CN107727305A - A kind of method for measuring hydraulic actuator axial force - Google Patents
A kind of method for measuring hydraulic actuator axial force Download PDFInfo
- Publication number
- CN107727305A CN107727305A CN201710913368.0A CN201710913368A CN107727305A CN 107727305 A CN107727305 A CN 107727305A CN 201710913368 A CN201710913368 A CN 201710913368A CN 107727305 A CN107727305 A CN 107727305A
- Authority
- CN
- China
- Prior art keywords
- hydraulic actuator
- axial force
- compensating plate
- temperature
- auricle
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
- G01L9/02—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means by making use of variations in ohmic resistance, e.g. of potentiometers, electric circuits therefor, e.g. bridges, amplifiers or signal conditioning
- G01L9/04—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means by making use of variations in ohmic resistance, e.g. of potentiometers, electric circuits therefor, e.g. bridges, amplifiers or signal conditioning of resistance-strain gauges
- G01L9/045—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means by making use of variations in ohmic resistance, e.g. of potentiometers, electric circuits therefor, e.g. bridges, amplifiers or signal conditioning of resistance-strain gauges with electric temperature compensating means
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Measurement Of Force In General (AREA)
Abstract
A kind of method for measuring hydraulic actuator axial force, first by the hoop sleeve matched with hydraulic actuator end cap external diameter on hydraulic actuator end cap, piece of metal piece is then fixed at clip auricle, it is pasted onto by temperature-compensating plate on sheet metal, foil gauge Parallel Symmetric is pasted onto on hydraulic actuator auricle, finally by temperature-compensating plate, foil gauge composition Wheatstone bridge is connected with strain testing equipment, strain testing device measuring hydraulic actuator is in the axial force itself moved during folding and unfolding, effectively eliminating temperature-compensating plate and being brought by hydraulic actuator self-deformation is influenceed, and then reduce the measurement error to hydraulic actuator axial force, make test result more accurate.
Description
Technical field
The present invention relates to engineer applied technical field, more particularly to a kind of method for measuring hydraulic actuator axial force.
Background technology
Various types of hydraulic actuators are usually mounted with plane hydraulic system, are distributed in each power of hydraulic system
Position is performed, hydraulic actuator is the key element of aircraft, and take off landing, the cabin door open and close of aircraft will be directly affected by breaking down
Deng flight safety will be threatened when failure is serious;Need to survey pressurized strut power in airplane design, carried to design, testing
Supported for data.
Hydraulic actuator itself often moves when carrying out folding and unfolding, is difficult to find preferably to paste temperature in machine upper-deck cabin
The position of compensating plate is spent, the method for generally measuring hydraulic actuator power is that foil gauge is attached to the auricle of hydraulic actuator fixing end
On, temperature-compensating plate is attached on the hydraulic actuator end cap of auricle, but hydraulic actuator is after intracavitary leads to hydraulic pressure or stress
Certain deformation can also occur for end cap so that temperature-compensating plate resistance change, in turn result in measurement error.
The content of the invention
Technical problem solved by the invention is to provide a kind of method for measuring hydraulic actuator axial force, with solution
The shortcomings that stating in background technology.
Technical problem solved by the invention is realized using following technical scheme:
The hoop sleeve matched with hydraulic actuator end cap external diameter, is mounted in by a kind of method for measuring hydraulic actuator axial force first
On hydraulic actuator end cap, piece of metal piece is then fixed at clip auricle, is pasted onto by temperature-compensating plate on sheet metal,
Foil gauge Parallel Symmetric is pasted onto on hydraulic actuator auricle, finally by temperature-compensating plate, foil gauge form Wheatstone bridge with
Strain testing equipment connects, strain testing device measuring hydraulic actuator in the axial force itself moved during folding and unfolding,
Effectively eliminating temperature-compensating plate and being brought by hydraulic actuator self-deformation is influenceed, and then is reduced to hydraulic actuator axial force
Measurement error, make test result more accurate.
In the present invention, clip is r c steel clamping band.
In the present invention, sheet metal uses identical material with hydraulic actuator earrings.
