CN108709576B - Harrow type instrument test structure - Google Patents

Harrow type instrument test structure Download PDF

Info

Publication number
CN108709576B
CN108709576B CN201810581031.9A CN201810581031A CN108709576B CN 108709576 B CN108709576 B CN 108709576B CN 201810581031 A CN201810581031 A CN 201810581031A CN 108709576 B CN108709576 B CN 108709576B
Authority
CN
China
Prior art keywords
instrument
radius
rake
meter
rake type
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.)
Active
Application number
CN201810581031.9A
Other languages
Chinese (zh)
Other versions
CN108709576A (en
Inventor
高修磊
盖国盛
王鑫
冯忠帅
曹焱焱
张小刚
李文博
陈旭东
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.)
AECC Shenyang Engine Research Institute
Original Assignee
AECC Shenyang Engine Research Institute
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 AECC Shenyang Engine Research Institute filed Critical AECC Shenyang Engine Research Institute
Priority to CN201810581031.9A priority Critical patent/CN108709576B/en
Publication of CN108709576A publication Critical patent/CN108709576A/en
Application granted granted Critical
Publication of CN108709576B publication Critical patent/CN108709576B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

The invention relates to the technical field of aero-engine experimental tests, in particular to a rake type instrument, which comprises: an instrument strut; and a plurality of meter measuring points are uniformly distributed at one end of the meter supporting rod along an arc with the radius of R1, and R1 is equal to the radius of the rake type meter testing position. The rake type instrument has the advantages that the instrument measuring points are distributed in an arc shape, the arc radius of the instrument measuring points is equal to the radius of the position of the rake type instrument to be measured, so that the test error caused by radial change of the instrument measuring points in a flow channel is eliminated, the accuracy of test data is improved, and a reliable basis is provided for performance evaluation of an aircraft engine, a fan/compressor and a turbine.

Description

Harrow type instrument test structure
Technical Field
The invention relates to the technical field of experimental tests of aero-engines, in particular to a rake type instrument test structure.
Background
The rake type test instrument can simultaneously complete the measurement of parameters within a grid distance range at one time, so that the rake type instrument is frequently used for temperature and pressure tests in aero-engines, fans/compressors and turbine tests.
The distribution of the rake type instrument measuring points on the current engineering is in-line distribution, so that in the test, parameters of an aircraft engine, a fan/compressor and a turbine within a grid distance range are measured by using the rake type instrument measuring points, and the obtained test data of each measuring point cannot eliminate test errors caused by radial change of the instrument measuring points in a flow channel.
Disclosure of Invention
The object of the present invention is to provide a solution to the above mentioned problems.
The technical scheme of the invention is as follows:
a rake meter comprising:
an instrument strut;
and a plurality of instrument measuring points are uniformly distributed at one end of the instrument supporting rod along an arc with the radius of R1, and R1 is equal to the radius of the rake-type instrument testing position.
Preferably, the rake type meter further includes: the instrument mounting seat is provided with a through hole, one end of the instrument supporting rod, which is back to the instrument measuring point, is arranged in the through hole, the surface of one side, which faces the instrument measuring point, of the instrument mounting seat is in an arc shape with the radius of R2, and the length of the instrument supporting rod between the instrument measuring point and the instrument mounting seat is L; wherein the content of the first and second substances,
r2 is equal to the radius of the inner surface of the measurement flow channel of the rake type instrument;
l is equal to the distance from the test position of the rake meter to the inner surface of the measurement flow channel.
The rake type instrument has the advantages that the rake type instrument is provided, the instrument measuring points of the rake type instrument are distributed in an arc shape, the radius of the arc shape is equal to the radius of the position to be tested of the rake type instrument, therefore, the test error caused by the radial change of the instrument measuring points in a flow channel is eliminated, the accuracy of test data is improved, and a reliable basis is provided for the performance evaluation of an aircraft engine, a fan/compressor and a turbine.
Drawings
Fig. 1 is a schematic structural view of the rake type meter of the present invention.
Detailed Description
In order to make the implementation objects, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below with reference to the accompanying drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are only some, but not all embodiments of the invention. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience in describing the present invention and for simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be taken as limiting the scope of the present invention.
The present invention is described in further detail below with reference to fig. 1.
The present invention provides a rake-type instrument, comprising:
an instrument strut 1;
a plurality of instrument measuring points 2 are uniformly distributed at one end of an instrument supporting rod 1 along an arc with the radius of R1, and R1 is equal to the radius of a rake type instrument testing position.
Further, the rake type meter further includes: the instrument mounting seat 3 is provided with a through hole, one end of the instrument strut 1, which is back to the instrument measuring point, is arranged in the through hole, the surface of one side of the instrument mounting seat 3, which faces the instrument measuring point 2, is in an arc shape with the radius of R2, and the length of the instrument strut 1 between the instrument measuring point 2 and the instrument mounting seat 3 is L; wherein the content of the first and second substances,
r2 is equal to the radius of the inner surface of the measurement flow channel of the rake type instrument;
l is equal to the distance from the test position of the rake meter to the inner surface of the measurement flow channel.
The side surface of the instrument mounting seat 3 facing the instrument measuring point 1 is designed to be arc-shaped, the radius of the arc-shaped is equal to the radius of the inner surface of the rake-shaped instrument measuring flow channel, and after the rake-shaped instrument is mounted, the inner surface of the instrument mounting seat 3 is flush with the inner surface of the measuring flow channel, so that the interference of the deviation of the instrument mounting seat 3 and the inner surface of the flow channel on a test flow field is avoided, and the accuracy and the reliability of the rake-shaped instrument test are improved.
The above description is only for the specific embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention are included in the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the appended claims.

