CN106918409B - Porous close-proximity total temperature probe - Google Patents

Porous close-proximity total temperature probe Download PDF

Info

Publication number
CN106918409B
CN106918409B CN201710190095.1A CN201710190095A CN106918409B CN 106918409 B CN106918409 B CN 106918409B CN 201710190095 A CN201710190095 A CN 201710190095A CN 106918409 B CN106918409 B CN 106918409B
Authority
CN
China
Prior art keywords
heat exchange
convection heat
probe
holes
temperature
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
CN201710190095.1A
Other languages
Chinese (zh)
Other versions
CN106918409A (en
Inventor
马宏伟
郑春泰
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.)
Beihang University
Original Assignee
Beihang University
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 Beihang University filed Critical Beihang University
Priority to CN201710190095.1A priority Critical patent/CN106918409B/en
Publication of CN106918409A publication Critical patent/CN106918409A/en
Application granted granted Critical
Publication of CN106918409B publication Critical patent/CN106918409B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00Thermometers specially adapted for specific purposes
    • G01K13/02Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00Thermometers specially adapted for specific purposes
    • G01K13/02Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G01K13/024Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow of moving gases
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K7/00Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
    • G01K7/02Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements using thermoelectric elements, e.g. thermocouples
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01KMEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K7/00Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
    • G01K7/16Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements using resistive elements

Abstract

The invention belongs to the technical field of total temperature testing, and discloses a porous adjacent total temperature probe, which comprises a stagnation cover, a convection heat exchange hole, a temperature sensor, a probe supporting rod, a heat insulation sealing piece, a heat insulation sealing cover and a temperature measurement lead. On the stagnation cover, 3 to 5 convection heat exchange holes are arranged along the axial direction or the circumferential direction, and the upper and lower or the left and right sides of the convection heat exchange holes are obliquely opened. The temperature sensor can be various types of thermocouples or thermal resistors, is arranged in the stagnation cover and is fixed through a heat insulation sealing piece, a temperature measurement lead is led out from the tail of the probe supporting rod, and the heat insulation sealing cover can be opened to facilitate replacement of the temperature sensor. Compared with the existing total temperature probe, the temperature measuring part of the invention has small size and larger insensitive angle of airflow, can accurately measure the total temperature of the incoming flow under the condition of larger deflection angle or pitch angle, and is suitable for measuring the total temperature of a flow field with small blade row clearance at the outlet of the centrifugal compressor rotor and larger change of the incoming flow angle.