In the present invention, foil gauge is two panels, and Parallel Symmetric is pasted onto on hydraulic actuator auricle lower planes.
Beneficial effect:The present invention is fixed with sheet metal by being loaded hoop in hydraulic actuator end sleeve of top cover at clip auricle,
It is pasted onto by temperature-compensating plate on sheet metal, effectively eliminates the shadow that temperature-compensating plate is brought by hydraulic actuator self-deformation
Ring, and then reduce the measurement error to hydraulic actuator axial force, make test result more accurate.
Brief description of the drawings
Fig. 1 is the structural representation of presently preferred embodiments of the present invention.
Fig. 2 is the yoke configurations schematic diagram in presently preferred embodiments of the present invention.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is expanded on further.
Referring to a kind of method of Fig. 1~Fig. 2 measurement hydraulic actuator axial force, clip 1 is sleeved on hydraulic pressure first and made
On dynamic cylinder end cap 2, clip 1 matches with the external diameter of hydraulic actuator end cap 2, is then bolted at clip auricle 3 a piece of
With the earrings material identical sheet metal 6 of hydraulic actuator 4, it is pasted onto by temperature-compensating plate 5 on sheet metal 6, two panels foil gauge 7
Parallel Symmetric is pasted onto on the lower planes of hydraulic actuator auricle 8, and temperature-compensating plate 5, foil gauge 7 finally are formed into favour stone electricity
Bridge is connected with strain testing equipment, and strain testing device measuring hydraulic actuator 4 is in the axle itself moved during folding and unfolding
Xiang Li, effectively eliminating temperature-compensating plate 5 and being brought by the self-deformation of hydraulic actuator 4 is influenceed, and then is reduced to hydraulic actuation
The measurement error of 4 axial forces of cylinder, makes test result more accurate.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the simply explanation described in above-described embodiment and specification is originally
The principle of invention, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its
Equivalent thereof.
Claims (4)
- A kind of 1. method for measuring hydraulic actuator axial force, it is characterised in that first will be with hydraulic actuator end cap external diameter The hoop sleeve matched somebody with somebody then fixes piece of metal piece on the hydraulic actuator end cap at clip auricle, by temperature-compensating plate It is pasted onto on sheet metal, foil gauge Parallel Symmetric is pasted onto on hydraulic actuator auricle, finally by temperature-compensating plate, foil gauge group It is connected into Wheatstone bridge with strain testing equipment, strain testing device measuring hydraulic actuator itself occurs when carrying out folding and unfolding The axial force of motion, effectively eliminating temperature-compensating plate and being brought by hydraulic actuator self-deformation is influenceed.
- 2. a kind of method for measuring hydraulic actuator axial force according to claim 1, it is characterised in that clip is rubber The steel clamping band of parcel.
- 3. a kind of method for measuring hydraulic actuator axial force according to claim 1, it is characterised in that sheet metal and liquid Pressure pressurized strut earrings uses identical material.
