CN106018866A - Integrated quick-disassembling airspeed meter - Google Patents
Integrated quick-disassembling airspeed meter Download PDFInfo
- Publication number
- CN106018866A CN106018866A CN201610639202.XA CN201610639202A CN106018866A CN 106018866 A CN106018866 A CN 106018866A CN 201610639202 A CN201610639202 A CN 201610639202A CN 106018866 A CN106018866 A CN 106018866A
- Authority
- CN
- China
- Prior art keywords
- head
- machine head
- block
- installation block
- airspeed
- 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
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P1/00—Details of instruments
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measuring Fluid Pressure (AREA)
Abstract
The invention discloses an integrated quick-disassembling airspeed meter. The integrated quick-disassembling airspeed meter comprises an airspeed pipe module, an upper machine head fixing installation block, a lower machine head fixing installation block and a machine head installation fixing plate. The upper machine head fixing installation block and the lower machine head fixing installation block are in butt joint together in the vertical direction, the machine head installation fixing plate is installed at the front ends of the upper machine head fixing installation block and the lower machine head fixing installation block, and a cavity is defined by the upper machine head fixing installation block, the lower machine head fixing installation block and the machine head installation fixing plate together. The airspeed pipe module is installed between the upper machine head fixing installation block and the lower machine head fixing installation block, part of the airspeed pipe module is located outside the cavity, part of the airspeed pipe module is located in the cavity, and a static pressing connecting pipe and a movable pressing connecting pipe at the front end stretch out of the machine head installation fixing plate. The integrated quick-disassembling airspeed meter has the advantages that by means of the design of the upper machine head fixing installation block, the lower machine head fixing installation block and the machine head installation fixing plate, the integration of the airspeed meter is achieved, the whole airspeed meter can be quickly replaced, and meanwhile the rigidity and the consistency of an airspeed installation part can be enhanced; the integrated quick-disassembling airspeed meter is convenient to install, safe, reliable and capable of saving time and omitting a jig.
Description
Technical field
The present invention relates to a kind of pitot meter, be specifically related to a kind of integral type Quick Release pitot meter.
Background technology
On the machine of unmanned plane and rapid movement, pitot meter the most all can be installed, be used for carrying out
Test the speed.
As a example by unmanned plane, current pitot meter, is all pitot module to be directly installed on fly
On the head of machine and wing, owing to transportation environment and artificial behaviour in service are uncontrollable, so air speed
Tube module once damaged or blocking, may result in whole aircraft airspeed system damage, aircraft
Cannot normally use.
Summary of the invention
For solving the deficiencies in the prior art, it is an object of the invention to provide a kind of integral type Quick Release
Pitot meter, it both can strengthen again air speed installation portion with quick-replaceable whole pitot module
The rigidity of position and concordance.
In order to realize above-mentioned target, the present invention adopts the following technical scheme that:
Integral type Quick Release pitot meter, including: pitot module (1), aforementioned pitot module (1)
Front end be provided with static pressure connecting tube (2) and dynamic pressure connecting tube (3), it is characterised in that also
Including: fixedly mount on head and under block (4), head, fixedly mount block (5) and head installation
Fixed plate (6),
Fixedly mount fixed installation block (5) under block (4) and head on aforementioned head to dock up and down
Together, head mounting plate (6) is arranged on the front end of the two, and three surrounds one jointly
Individual cavity, aforementioned pitot module (1) is installed on head fixed installation block (4) and head
Between lower fixed installation block (5), a part is positioned at outside cavity, a part of within the cavity,
And static pressure connecting tube (2) and dynamic pressure connecting tube (3) stretch out head mounting plate (6).
Aforesaid integral type Quick Release pitot meter, it is characterised in that fixedly mount block on aforementioned head
(4) block (5) and the machine of fixedly mounting between block (5), under head and is fixedly mounted under head
All fastened by screw between head mounting plate (6).
Aforesaid integral type Quick Release pitot meter, it is characterised in that fixedly mount block on aforementioned head
(4), fixedly mount block (5) under head and head mounting plate (6) is all formed in one.
The invention have benefit that: solid by fixedly mounting under block, head on design head
Determine mounting blocks and head mounting plate, both achieve the integration of pitot meter, again can be quick
Change whole pitot meter, rigidity and the concordance of air speed installation position can also be strengthened simultaneously；This
Outward, the integral type Quick Release pitot meter of the present invention also has easy for installation, safe and reliable, during saving
Between, save the advantages such as tool.
Accompanying drawing explanation
Fig. 1 is the structural representation of a specific embodiment of the integral type Quick Release pitot meter of the present invention
Figure.