Description

Porous close-proximity total temperature probe
Technical Field
The invention belongs to the technical field of flow field total temperature testing, and particularly relates to a porous adjacent total temperature probe.
Background
Under various total temperature test conditions, different types of total temperature probes are needed to measure the total temperature of the flow field. The key of accurately measuring the total temperature of the airflow is whether the airflow can be rapidly stagnant at a temperature measuring point and the rapid heat exchange of the gas in the stagnation cover is ensured.
Most of the existing total temperature probes are front hole air inlet and two side holes or rear hole air exhaust, and have the defects of large axial size, small insensitive angle of air flow, incapability of fully stagnating the air flow in a stagnating cover when the pitch angle or deflection angle of incoming flow to be detected is large, and large total temperature measurement error. The armored thermocouple has slow reaction and low frequency response.
The total temperature of the airflow at the outlet of the rotor of the centrifugal compressor is measured, and the total temperature probe is required to be small in axial size and large in airflow insensitivity angle due to small blade row gaps and large inflow angles.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: aiming at the problems of the conventional total temperature probe, the invention provides a porous adjacent total temperature probe which can accurately measure the total temperature of a flow field with small blade row gap and large inflow angle at the rotor outlet of a centrifugal compressor and has the characteristics of small head size of a temperature measuring part and large insensitive angle of airflow.
The technical solution of the invention is as follows:
1. the utility model provides a porous total warm probe of next-door neighbour, by stagnation cover (1), convection heat transfer hole (2), temperature sensor (3), probe branch (4), adiabatic sealing member (5), adiabatic sealed lid (6) and temperature measurement lead wire (7) constitute its characterized in that: the stagnation cover (1) is made of nickel-based alloy materials, one end of the stagnation cover is sealed, the other end of the stagnation cover is connected with the probe supporting rod (4), 3-5 convection heat exchange holes are formed in the stagnation cover (1) along the axial direction or the circumferential direction, and the degree of finish of the outer surface of the stagnation cover is not lower than 3.2 microns.
2. Further, convection heat transfer hole (2) are circular, and the hole diameter is 2 millimeters to 4 millimeters, and it has 3 convection heat transfer holes (2) to open on stagnant cover (1), and convection heat transfer hole (2) can be followed the axial distribution of stagnant cover (1), also can be followed the circumference distribution of stagnant cover (1), and to opening 5 convection heat transfer holes (2) on stagnant cover (1), the convection heat transfer hole is followed stagnant cover (1) axial and circumference and is distributed. The central line of the middle convection heat exchange hole (2) is vertical to the axis of the stagnation cover (1), the central lines of the upper and lower or left and right convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are on a plane and can be intersected at a point, the included angles of the central lines of the two convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are the same, the range is 30-60 degrees, and the spacing distance of the central lines of the adjacent convection heat exchange holes (2) along the surface of the stagnation cover (1) is 1.1-3 times of the diameter of the small hole.
3. Furthermore, the probe supporting rod (4) is supported by high-temperature-resistant alloy and is in an L shape or a straight rod shape. When the probe supporting rod (4) is L-shaped, holes with the diameter of 6 mm to 12 mm are formed in the corners of the L-shaped supporting rod and are sealed by the heat-insulating sealing cover (6), and the heat-insulating sealing cover (6) can be opened and used for replacing the temperature sensor (3). The surface finish is not less than 3.2 microns.
4. Further, the heat insulation sealing piece (5) is made of a ceramic material and is a hollow cylinder, the outer diameter of the heat insulation sealing piece is the same as the inner diameter of the probe supporting rod (4), the heat insulation sealing piece is pasted and fixed at one end of the probe supporting rod (4) through an adhesive, a through hole is formed in the middle of the heat insulation sealing piece, the diameter of the through hole is the same as that of the temperature sensor (3), and the temperature sensor (3) is pasted and fixed.
5. Furthermore, the temperature sensor (3) can be various thermocouples or thermal resistors, the axial position of the head of the sensor corresponds to the convection heat transfer hole (3) in the middle of the stagnation cover (1), and the temperature measurement lead (7) is led out through the tail of the probe support rod (4).
The invention has the advantages and positive effects that:
compared with the traditional total temperature probe, the porous adjacent total temperature probe has the advantages that the diameter of the convection heat exchange holes (2) on the stagnation cover (1) of the probe is larger, the convection heat exchange holes (2) on the two sides are obliquely opened, so that the total temperature probe has a larger air flow insensitive angle, and the total temperature of incoming flow is accurately measured under the condition that the deflection angle or pitch angle of the probe is larger.
The axial direction of the temperature measurement part of the temperature sensor (3) is over against the middle convection heat exchange hole (2), so that the rapid heat exchange of the air flow at the temperature measurement part of the sensor is ensured, and meanwhile, a thermocouple with a smaller time constant can be selected, so that the probe frequency response can be improved.
The heat insulation sealing piece (5) is used for fixing the temperature sensor (3), heat transfer and heat conduction errors can be reduced, the heat insulation sealing cover (6) can be opened, and the temperature sensor (3) is convenient to replace.
The probe has small size of the temperature measuring part and can be applied to a measuring area with narrow space. The method can accurately measure the total temperature of the flow field with small blade row clearance at the outlet of the centrifugal compressor rotor and large change of the incoming flow angle.
Drawings
FIG. 1 is a schematic cross-sectional view of a multi-hole close proximity total temperature probe created by the present invention, with convective heat transfer holes arranged axially along the stagnation housing.
Wherein: 1-stagnation cover, 2-convection heat exchange hole, 3-temperature sensor, 4-probe support rod, 5-heat insulation sealing element, 6-heat insulation sealing cover and 7-temperature measuring lead.
Detailed Description
The invention is further described below with reference to the accompanying drawings:
as shown in figure 1, the porous close-to-total temperature measurement probe comprises a stagnation cover (1), a convection heat transfer hole (2), a temperature sensor (3), a probe support rod (4), a heat insulation sealing piece (5), a heat insulation sealing cover (6) and a temperature measurement lead (7), wherein the stagnation cover (1) is connected with the probe support rod (5), the diameter of the stagnation cover (1) is 3 mm, and the wall thickness of the stagnation cover is 0.3 mm.
The stagnation cover (1) is provided with 3 convection heat exchange holes (2), the holes are circular, the diameters of the convection heat exchange holes (2) are 3 mm, the convection heat exchange holes (2) are distributed along the axial direction of the stagnation cover (1), the central line of the middle convection heat exchange hole (2) is vertical to the axis of the stagnation cover (1), the central lines of the convection heat exchange holes (2) at two sides and the central line of the middle convection heat exchange hole (2) are on the same plane and can be intersected at one point, the included angles of the central lines of the convection heat exchange holes (2) at two sides and the central line of the middle convection heat exchange hole (2) are the same and are 40 degrees, and the interval distance of the central lines of the adjacent convection heat exchange holes (2) is 6 mm along the surface of the stagnation cover (1).
The probe supporting rod (4) is L-shaped, the cross section of the probe supporting rod is circular, the diameter of the probe supporting rod is 8 mm, the wall thickness of the probe supporting rod is 2 mm, and the heat insulation sealing element (5) is fixed in the probe supporting rod (4). The temperature sensor (3) is fixed on the heat insulation sealing element (5), the temperature sensor (3) is positioned on the axis of the stagnation cover (1), the axial position of the temperature measuring end of the temperature sensor corresponds to the convection heat transfer hole (2) in the middle of the stagnation cover (1), and the temperature measuring lead (7) is led out through the tail part of the probe supporting rod (4).
The porous adjacent total temperature probe provided by the embodiment of the invention can accurately measure the total temperature of incoming flow under the condition of a larger deflection angle or pitch angle, and is suitable for measuring the total temperature of a flow field with small blade row clearance and larger change of the incoming flow angle at the rotor outlet of a centrifugal compressor.