- A kind of 4. method for measuring hydraulic actuator axial force according to claim 1, it is characterised in that foil gauge two Piece, Parallel Symmetric are pasted onto on hydraulic actuator auricle lower planes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710913368.0A CN107727305A (en) | 2017-09-30 | 2017-09-30 | A kind of method for measuring hydraulic actuator axial force |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710913368.0A CN107727305A (en) | 2017-09-30 | 2017-09-30 | A kind of method for measuring hydraulic actuator axial force |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107727305A true CN107727305A (en) | 2018-02-23 |
Family
ID=61209423
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710913368.0A Pending CN107727305A (en) | 2017-09-30 | 2017-09-30 | A kind of method for measuring hydraulic actuator axial force |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107727305A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110864798A (en) * | 2019-11-18 | 2020-03-06 | 中国矿业大学(北京) | Temperature correction device and micro-vibration measurement system |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020172446A1 (en) * | 1998-12-04 | 2002-11-21 | Fernald Mark R. | Pressure-isolated Bragg grating temperature sensor |
CN101397903A (en) * | 2008-11-05 | 2009-04-01 | 大庆油田有限责任公司 | Method for monitoring sleeve circumferential strain by using optical fibre grating sensor |
CN202870024U (en) * | 2012-10-19 | 2013-04-10 | 沈阳建筑大学 | Intelligent piezoelectric aggregate sensor for concrete structure |
CN103335772A (en) * | 2013-07-15 | 2013-10-02 | 东北石油大学 | Temperature and pressure sensor of fiber Bragg grating |
CN105675184A (en) * | 2016-02-19 | 2016-06-15 | 沈阳埃克斯邦科技有限公司 | Compensation method for zero point temperature drift of silicon strain gage bridge circuit |
-
2017
- 2017-09-30 CN CN201710913368.0A patent/CN107727305A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020172446A1 (en) * | 1998-12-04 | 2002-11-21 | Fernald Mark R. | Pressure-isolated Bragg grating temperature sensor |
CN101397903A (en) * | 2008-11-05 | 2009-04-01 | 大庆油田有限责任公司 | Method for monitoring sleeve circumferential strain by using optical fibre grating sensor |
CN202870024U (en) * | 2012-10-19 | 2013-04-10 | 沈阳建筑大学 | Intelligent piezoelectric aggregate sensor for concrete structure |
CN103335772A (en) * | 2013-07-15 | 2013-10-02 | 东北石油大学 | Temperature and pressure sensor of fiber Bragg grating |
CN105675184A (en) * | 2016-02-19 | 2016-06-15 | 沈阳埃克斯邦科技有限公司 | Compensation method for zero point temperature drift of silicon strain gage bridge circuit |
Non-Patent Citations (1)
Title |
---|
苏清友: "《航空涡喷、涡扇发动机主要零部件定寿指南》", 29 February 2004, 航空工业出版社 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110864798A (en) * | 2019-11-18 | 2020-03-06 | 中国矿业大学(北京) | Temperature correction device and micro-vibration measurement system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105649817B (en) | Vector thrust loading device for attitude control engine | |
CN104697761B (en) | A kind of following loading method of movable aerofoil | |
CN107782481B (en) | Ground calibration method for torsion arm load of double-wheel strut type nose landing gear | |
Sturm et al. | Failure of CFRP airframe sandwich panels under crash-relevant loading conditions | |
CN105300595B (en) | The balance loading head and loading method of link model calibration | |
CN104931250B (en) | A kind of full machine loading dynamic test method of high-lift system | |
CN204214583U (en) | Brake torque measurement mechanism in aircraft taxi wheels-locked testing | |
CN107727305A (en) | A kind of method for measuring hydraulic actuator axial force | |
CN107766612B (en) | Method for measuring wing load in connecting wing structure form | |
CN107757947A (en) | A kind of adjustable hydraulic pressure of rigidity does device debugging stand and adjustment method | |
CN105466371A (en) | Apparatus of measuring aircraft landing gear wheel shaft end position and measurement method thereof | |
CN104596697B (en) | Undercarriage wheel brake kinetic moment measuring method | |
CN105865920A (en) | Four-direction equally-loaded stress application device for cellular materials | |
CN103604545B (en) | A kind of bolt tension force measures structure | |
CN103926068A (en) | Torsion device used for large horizontal tail shaft torsion fatigue test | |
CN104500459A (en) | Hydraulic gravity balancing system realizing micro gravity environment | |
CN108982041B (en) | Air rudder core excitation testing device | |
CN111003198A (en) | Airplane cabin door connecting rod force fixing method and device | |
CN215812027U (en) | A loading device for static test | |
CN204979273U (en) | Front wing drive mechanism analogue means | |
Prasad et al. | Design And Structural Analysis Of Aircraft Landing Gear Using Different Alloys | |
Hu et al. | Design technique of the test static for large curvature composite radome | |
Li | Structural Validation Testing for X-57 Airworthiness | |
CN106951585B (en) | Modeling method of elastic-plastic bending deformation force-limiting structure | |
Chen et al. | The Residual Strength Test and Analysis of Composite Rudder After Lightning Strike |
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 | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180223 |