The implication of reference in figure: 1-pitot module, 2-static pressure connecting tube, 3-dynamic pressure connect
Fixedly mount on pipe, 4-head and under block, 5-head, fixedly mount block, 6-head mounting plate.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention made concrete introduction.
With reference to Fig. 1, the integral type Quick Release pitot meter of the present invention includes: pitot module (1),
Fixedly mount on head and under block (4), head, fixedly mount block (5) and head mounting plate
(6).Wherein, the front end of pitot module (1) is provided with static pressure connecting tube (2) and dynamic pressure
Connecting tube (3)；Fixedly mount on head and fixedly mount block (5) up and down under block (4) and head
Being docking together, head mounting plate (6) is arranged on the front end of the two, and three encloses jointly
Become a cavity；Pitot module (1) is installed on head fixed installation block (4) and head
Between lower fixed installation block (5), a part is positioned at outside cavity, a part of within the cavity,
And static pressure connecting tube (2) and dynamic pressure connecting tube (3) stretch out head mounting plate (6).
As the preferred scheme of one, head fixedly mounts block (4) and fixedly mounts under head
Fastened by screw (not shown) between block (5), under head, fixedly mount block (5)
And fasten also by screw (not shown) between head mounting plate (6), install
Convenient, safe and reliable, save the time.
Block (5) is fixedly mounted under block (4), head it is further preferred that fixedly mount on head
All it is formed in one with head mounting plate (6), tool can be saved.
Installation process: first pitot module (1) is arranged on head fixed installation block (4)
And fixedly mount under head between block (5), then will fixedly mount block (5) and machine under head
Head mounting plate (6) is tightened together by screw, then will fixedly mount block (4) on head
Tightened together by screw with fixedly mounting block (5) under head, be i.e. assembled into an one
Formula pitot meter, is finally arranged on this integral type pitot meter by head mounting plate (6)
On head.
Unloading process: head mounting plate (6) is separated with head, i.e. completes whole
Integral type pitot meter disassembles from head, and dismantlement work is the quickest.
As can be seen here, by fixedly mounting fixed installation block under block (4), head on design head
And head mounting plate (6) (5), the integration of pitot meter had both been achieved, again can be fast
Speed changes whole pitot meter, can also strengthen rigidity and the concordance of air speed installation position simultaneously.
Additionally, pitot module (1) is an easily damaged unit, by fixing on design head
Block (5) and head mounting plate (6) is fixedly mounted under mounting blocks (4), head, the most real
Show the structure to easily damaged unit to strengthen, extend the service life of pitot meter.
It should be noted that above-described embodiment limits the present invention, all employings etc. the most in any form
The technical scheme obtained with the mode of replacement or equivalent transformation, all falls within the protection model of the present invention
In enclosing.
Claims (3)
1. integral type Quick Release pitot meter, including: pitot module (1), described pitot module
(1) front end is provided with static pressure connecting tube (2) and dynamic pressure connecting tube (3), it is characterised in that
Also include: fixedly mount on head and under block (4), head, fixedly mount block (5) and head peace
Dress fixed plate (6),
Fixedly mount fixed installation block (5) under block (4) and head on described head to dock up and down
Together, head mounting plate (6) is arranged on the front end of the two, and three surrounds one jointly
Individual cavity, described pitot module (1) is installed on head fixed installation block (4) and head
Between lower fixed installation block (5), a part is positioned at outside cavity, a part of within the cavity,
And static pressure connecting tube (2) and dynamic pressure connecting tube (3) stretch out head mounting plate (6).
Integral type Quick Release pitot meter the most according to claim 1, it is characterised in that described
Fixedly mount on head to fixedly mount under block (4) and head and fix between block (5), under head
All fastened by screw between mounting blocks (5) and head mounting plate (6).
