CN107238366A - Weather vane type angle of attack airspeed sensor protection device - Google Patents
Weather vane type angle of attack airspeed sensor protection device Download PDFInfo
- Publication number
- CN107238366A CN107238366A CN201710382646.4A CN201710382646A CN107238366A CN 107238366 A CN107238366 A CN 107238366A CN 201710382646 A CN201710382646 A CN 201710382646A CN 107238366 A CN107238366 A CN 107238366A
- Authority
- CN
- China
- Prior art keywords
- block
- protection
- protection block
- attack
- angle
- 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.)
- Granted
Links
- 230000004224 protection Effects 0.000 title claims abstract description 191
- 230000032258 transport Effects 0.000 abstract description 7
- 230000004048 modification Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000007306 turnover Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C1/00—Measuring angles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING 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
- G01D11/00—Component parts of measuring arrangements not specially adapted for a specific variable
- G01D11/24—Housings ; Casings for instruments
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Testing Or Calibration Of Command Recording Devices (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The present invention discloses a kind of weather vane type angle of attack airspeed sensor protection device, it is desirable to provide a kind of convenient mounting and clamping, transports reliable protection device, the technical scheme is that：The side openend of the first half arc connectors is fixedly connected with the first guard member and its first flipping block; opposite side openend is fixedly connected with the second protection block, and the first protection block and the second protection block are connected with the first half arc connector with the two ends of axis parallel respectively；The second half arc connector side openends are fixedly connected with the second guard member and its second flipping block；3rd protection block and the second protection block are located at the opposite sides of the right angle of attack or right yaw angle respectively; 3rd protection block and the second protection block interfix; now rotate second flipping block; so that second flipping block fits with the described 3rd protection block; the opposite side located at the right angle of attack or right yaw angle is kept off together with the described second protection block, and second flipping block is fixed on the 3rd protection block.
Description
Technical field
The present invention relates to flight equipment technical field, more particularly to a kind of protection device of pitot weathercock.
Background technology
Pitot weathercock installed in aircraft tip center is divided to single weathercock and double two kinds of weathercocks, and single weather vane type angle of attack is passed
Loaded on aircraft side more than sensor, and double weather vane type sensors are often combined with pitot, are installed on strut before the handpiece,
The latter is the combination sensor of the angle of attack and yaw angle.Generally, weathercock is made up of a pair of angles of attack and a pair of yaw angle two parts, the angle of attack
It is distributed in yaw angle in 90 degree in air speed tube axis line.Survey aircraft air speed and the instrument referred to as air speed for exporting corresponding electric signal
Sensor or pitot.Pitot also turns into Pitot tube or stagnation pressure tube, is very important parameter measuring instrumentss on aircraft.In order to
Prevent pitot weathercock to be damaged, during transport or after installation, before not taking off, be required for entering the pitot weathercock
Row protection.Pitot typically uses electro-thermal anti-ice, due to can not for a long time be heated to pitot at ground, adds in pitot
Circuit temperature sets Power control component to gradually rise electric current, the mounting temperature sensor generally in pitot.To be overheated
Protection, it is to avoid burn out, heats in circuit in pitot and sets overtemperature relay to carry out overtemperature protection.In the prior art in order in fortune
During defeated, or before installation is not taken off, circle is all located at using the cylindrical sleeve angle of attack and yaw angle on pitot weathercock
In cylinder, to reach the purpose of protection pitot weathercock, but in use, the cylindrical sleeve protected mode is not easy to air speed manage-style
Target clamping and transport.
The content of the invention
The purpose of the present invention is the presence of the weak point for being not easy to clamping and transport pitot weathercock for prior art, is carried
For a kind of convenient mounting and clamping, reliable weather vane type angle of attack airspeed sensor protection device is transported.
