wave simultaneously
Receive the ultrasonic electromagnetic wave for running into air blast return, ultrasonic electromagnetic wave transceiver（1）The ultrasonic electromagnetism received will be returned to
Ripple passes to computing controller（2）, computing controller（2）In display screen after processing（3）Upper display is reported out coming, and joins for pilot
Examine whether change of flight course line, ultrasonic electromagnetic wave transceiver（1）On plane nose, display screen（3）Installed in winged
Machine operating console.
Claims (1)
- A kind of 1. high-altitude air blast remote probe instrument, it is characterised in that：It is by ultrasonic electromagnetic wave transceiver（1）, calculate control Device processed（2）And display screen（3）Device forms, and ultrasonic electromagnetic wave meets with high-altitude air blast causes ultrasonic electromagnetic wave to change, The effect of ultrasonic electromagnetic wave is to detect 100 kilometers from the aircraft air blasts on course line in addition, ultrasonic electromagnetic wave transceiver（1） Connect computing controller（2）, computing controller（2）Connect display screen（3）, ultrasonic electromagnetic wave transceiver（1）Transmitting ultrasound Electromagnetic wave simultaneously receives the ultrasonic electromagnetic wave for running into air blast return, ultrasonic electromagnetic wave transceiver（1）It will return what is received Ultrasonic electromagnetic wave passes to computing controller（2）, computing controller（2）In display screen after processing（3）Upper display is reported out coming, and supplies Pilot with reference to whether change of flight course line, ultrasonic electromagnetic wave transceiver（1）On plane nose, display screen（3） Installed in airplane operation console.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711272658.8A CN107957595A (en) | 2017-12-06 | 2017-12-06 | High-altitude air blast remote probe instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711272658.8A CN107957595A (en) | 2017-12-06 | 2017-12-06 | High-altitude air blast remote probe instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107957595A true CN107957595A (en) | 2018-04-24 |
Family
ID=61957507
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711272658.8A Withdrawn CN107957595A (en) | 2017-12-06 | 2017-12-06 | High-altitude air blast remote probe instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107957595A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6034760A (en) * | 1997-10-21 | 2000-03-07 | Flight Safety Technologies, Inc. | Method of detecting weather conditions in the atmosphere |
| CN1957267A (en) * | 2004-05-25 | 2007-05-02 | 法国空中客车公司 | System for pretesting raising turbulence of an aircraft |
| CN101268384A (en) * | 2005-07-21 | 2008-09-17 | 空中客车德国有限公司 | Method and lidar system for measuring air turbulences on board aircraft and for airports and wind farms |
| US20090267826A1 (en) * | 2004-12-03 | 2009-10-29 | The Boeing Company | System for measuring turbulence remotely |
| CN102129795A (en) * | 2011-02-18 | 2011-07-20 | 北京航空航天大学 | Airborne weather radar teaching simulation system |
| CN106887055A (en) * | 2017-01-23 | 2017-06-23 | 广州博进信息技术有限公司 | Flight is jolted method for early warning and its system |
-
2017
- 2017-12-06 CN CN201711272658.8A patent/CN107957595A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6034760A (en) * | 1997-10-21 | 2000-03-07 | Flight Safety Technologies, Inc. | Method of detecting weather conditions in the atmosphere |
| CN1957267A (en) * | 2004-05-25 | 2007-05-02 | 法国空中客车公司 | System for pretesting raising turbulence of an aircraft |
| US20090267826A1 (en) * | 2004-12-03 | 2009-10-29 | The Boeing Company | System for measuring turbulence remotely |
| CN101268384A (en) * | 2005-07-21 | 2008-09-17 | 空中客车德国有限公司 | Method and lidar system for measuring air turbulences on board aircraft and for airports and wind farms |
| CN102129795A (en) * | 2011-02-18 | 2011-07-20 | 北京航空航天大学 | Airborne weather radar teaching simulation system |
| CN106887055A (en) * | 2017-01-23 | 2017-06-23 | 广州博进信息技术有限公司 | Flight is jolted method for early warning and its system |
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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: 20180424 |