Integral type Quick Release pitot meter the most according to claim 1 and 2, it is characterised in that
Fixedly mount fixed installation block (5) and head under block (4), head on described head and install solid
Determine plate (6) to be all formed in one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610639202.XA CN106018866A (en) | 2016-08-05 | 2016-08-05 | Integrated quick-disassembling airspeed meter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610639202.XA CN106018866A (en) | 2016-08-05 | 2016-08-05 | Integrated quick-disassembling airspeed meter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106018866A true CN106018866A (en) | 2016-10-12 |
Family
ID=57133954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610639202.XA Pending CN106018866A (en) | 2016-08-05 | 2016-08-05 | Integrated quick-disassembling airspeed meter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106018866A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10739372B2 (en) | 2018-06-15 | 2020-08-11 | Rosemount Aerospace Inc. | Detachable probe and sealing of an integrated air data sensor |
| US10809276B2 (en) | 2018-06-15 | 2020-10-20 | Rosemount Aerospace Inc. | Detachable probe and sealing of an integrated air data sensor |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2786353A (en) * | 1953-10-02 | 1957-03-26 | Norris E Slabaugh | Pitot tube cover |
| US3781895A (en) * | 1972-11-22 | 1973-12-25 | Raytheon Co | Combined pitot tube and antenna |
| US4677858A (en) * | 1986-03-13 | 1987-07-07 | Ohnhaus Buford U | Double-acting pitot tube |
| CN1670534A (en) * | 2004-03-15 | 2005-09-21 | 清华大学 | Minisize low speed airspeedometer for mini aircrafts |
| US20050252288A1 (en) * | 2004-05-11 | 2005-11-17 | Igor Giterman | Using non-contact forming as a novel method to attach parts in fluid sensor assemblies |
| CN102141447A (en) * | 2010-12-31 | 2011-08-03 | 中国航天科技集团公司第六研究院第十一研究所 | Total temperature/total pressure and static probe |
| CN202281781U (en) * | 2011-10-10 | 2012-06-20 | 北京雪迪龙科技股份有限公司 | Pitot tube flow meter and pitot tube thereof |
| CN103353538A (en) * | 2013-07-18 | 2013-10-16 | 广东电网公司电力科学研究院 | Pitot tube apparatus for multiple-detection-point flue gas flow velocity measuring |
| CN203428039U (en) * | 2013-05-30 | 2014-02-12 | 江西洪都航空工业集团有限责任公司 | Aircraft nose pitot installing and fixing device |
| CN203849280U (en) * | 2014-04-29 | 2014-09-24 | 国家电网公司 | Length adjustable backrest velocity measurement tube applicable to any pipe diameters |
| CN205193090U (en) * | 2015-11-16 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Airspeed meter module |
| CN205374505U (en) * | 2015-12-28 | 2016-07-06 | 江阴市嘉臣光电科技有限公司 | Can tear pitot tube device that trades fast open |
| CN205861713U (en) * | 2016-08-05 | 2017-01-04 | 北京奇正数元科技股份有限公司 | Integral type Quick Release pitot meter |
-
2016
- 2016-08-05 CN CN201610639202.XA patent/CN106018866A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2786353A (en) * | 1953-10-02 | 1957-03-26 | Norris E Slabaugh | Pitot tube cover |
| US3781895A (en) * | 1972-11-22 | 1973-12-25 | Raytheon Co | Combined pitot tube and antenna |
| US4677858A (en) * | 1986-03-13 | 1987-07-07 | Ohnhaus Buford U | Double-acting pitot tube |
| CN1670534A (en) * | 2004-03-15 | 2005-09-21 | 清华大学 | Minisize low speed airspeedometer for mini aircrafts |
| US20050252288A1 (en) * | 2004-05-11 | 2005-11-17 | Igor Giterman | Using non-contact forming as a novel method to attach parts in fluid sensor assemblies |
| CN102141447A (en) * | 2010-12-31 | 2011-08-03 | 中国航天科技集团公司第六研究院第十一研究所 | Total temperature/total pressure and static probe |
| CN202281781U (en) * | 2011-10-10 | 2012-06-20 | 北京雪迪龙科技股份有限公司 | Pitot tube flow meter and pitot tube thereof |
| CN203428039U (en) * | 2013-05-30 | 2014-02-12 | 江西洪都航空工业集团有限责任公司 | Aircraft nose pitot installing and fixing device |
| CN103353538A (en) * | 2013-07-18 | 2013-10-16 | 广东电网公司电力科学研究院 | Pitot tube apparatus for multiple-detection-point flue gas flow velocity measuring |
| CN203849280U (en) * | 2014-04-29 | 2014-09-24 | 国家电网公司 | Length adjustable backrest velocity measurement tube applicable to any pipe diameters |
| CN205193090U (en) * | 2015-11-16 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Airspeed meter module |
| CN205374505U (en) * | 2015-12-28 | 2016-07-06 | 江阴市嘉臣光电科技有限公司 | Can tear pitot tube device that trades fast open |
| CN205861713U (en) * | 2016-08-05 | 2017-01-04 | 北京奇正数元科技股份有限公司 | Integral type Quick Release pitot meter |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10739372B2 (en) | 2018-06-15 | 2020-08-11 | Rosemount Aerospace Inc. | Detachable probe and sealing of an integrated air data sensor |
| US10809276B2 (en) | 2018-06-15 | 2020-10-20 | Rosemount Aerospace Inc. | Detachable probe and sealing of an integrated air data sensor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161012 |
|
| RJ01 | Rejection of invention patent application after publication |