The technical solution adopted for the present invention to solve the technical problems is that a kind of weather vane type angle of attack airspeed sensor protection is filled
Put, including：It is distributed in a pair of weathercock guard members in the pitot pipe shaft both sides angle of attack or yaw angle and wraps up the pitot pipe
The cylindrical sleeve of body, it is characterised in that：Described cylindrical sleeve is made up of half arc connector of two pieces of mutual pairings, wherein, first
The side openend of half arc connector 113 is fixedly connected with the first guard member 11 and its by the first protection active link of block 111
First flipping block 21, opposite side openend is fixedly connected with the second protection block 112, the second guard member 12 and first guard member 11
The heart piles setting, the first half arc connectors 113 and the second half arc connectors（122）Bag is located at the pitot（230）On,
First protection block（111）It is located at the opposite sides of the left angle of attack or left yaw angle respectively with the 4th protection block 124, and by institute
State the first protection block（111）Interfixed with the described 4th protection block 124；；The second half side openends of arc connector 122 are consolidated
The second guard member 12 and its second flipping block 22 by the 3rd protection active link of block 123 are associated with, accordingly, the described 3rd protects
Protecting block 123 is longer than the described second protection block 112；3rd protection block 123 and second protection block 112 respectively be located at the right angle of attack or
The opposite sides of right yaw angle, and the described 3rd protection block 123 and the second protection block 112 are interfixed, now turn
Move second flipping block 22 so that second flipping block 22 fits with the described 3rd protection block 123, is protected with described second
Protecting block 112 keeps off the opposite side located at the right angle of attack or right yaw angle together, and second flipping block 22 is fixed on described
On 3rd protection block 123.
The present invention has the advantages that compared to prior art.
The first half arc connectors and the second half arc connectors 122 are wrapped on pitot by convenient mounting and clamping, the present invention,
First protection block and the 4th protection block 124 are located to the opposite sides of the left angle of attack or left yaw angle respectively, and will be described
First protection block and the 4th protection block 124 interfix, and are fitted by the first flipping block 21 with the first protection block, clamping
It is convenient.
Transport is reliable, and the present invention keeps off the opposite side located at the left angle of attack or left yaw angle using the 4th protection block 124 together, and
The 3rd protection protection of block 123 and second block is located to the opposite sides of the right angle of attack or right yaw angle respectively, and will be described
3rd protection block 123 and the second protection block are interfixed, and the second flipping block 22 is kept off located at described together with the second protection block
The opposite side of the right angle of attack or right yaw angle, and second flipping block 22 is fixed on the 3rd protection block 123 so that institute
The shape and the profile of weathercock component for stating protection device match, and are readily transported and clamping, solve cylindrical sleeve in the prior art
If protected mode be not easy to the transport of pitot weathercock and the technical problem of clamping.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, embodiment will be described below
In required for the accompanying drawing that uses be briefly described, it should be apparent that, drawings in the following description are only some of the present invention
Embodiment.
Fig. 1 is the stereogram of weather vane type angle of attack airspeed sensor protection device of the present invention.
Fig. 2 is Fig. 1 exploded view.
Fig. 3 is the structural representation of pitot weathercock.
Fig. 4 is the use state of Fig. 1 weather vane type angle of attack airspeed sensor protection devices with reference to figure.
In figure：11 first guard members, 12 second guard members, 21 first flipping blocks, 22 second flipping blocks, 111 first protections
Block, 112 second protection blocks, 113 the first half arc connectors, 122 the second half arc connectors, 123 the 3rd protection blocks, 124 the
Four protection blocks, 200 pitot weathercocks, 210 a pair of angles of attack, 220 a pair of yaw angles, 230 pitots.
Embodiment
Refering to Fig. 1, Fig. 2, in embodiment described below, a kind of weather vane type angle of attack airspeed sensor protection device, bag
Include：It is distributed in a pair of weathercock guard members in the pitot pipe shaft both sides angle of attack or yaw angle and wraps up the circle of the pitot pipe shaft
Jacket casing, the pitot weathercock 200 includes an offside of pitot 230, a pair of angles of attack 210 positioned at pipe shaft both sides and its rear
Sliding angle 220, and angle between a pair of angles of attack 210 and a pair of yaw angles 220 is 90 degree.The angle of attack 210 and yaw angle 220
A pair of weathercocks are individually fixed on two sections of the pitot 230.Described cylindrical sleeve is connected by half arc of two pieces of mutual pairings
Fitting is constituted, wherein, the side openend of the first half arc connectors 113 is fixedly connected with the first guard member 11 and its protected by first
First flipping block 21 of the active link of protecting block 111, opposite side openend is fixedly connected with the second protection block 112, the first protection block
111 and second protection block 112 be connected respectively with the first half arc connector 113 with the two ends of axis parallel, and the
The length of one protection block 111 is more than the length of the described second protection block 112；The second half side openends of arc connector 122 are consolidated
The second guard member 12 and its second flipping block 22 by the 3rd protection active link of block 123 are associated with, accordingly, the described 3rd protects
Protecting block 123 is longer than the described second protection block 112；3rd protection block 123 and second protection block 112 respectively be located at the right angle of attack or
The opposite sides of right yaw angle, and the described 3rd protection block 123 and the second protection block 112 are interfixed, now turn
Move second flipping block 22 so that second flipping block 22 fits with the described 3rd protection block 123, is protected with described second
Protecting block 112 keeps off the opposite side located at the right angle of attack or right yaw angle together, and second flipping block 22 is fixed on described
On 3rd protection block 123.