Claims (1)

1. A rake meter, comprising:
an instrument strut;
a plurality of meter measuring points are uniformly distributed at one end of the meter supporting rod along an arc with the radius of R1, and R1 is equal to the radius of the rake-type meter testing position; further comprising:
the instrument mounting seat is provided with a through hole, one end of the instrument supporting rod, which is back to the instrument measuring point, is arranged in the through hole, the surface of one side, which faces the instrument measuring point, of the instrument mounting seat is in an arc shape with the radius of R2, and the length of the instrument supporting rod between the instrument measuring point and the instrument mounting seat is L;
wherein the content of the first and second substances,
r2 is equal to the radius of the inner surface of the measurement flow channel of the rake type instrument;
l is equal to the distance from the testing position of the rake type instrument to the inner surface of the measuring flow channel.
CN201810581031.9A 2018-06-05 2018-06-05 Harrow type instrument test structure Active CN108709576B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810581031.9A CN108709576B (en) 2018-06-05 2018-06-05 Harrow type instrument test structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810581031.9A CN108709576B (en) 2018-06-05 2018-06-05 Harrow type instrument test structure

Publications (2)

Publication Number Publication Date
CN108709576A CN108709576A (en) 2018-10-26
CN108709576B true CN108709576B (en) 2021-10-01

Family

ID=63871438

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810581031.9A Active CN108709576B (en) 2018-06-05 2018-06-05 Harrow type instrument test structure

Country Status (1)

Country Link
CN (1) CN108709576B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110954333A (en) * 2019-12-05 2020-04-03 中国航发四川燃气涡轮研究院 Probe and method of using the same

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001174294A (en) * 1999-12-16 2001-06-29 Ishikawajima Harima Heavy Ind Co Ltd Variable natural vibration frequency measuring rake
CN202793795U (en) * 2012-09-18 2013-03-13 中航商用航空发动机有限责任公司 Fixed measuring rake for measuring pneumatic parameters
KR101185999B1 (en) * 2009-12-23 2013-03-14 한국항공우주연구원 Rake Module and Measuring Apparatus having the Same
CN103115747A (en) * 2012-12-21 2013-05-22 中国飞行试验研究院 Large-size composite material air inlet passage measuring rake
CN203595596U (en) * 2013-10-30 2014-05-14 北京航天益森风洞工程技术有限公司 Boundary layer measuring rake for wind tunnel measurement
CN204202846U (en) * 2014-09-30 2015-03-11 中国航天科技集团公司第六研究院第十一研究所 A kind of total pressure measurement rake
CN106289784A (en) * 2016-08-02 2017-01-04 中国航空工业集团公司沈阳发动机设计研究所 A kind of inlet distortion stagnation pressure rake structure
CN107631753A (en) * 2017-09-18 2018-01-26 中国人民解放军空军工程大学 A kind of aviation turbojet engine wake flow field test device
CN107748381A (en) * 2017-09-01 2018-03-02 兰州空间技术物理研究所 A kind of semicircle rake ion thruster beam divergence angle test device
CN107917793A (en) * 2017-11-14 2018-04-17 中国空气动力研究与发展中心高速空气动力研究所 The multiple rows of pressure measurement rake device of one kind experiment
CN207423242U (en) * 2017-11-20 2018-05-29 中国航发沈阳发动机研究所 The instrument configuration of adjustable angle

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8011251B1 (en) * 2010-03-24 2011-09-06 General Electric Company Bifurcated pressure instrumentation rake
US8944678B2 (en) * 2011-05-13 2015-02-03 General Electric Company Instrumentation rake assembly
CN103335773B (en) * 2013-02-20 2017-01-25 江苏安邦伟业人工环境有限公司 Pipeline gas pressure measuring device
CN203414115U (en) * 2013-07-12 2014-01-29 皇家空调设备工程(广东)有限公司 Air quantity sensor with double-cross structure
CN203848879U (en) * 2014-03-27 2014-09-24 江阴市节流装置厂有限公司 Logarithmic liner cross section air volume measuring device