Claims (1)

1. The utility model provides a porous total warm probe of next-door neighbour, by stagnation cover (1), convection heat transfer hole (2), temperature sensor (3), probe branch (4), adiabatic sealing member (5), adiabatic sealed lid (6) and temperature measurement lead wire (7) constitute its characterized in that: the stagnation cover (1) is connected with the probe supporting rod (4), 3-5 circular convection heat exchange holes (2) are formed in the stagnation cover (1) according to needs, the middle convection heat exchange hole (2) is vertically perforated, the convection heat exchange holes (2) on the upper side, the lower side or the left side and the right side are obliquely perforated, the head of the temperature sensor (3) corresponds to the middle convection heat exchange hole (2) and is fixed through a heat insulation sealing piece (5), and the heat insulation sealing cover (6) can be opened to facilitate replacement of the temperature sensor (3);
the stagnation cover (1) is a hollow cylinder, the diameter is 2 mm to 6 mm, and the wall thickness is 0.1 mm to 0.6 mm;
the stagnation cover (1) is provided with 3 to 5 convection heat transfer holes (2), the holes are circular, the diameter of each hole is 2 to 4 millimeters, for the total temperature probe provided with 3 convection heat exchange holes (2), the convection heat exchange holes (2) are distributed along the axial direction of the stagnation cover (1) or distributed along the circumferential direction of the stagnation cover (1), the central line of the middle convection heat exchange hole (2) is vertical to the axis of the stagnation cover (1), the central lines of the two side convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are on the same plane and can be intersected at one point, the included angles of the central lines of the two side convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are the same, the range is 30-60 degrees, and the spacing distance of the central lines of the adjacent convection heat exchange holes (2) along the surface of the stagnation cover (1) is 1.1-3 times of the diameter of the convection heat exchange hole; for a total temperature probe with 5 convection heat exchange holes (2) arranged on a stagnation cover (1), the convection heat exchange holes (2) are distributed along the axial direction and the circumferential direction of the stagnation cover (1), the central lines of the upper and lower and left and right side convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are on the same plane and can be intersected at one point, the included angles between the central lines of the upper and lower and left and right side convection heat exchange holes (2) and the central line of the middle convection heat exchange hole (2) are the same, the range is 30-60 degrees, along the surface of the stagnation cover (1), the spacing distance between the central lines of the adjacent convection heat exchange holes (2) is 1.1 times of the diameter of the convection heat exchange hole to 3 times of the diameter of the convection heat exchange hole;
the temperature sensor (3) is positioned on the axis of the stagnation cover (1), the axial position of the temperature measuring end corresponds to the middle convection heat exchange hole (2), and the temperature measuring end is fixed on the probe supporting rod (4) through a heat insulation sealing piece (6);
the probe supporting rod (4) is L-shaped or straight rod, the cross section of the probe supporting rod (4) is circular, the diameter is 6 mm to 12 mm, the wall thickness is 1 mm to 3 mm, when the probe supporting rod (4) is L-shaped, holes with the diameter of 6 mm to 12 mm are formed in the corners of the L-shaped supporting rod and are sealed by heat-insulating sealing covers (6) with the same diameter, the heat-insulating sealing covers are used for facilitating replacement of the temperature sensor (3), and a temperature measuring lead (7) is led out through the tail of the probe supporting rod (4);
the temperature sensor (3) is a thermal resistor.
CN201710190095.1A 2017-03-27 2017-03-27 Porous close-proximity total temperature probe Active CN106918409B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710190095.1A CN106918409B (en) 2017-03-27 2017-03-27 Porous close-proximity total temperature probe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710190095.1A CN106918409B (en) 2017-03-27 2017-03-27 Porous close-proximity total temperature probe

Publications (2)

Publication Number Publication Date
CN106918409A CN106918409A (en) 2017-07-04
CN106918409B true CN106918409B (en) 2020-04-28

Family

ID=59460424

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710190095.1A Active CN106918409B (en) 2017-03-27 2017-03-27 Porous close-proximity total temperature probe

Country Status (1)

Country Link
CN (1) CN106918409B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107449527B (en) * 2017-07-19 2020-01-31 北京航空航天大学 method for improving measurement accuracy of stagnation type total temperature probe
CN108917965B (en) * 2018-05-14 2021-02-02 北京航空航天大学 Total temperature probe head based on thermal resistor and provided with wide insensitive angle

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104122009A (en) * 2014-07-03 2014-10-29 沈阳航空航天大学 Longitudinal-transverse single shield stagnation cover
CN204242603U (en) * 2014-11-11 2015-04-01 中科华核电技术研究院有限公司 Hot channel temperature survey sleeve pipe

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040227519A1 (en) * 2003-05-12 2004-11-18 Mamac Systems, Inc. Fluid sensing probe
JP2008261796A (en) * 2007-04-13 2008-10-30 Denso Corp Temperature-sensor-integrated pressure sensor apparatus

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104122009A (en) * 2014-07-03 2014-10-29 沈阳航空航天大学 Longitudinal-transverse single shield stagnation cover
CN204242603U (en) * 2014-11-11 2015-04-01 中科华核电技术研究院有限公司 Hot channel temperature survey sleeve pipe

Also Published As

Publication number Publication date
CN106918409A (en) 2017-07-04

Similar Documents

Publication Publication Date Title
CN106840271B (en) Combined dynamic probe with temperature correction function for measuring total pressure and speed of fluid
CN109341883A (en) A kind of total temperature measurement device in aeroengine combustor buring room
CN106940230B (en) Nine-hole total temperature measuring probe
CN106918409B (en) Porous close-proximity total temperature probe
CN209148167U (en) A kind of total temperature measurement device in aeroengine combustor buring room
CN204389067U (en) A kind of shallow type temperature checking stove that declines
CN207195266U (en) Stagnation temperature probe between compressor stage
CN106840459A (en) A kind of total temperature measurement probe in ten holes
CN115435929A (en) High-frequency total temperature and total pressure probe
CN106885649B (en) Dynamic temperature and pressure combined probe for measuring subsonic two-dimensional unsteady flow field
CN106918410B (en) Total temperature leaf type probe
CN111076832A (en) Radiation-proof total temperature measuring probe
CN106768826B (en) Dynamic temperature and pressure combined probe for measuring ultrasonic two-dimensional unsteady flow field
CN106840268B (en) Five-hole probe integrating total temperature measurement
CN212082825U (en) Full-parameter probe for measuring high subsonic three-dimensional steady flow field
CN108896198B (en) Straight rod type total temperature probe head based on thermal resistor
CN106969876B (en) Dynamic total pressure probe with temperature correction function
CN111089703A (en) Full-parameter probe for measuring two-dimensional steady-state flow field of boundary layer of outer wall of hub
CN212082624U (en) Radiation-proof total temperature measuring probe
CN106940207B (en) Combined dynamic probe for measuring distortion flow field at inlet of turbine
CN110274801A (en) A kind of isokinetic sampling pipe, the method for sampling and Fuel Concentration Measurement system
CN109799030A (en) A kind of water-cooled pressure measurement probe suitable for high-enthalpy flow
CN201611296U (en) Pressure sensor
CN108489855A (en) A kind of sound-absorbing material flow resistance measuring instrument of temperature-controllable
CN104034532A (en) Total temperature and total pressure wing-shaped sensing part

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