First guard member 11 includes the first protection block 111, second protection block and the first half arc connectors, and the first protection
The protection of block 111 and second block 12 is connected with the first half arc connector with the two ends of axis parallel respectively.
Second guard member 12 includes the 3rd protection block the 123, the 4th protection block 124 and the second half arc connectors 122, and the
Three protection blocks 123 and the 4th protection block 124 respectively with the second half arc connector 122 with axis parallel two
End connection, the 3rd protection protection of block 123 and second block is located at the opposite sides of the right angle of attack or right yaw angle respectively, and mutually
Fixed second flipping block 22 is turned in the same side of the described second protection block, and is fixed on the 3rd protection block 123
On.
First flipping block 21 is rotated with one end away from the first half arc connector on the described first protection block 111 to be connected
Connect；
One end away from the second half arc connector 122, which is rotated, on second flipping block 22, with the described 3rd protection block 123 connects
Connect；
Preferably, first flipping block 21 mutually splices with the described 4th protection block 124, and the second flipping block 22 is protected with described second
Protecting block 112 is mutually spliced.
Preferably, the 3rd protection block 123 and the 4th protection block 124 is tabular, and the second half arc connectors 122 are half
Arcuation.
Preferably, the shape and structure of second guard member 12 and the shape and structure of the first guard member 11 are identical, and
And be centrosymmetric setting with first guard member.
The first half arc connectors and the second half arc connector 122 are wrapped on the pitot, the first protection
The protection of block 111 and the 4th block 124 is located at the opposite sides of the left angle of attack or left yaw angle and interfixed respectively, and first protects
The protection of protecting block 111 and the 4th block 124 is located at the opposite sides of the left angle of attack or left yaw angle respectively, and described first is protected
Protecting block 111 and the 4th protection block 124 interfix.
First flipping block 21 turns to the same side of the 4th protection block 124, and is fixed on the first protection block 111
On, and the first flipping block 21 protects block 111 to fit with described first, and institute is located to be kept off together with the described 4th protection block 124
State the opposite side of the left angle of attack or left yaw angle.The 3rd protection protection block of block 123 and second is located at the right angle of attack or right side respectively
The opposite sides at sliding angle, and the described 3rd protection block 123 and the second protection block are interfixed.Second flipping block 22 with
The second protection block keeps off the opposite side located at the right angle of attack or right yaw angle together, and second flipping block 22 is fixed
In the described 3rd protection block 123 on so that the shape of the protection device and the profile of weathercock component match, be readily transported with
Clamping, to solve the protected mode that cylinder is arranged in the prior art, is not easy to the transport of the pitot weathercock and the skill of clamping
Art problem.
First guard member 11 includes the first protection block 111 and second protection block 112 and the first half arc connectors 113, and
The first protection protection block 112 of block 111 and second is tabular, and the first half arc connectors 113 are semiarc shape.The first protection block
111 and second protection block 112 be connected respectively with the first half arc connector 113 with the two ends of axis parallel, it is described
The length of first protection block 111 is more than the length of the described second protection block 112.
Second guard member 12 includes the 3rd protection block 123 and the 4th protection block 124 and the second half arc connectors 122, its
In, the 3rd protection protection of block 123 and the 4th block 124 respectively with the second half arc connector 122 with axis parallel
Two ends are connected, and the length of the 3rd protection block 123 is more than the described 4th length for protecting block 124；3rd protection block 123 and the 4th
Protection block 124 is tabular, and the second half arc connectors 122 are semiarc shape.