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001174294A (en) * 1999-12-16 2001-06-29 Ishikawajima Harima Heavy Ind Co Ltd Variable natural vibration frequency measuring rake
KR101185999B1 (en) * 2009-12-23 2013-03-14 한국항공우주연구원 Rake Module and Measuring Apparatus having the Same
CN202793795U (en) * 2012-09-18 2013-03-13 中航商用航空发动机有限责任公司 Fixed measuring rake for measuring pneumatic parameters
CN103115747A (en) * 2012-12-21 2013-05-22 中国飞行试验研究院 Large-size composite material air inlet passage measuring rake
CN203595596U (en) * 2013-10-30 2014-05-14 北京航天益森风洞工程技术有限公司 Boundary layer measuring rake for wind tunnel measurement
CN204202846U (en) * 2014-09-30 2015-03-11 中国航天科技集团公司第六研究院第十一研究所 A kind of total pressure measurement rake
CN106289784A (en) * 2016-08-02 2017-01-04 中国航空工业集团公司沈阳发动机设计研究所 A kind of inlet distortion stagnation pressure rake structure
CN107748381A (en) * 2017-09-01 2018-03-02 兰州空间技术物理研究所 A kind of semicircle rake ion thruster beam divergence angle test device
CN107631753A (en) * 2017-09-18 2018-01-26 中国人民解放军空军工程大学 A kind of aviation turbojet engine wake flow field test device
CN107917793A (en) * 2017-11-14 2018-04-17 中国空气动力研究与发展中心高速空气动力研究所 The multiple rows of pressure measurement rake device of one kind experiment
CN207423242U (en) * 2017-11-20 2018-05-29 中国航发沈阳发动机研究所 The instrument configuration of adjustable angle

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
一种复合结构航空测量耙模态仿真方法;陶冶 等;《机械研究与应用》;20170630;第30卷(第152期);第90-95页 *
复合结构航空测量耙振动应变测量试验研究;陶冶 等;《科学技术与工程》;20160228;第16卷(第6期);第249-253页 *
某型发动机测量耙动态特性分析;董瑞国 等;《内燃机与配件》;20180228(第4期);第26-27页 *
某型飞机进气道测量耙研制;和永进 等;《燃气涡轮试验与研究》;20080831;第21卷(第3期);第59-62页 *
飞机进气道流场品质测量耙风洞校准试验研究;高颖 等;《科学技术与工程》;20150630;第15卷(第18期);第235-238页 *

Also Published As

Publication number Publication date
CN108709576A (en) 2018-10-26

Similar Documents

Publication Publication Date Title
US20210278312A1 (en) Dynamic Strain Field Measuring Method and System for Rotor Blade Based on Blade Tip Timing
US12007309B2 (en) Non-contact dynamic strain field measuring method and system for rotating blade
US8806926B2 (en) Device for multipoint acquisition/distribution of fluid, in particular probe for tapping pressure in a turbomachine air inlet
US10281297B2 (en) Blade tip timing
CN107747897B (en) Combine centring type blade angle degree measuring device
CN108709576B (en) Harrow type instrument test structure
US8413501B2 (en) Wake measurement probe
US10156440B2 (en) Blade tip timing
CN106885649B (en) Dynamic temperature and pressure combined probe for measuring subsonic two-dimensional unsteady flow field
US9599452B2 (en) Non-contact electrical machine air gap measurement tool
US9274027B2 (en) Apparatus and process for measuring the depth of a groove in a rotor of a gas turbine engine
CN219736607U (en) Platinum resistance total temperature probe head with outer layer stagnation cover
CN103196350A (en) Angle measuring device
CN203837641U (en) Measuring tool of X-axial symmetry degree of valve seat hole in valve body
CN112179665B (en) Method for acquiring inlet stagnation pressure of low-pressure turbine performance test
CN109307463A (en) A kind of cubing and method for examining special-shaped part length dimension
CN104677324A (en) Detection device of rail distance
US3959886A (en) Classification gauge for vane clusters
CN204988122U (en) Piston compressor is high, and utensil is examined in measuring special use
US9897431B2 (en) Edge detector
KR101326280B1 (en) Portable center of gravity measuring device
CN105180788B (en) A kind of babinet measuring device
CN111609940B (en) Infrared temperature measurement method
CN216558627U (en) Valve stroke measuring assembly
BENNETT Measurements of periodic flow in rotating machinery

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