Away from the first half arc connector on first protection block 111 of the first flipping block 21 and the first guard member 11
113 one end rotates connection, and can be turned to the position fitted with the described first protection block 111.
Away from the second half arc connector on 3rd protection block 123 of the second flipping block 22 and the second guard member 12
122 one end rotates connection, and can be turned to the position fitted with the described second protection block 111.
In use, the second guard member 12 shown in Fig. 3 and the center of the first guard member 11 pile setting, the first half arcs
Connector 113 and the second half arc connectors 122 bag are on the pitot 230, the first protection protection block of block 111 and the 4th
124 are located at the opposite sides of the left angle of attack or left yaw angle respectively, and the described first protection block 111 and the described 4th are protected
Protecting block 124 interfixes.Because the described first protection block 111 is longer than the described 4th protection block 124, the first flipping block is now rotated
21 fit with the first protection block 111, with together with the 4th protection block 124 gear located at the another of the left angle of attack or left yaw angle
Side, and the first flipping block 21 is fixed on the first protection block 111, accordingly, the 3rd protection protection block of block 123 and second
112 are located at the opposite sides of the right angle of attack or right yaw angle respectively, and the described 3rd protection block 123 and described second are protected
Protecting block 112 interfixes.Because the described 3rd protection block 123 is longer than the described second protection block 112, now rotates described second and turn over
Switch block 22 so that second flipping block 22 fits with the described 3rd protection block 123, to protect block 112 1 with described second
Gear is played located at the right angle of attack or the opposite side of right yaw angle, and second flipping block 22 is fixed on the 3rd protection block
On 123.
Refering to Fig. 4, pitot 230 is wrapped in by the first half arc connectors 113 and the second half arc connectors 122
On, the first protection protection of block 111 and the 4th block 124 is located at the opposite sides of the left angle of attack or left yaw angle respectively, and will
The first protection block 111 and the 4th protection block 124 interfix, the first flipping block 21 and the described first protection block 111
Fit, to keep off the opposite side located at the left angle of attack or left yaw angle, the 3rd protection block together with the described 4th protection block 124
123 and second protect block 112 to be located at the opposite sides of the right angle of attack or right yaw angle respectively, and protect block by the described 3rd
123 and described second protect block 112 to interfix.
Although above-mentioned have been described for the preferred embodiments of the present invention, those skilled in the art once know substantially
Creative concept, then can make other change and modification to these embodiments.So, appended claims are intended to be construed to bag
Include preferred embodiment and fall into having altered and changing for the scope of the invention.Obviously, those skilled in the art can be to this
Invention carries out various changes and modification without departing from the spirit and scope of the present invention.So, if the present invention these modification and
Modification belongs within the scope of the claims in the present invention and its equivalent technologies, then the present invention is also intended to comprising these changes and modification
Inside.
Claims (10)
1. a kind of weather vane type angle of attack airspeed sensor protection device, including：It is distributed in the pitot pipe shaft both sides angle of attack or sideslip
A pair of weathercock guard members at angle and the cylindrical sleeve for wrapping up the pitot pipe shaft, it is characterised in that：Described cylindrical sleeve is by two pieces
The half arc connector composition of mutual pairing, wherein, the first half arc connectors（113）Side openend be fixedly connected with the first guarantor
Guard（11）And its pass through the first protection block（111）First flipping block of active link（21）, opposite side openend is fixedly connected with
Two protection blocks（112）, the second guard member（12）With first guard member（11）Center piles setting, the first half arc connectors
（113）With the second half arc connectors（122）Bag is located at the pitot（230）On, the first protection block（111）With the 4th protection
Block（124）It is located at the opposite sides of the left angle of attack or left yaw angle respectively, and block is protected by described first（111）With it is described
4th protection block（124）Interfix；The second half arc connectors（122）Side openend is fixedly connected with the second guard member（12）And
It passes through the 3rd protection block（123）Second flipping block of active link（22）, accordingly, the 3rd protection block（123）Compare institute
State the second protection block（112）It is long；3rd protection block（123）With the second protection block（112）It is located at the right angle of attack or right side respectively
The opposite sides at sliding angle, and protect block by the described 3rd（123）With the described second protection block（112）Interfix, now turn
Move second flipping block（22）So that second flipping block（22）With the described 3rd protection block（123）Fit, it is and described
Second protection block（112）Together gear located at the right angle of attack or right yaw angle opposite side, and by second flipping block（22）
It is fixed on the 3rd protection block（123）On.
2. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：The pitot weathercock
（200）Including pitot（230）, a pair of angles of attack positioned at pipe shaft both sides（210）And its a pair of yaw angles at rear（220）, and
A pair of angles of attack（210）With a pair of yaw angles（220）Between angle be 90 degree.
3. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：Second guard member（12）
Shape and structure and the first guard member（11）Shape it is identical with structure, and with first guard member（11）In center pair
Claim to set.
4. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：First guard member（11）
Including the first protection block（111）, the second protection block and the first half arc connectors, and the first protection block（111）With the second protection
Block（12）It is connected respectively with the first half arc connector with the two ends of axis parallel.
5. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：Second guard member（12）
Including the 3rd protection block（123）With the 4th protection block（124）With the second half arc connectors（122）, wherein, the 3rd protection block
（123）With the 4th protection block（124）Respectively with the second half arc connector（122）The two ends of upper and axis parallel connect
Connect, and the 3rd protection block（123）Length be more than the described 4th protection block（124）Length；3rd protection block（123）With the 4th
Protect block（124）For tabular, the second half arc connectors（122）For semiarc shape.
6. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：First flipping block（21）
With the 4th protection block（124）Mutually splice, the second flipping block（22）With the described second protection block（112）Mutually splice；Second flipping block
（22）With the 3rd protection block（123）It is upper away from the second half arc connector（122）One end rotate connection.
7. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：First flipping block（21）
With the first guard member（11）First protection block（111）It is upper away from the first half arc connector（113）One end rotate connect
Connect, and can be turned to and the described first protection block（111）The position fitted.
8. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：The first protection block
（111）With the second protection block（112）Respectively with the first half arc connector（113）The two ends of upper and axis parallel connect
Connect, and the first protection block（111）Length be more than described second protection block（112）Length.
9. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：Rotate the first flipping block
（21）With the first protection block（111）Fit, to protect block with the 4th（124）Gear is located at the left angle of attack or left yaw angle together
Opposite side, and by the first flipping block（21）It is fixed on the first protection block（111）On, accordingly, the 3rd protection block（123）
With the second protection block（112）It is located at the opposite sides of the right angle of attack or right yaw angle respectively, and block is protected by the described 3rd
（123）With the described second protection block（112）Interfix.
10. weather vane type angle of attack airspeed sensor protection device as claimed in claim 1, it is characterised in that：Rotate described second
Flipping block（22）So that second flipping block（22）With the described 3rd protection block（123）Fit, to be protected with described second
Block（112）Together gear located at the right angle of attack or right yaw angle opposite side, and by second flipping block（22）It is fixed on institute
State the 3rd protection block（123）On.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710382646.4A CN107238366B (en) | 2017-05-26 | 2017-05-26 | Wind vane type angle of attack airspeed sensor protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710382646.4A CN107238366B (en) | 2017-05-26 | 2017-05-26 | Wind vane type angle of attack airspeed sensor protection device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107238366A true CN107238366A (en) | 2017-10-10 |
| CN107238366B CN107238366B (en) | 2023-02-28 |
Family
ID=59985636
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710382646.4A Active CN107238366B (en) | 2017-05-26 | 2017-05-26 | Wind vane type angle of attack airspeed sensor protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107238366B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100530A (en) * | 2018-06-09 | 2018-12-28 | 成都凯天电子股份有限公司 | Pitot isolates and falls off protective case certainly |
Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3942376A (en) * | 1974-08-14 | 1976-03-09 | Gallington Roger W | Diaphragm type angle of attack indicator |
| US5833177A (en) * | 1995-05-15 | 1998-11-10 | The Boeing Company | Autopilot/flight director overspeed protection system |
| US6457373B1 (en) * | 1998-06-17 | 2002-10-01 | Pruftechnik Dieter Busch Ag | Shock protection device for position-measuring probes |
| US20040070751A1 (en) * | 2002-10-09 | 2004-04-15 | Roland Bergbach | Protective apparatus for the monitoring of a protected zone to be moved with a component |
| US8195346B1 (en) * | 2009-01-21 | 2012-06-05 | Garmin International, Inc. | Envelope protection for mechanically-controlled aircraft |
| JP2012126201A (en) * | 2010-12-14 | 2012-07-05 | Kawasaki Heavy Ind Ltd | Flight controller, and flight vehicle provided with the same |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| US20130062472A1 (en) * | 2009-12-07 | 2013-03-14 | Peter Hedley Stokes | Apparatus for Spacecraft |
| CN103513053A (en) * | 2012-06-29 | 2014-01-15 | 中国科学院大连化学物理研究所 | Device for synchronously adjusting direction of pitot tube sampling hole and sampling gun in rotating mode |
| CN103562682A (en) * | 2011-05-25 | 2014-02-05 | 波音公司 | Primary flight display pitch- and power-based unreliable airspeed symbology |
| CN203486146U (en) * | 2013-09-13 | 2014-03-19 | 山东太古飞机工程有限公司 | Aircraft attack angle weather cock protecting cover |
| CN103693203A (en) * | 2013-12-01 | 2014-04-02 | 太原航空仪表有限公司 | Small-size self-balancing type weather vane |
| CN104006766A (en) * | 2013-02-20 | 2014-08-27 | 空中客车营运有限公司 | Angle measurement probe on board an aircraft and aircraft implementing at least one such probe |
| CN204313836U (en) * | 2015-01-14 | 2015-05-06 | 成都康烨科技有限公司 | Portable solid sizing mark frame |
| US20160114903A1 (en) * | 2014-10-24 | 2016-04-28 | King Abdullah University Of Science And Technology | Flight envelope protection system for unmanned aerial vehicles |
| CN106092205A (en) * | 2016-07-29 | 2016-11-09 | 成都凯天电子股份有限公司 | Omnidirectional's atmosphere parameter measurement spheric probe |
| CN205785169U (en) * | 2016-05-31 | 2016-12-07 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft incidence vane protection grip assembly |
| CN106628234A (en) * | 2016-12-30 | 2017-05-10 | 美迪斯智能装备有限公司 | Arrival hall with swinging telescopic protection device |
| CN207072440U (en) * | 2017-05-26 | 2018-03-06 | 成都凯天电子股份有限公司 | Pitot Wind vane protection device |
-
2017
- 2017-05-26 CN CN201710382646.4A patent/CN107238366B/en active Active
Patent Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3942376A (en) * | 1974-08-14 | 1976-03-09 | Gallington Roger W | Diaphragm type angle of attack indicator |
| US5833177A (en) * | 1995-05-15 | 1998-11-10 | The Boeing Company | Autopilot/flight director overspeed protection system |
| US6457373B1 (en) * | 1998-06-17 | 2002-10-01 | Pruftechnik Dieter Busch Ag | Shock protection device for position-measuring probes |
| US20040070751A1 (en) * | 2002-10-09 | 2004-04-15 | Roland Bergbach | Protective apparatus for the monitoring of a protected zone to be moved with a component |
| US8195346B1 (en) * | 2009-01-21 | 2012-06-05 | Garmin International, Inc. | Envelope protection for mechanically-controlled aircraft |
| US20130062472A1 (en) * | 2009-12-07 | 2013-03-14 | Peter Hedley Stokes | Apparatus for Spacecraft |
| JP2012126201A (en) * | 2010-12-14 | 2012-07-05 | Kawasaki Heavy Ind Ltd | Flight controller, and flight vehicle provided with the same |
| CN103562682A (en) * | 2011-05-25 | 2014-02-05 | 波音公司 | Primary flight display pitch- and power-based unreliable airspeed symbology |
| CN103513053A (en) * | 2012-06-29 | 2014-01-15 | 中国科学院大连化学物理研究所 | Device for synchronously adjusting direction of pitot tube sampling hole and sampling gun in rotating mode |
| CN102806990A (en) * | 2012-07-27 | 2012-12-05 | 沈阳航天新光集团有限公司 | Portable mapping unmanned aerial plane |
| CN104006766A (en) * | 2013-02-20 | 2014-08-27 | 空中客车营运有限公司 | Angle measurement probe on board an aircraft and aircraft implementing at least one such probe |
| CN203486146U (en) * | 2013-09-13 | 2014-03-19 | 山东太古飞机工程有限公司 | Aircraft attack angle weather cock protecting cover |
| CN103693203A (en) * | 2013-12-01 | 2014-04-02 | 太原航空仪表有限公司 | Small-size self-balancing type weather vane |
| US20160114903A1 (en) * | 2014-10-24 | 2016-04-28 | King Abdullah University Of Science And Technology | Flight envelope protection system for unmanned aerial vehicles |
| CN204313836U (en) * | 2015-01-14 | 2015-05-06 | 成都康烨科技有限公司 | Portable solid sizing mark frame |
| CN205785169U (en) * | 2016-05-31 | 2016-12-07 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft incidence vane protection grip assembly |
| CN106092205A (en) * | 2016-07-29 | 2016-11-09 | 成都凯天电子股份有限公司 | Omnidirectional's atmosphere parameter measurement spheric probe |
| CN106628234A (en) * | 2016-12-30 | 2017-05-10 | 美迪斯智能装备有限公司 | Arrival hall with swinging telescopic protection device |
| CN207072440U (en) * | 2017-05-26 | 2018-03-06 | 成都凯天电子股份有限公司 | Pitot Wind vane protection device |
Non-Patent Citations (3)
| Title |
|---|
| UNKNOWN: "Winged Shadow Systems Flight Instruments improved", 《FLYING MODELS》 * |
| 张先华等: "直11型机雷电防护设计及试验研究", 《直升机技术》 * |
| 张羽白等: "三余度迎角传感器可靠性分析及重构技术研究", 《教练机》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100530A (en) * | 2018-06-09 | 2018-12-28 | 成都凯天电子股份有限公司 | Pitot isolates and falls off protective case certainly |
| CN109100530B (en) * | 2018-06-09 | 2024-02-20 | 成都凯天电子股份有限公司 | Airspeed tube self-separating and falling protective sleeve |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107238366B (en) | 2023-02-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107238366A (en) | Weather vane type angle of attack airspeed sensor protection device | |
| ES2320708T3 (en) | AMMUNITION OF ARTILLERIA STABILIZED BY ROTATION AND CORREGIBLE IN ITS TRAJECTORY. | |
| ES2745012T3 (en) | Tip with nozzle charge detection and wireless communication functionality for extendable refueling arm | |
| EP2796344A1 (en) | Vehicle steering control device and steering control method | |
| RU2016118697A (en) | FLIGHT CONTROL DEVICE FOR AIRCRAFT | |
| CN105667834A (en) | Device and method for testing unmanned aerial vehicle | |
| JP2009537024A5 (en) | ||
| CN106585998B (en) | Framework for the control of air data probe power supply | |
| CN104685321A (en) | Method for detecting a fault in a motor arrangement with an electrical machine and motor control unit | |
| US20160187174A1 (en) | Dual sensor head configuration in a fluid flow or liquid level switch | |
| WO2010068320A3 (en) | Steerable spin-stabalized projectile and method | |
| CN209055243U (en) | Charging gun temperature sensing circuit and charging gun | |
| EP3417235B1 (en) | Fuse system for projectile | |
| CN204057800U (en) | A kind of Intelligent shaft is to release miniature electric winding plant | |
| ZA202306511B (en) | Wrapping apparatus and method | |
| US10655493B2 (en) | Arrangement, turbo engine and method for the recognition of a shaft breakage of a shaft | |
| CN207072440U (en) | Pitot Wind vane protection device | |
| MD4439C1 (en) | Octocopter | |
| CN104930298B (en) | One kind can mobile device and its moving method in active steering pipeline | |
| CN103410682A (en) | Wind indicator | |
| CN209357928U (en) | A kind of high temperature based on liquid metal is from fusing heating cable connector | |
| CN105593688A (en) | Method and device for measuring the angle of attack and the sideslip of an aircraft | |
| MY182874A (en) | Propeller fan and blower | |
| CN206734010U (en) | A kind of electric automobile air conditioner PTC heating systems of high security | |
| CN104379447A (en) | Aircraft landing gear arrangement, a kit therefor, an aircraft comprising the same and a method of determining the angular position of an aircraft wheel |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |