CN103697791A - Spraying pipe diameter measurement tool for engine - Google Patents
Spraying pipe diameter measurement tool for engine Download PDFInfo
- Publication number
- CN103697791A CN103697791A CN201310657335.6A CN201310657335A CN103697791A CN 103697791 A CN103697791 A CN 103697791A CN 201310657335 A CN201310657335 A CN 201310657335A CN 103697791 A CN103697791 A CN 103697791A
- Authority
- CN
- China
- Prior art keywords
- ratchet
- engine
- measuring tool
- rotary screw
- pipe diameter
- 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
Images
Landscapes
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
The invention discloses a spraying pipe diameter measurement tool for an engine. The spraying pipe diameter measurement tool for the engine comprises a ruler measurement head, a fixing clamping hoop, a fixing nut, a replaceable measurement head, a ratchet, a pawl, a force adjustment bolt, a spring, a pawl fixing wheel, a rotary screw and a measurement tool shell, wherein the ruler is arranged on the rotary screw through the fixing clamping hoop; the fixing nut is arranged on the measurement tool shell; the replaceable measurement head is fixed to the measurement tool shell through the fixing nut; the rotary screw is arranged on the measurement tool shell and is rotatable; the ruler measurement head is connected with the rotary screw through screw threads; the pawl fixing wheel is fixed with the rotary screw integrally through a radial threaded pin; the pawl is fixed to the pawl fixing wheel through the spring and the force adjustment bolt; the ratchet is connected with the pawl fixing wheel through the pawl. The spraying pipe diameter measurement tool for the engine has the advantages that the diameter measurement of a spraying nozzle of the engine in a working state is realized by simulating airflow expansion force, the accuracy of spraying area measurement of the engine is guaranteed, and moreover, the spraying pipe diameter measurement tool for the engine is simple in structure, convenient to operate and easy to implement.
Description
Technical field
The present invention relates to diameter of nozzle of aircraft engine tail fields of measurement, particularly a kind of engine jet pipe diameter measuring tool.
Background technology
By adjustable jet tube critical cross-section area, change the operating mode of engine, for guaranteeing the accuracy of engine operating condition, needing can Measurement accuracy area of injection orifice.Because engine tail nozzle is comprised of adjustment sheet, adjustment sheet is deformable, and the major function of jet pipe is that high temperature, high-pressure gas are expanded and accelerate and discharge, and pipe critical cross-section is subject to gas tension, can bad student's distortion.Existing survey instrument cannot analog gas bulging force, cannot measure the working diameter of jet pipe.
Summary of the invention
The object of the invention is, in order to solve prior art, cannot measure engine jet pipe working diameter problem, spy provides a kind of engine jet pipe diameter measuring tool.
The invention provides a kind of engine jet pipe diameter measuring tool, it is characterized in that: described engine jet pipe diameter measuring tool, comprises scale gauge head 1, fixing hoop 2, hold-down nut 3, test probe replaceable 4, ratchet 5, ratchet 6, adjusts power bolt 7, spring 8, ratchet fast pulley 9, rotary screw 10, measuring tool housing 11;
Wherein: scale gauge head 1 is arranged on rotary screw 10 by fixing hoop 2, hold-down nut 3 is arranged on measuring tool housing 11;
Test probe replaceable 4 is fixed on measuring tool housing 11 by hold-down nut 3, rotary screw 10 is installed on measuring tool housing 11 and can be rotated, scale gauge head 1 and rotary screw 10 are threaded connection, ratchet fast pulley 9 is by radially threaded and rotary screw 10 are fixed as one, ratchet 6 is fixed on ratchet fast pulley 9 by spring 8 and the power of tune bolt 7, and ratchet 5 is connected with ratchet fast pulley 9 by ratchet 6.
Described measuring tool housing 11 is framed structure.
On described scale gauge head 1, with scale.
By rotation torsion-adjustable ratchet device, make scale gauge head protruding, when reaching the gas tension of jet pipe, torsion-adjustable ratchet structure is thrown off automatically, scale gauge head stops stretching out, and tightens the bolt on fixing hoop, and scale gauge head is fixed on to measuring tool object, prevent that scale gauge head from moving, and takes out reading by measuring tool.
Advantage of the present invention:
Engine jet pipe diameter measuring tool of the present invention, simulates flow expansion power by employing, has realized the diameter measurement of engine nozzle duty, guarantee the accuracy of engine spray area measurement, and it is simple in structure, easy to operate, is easy to realize.
Accompanying drawing explanation
Below in conjunction with drawings and the embodiments, the present invention is further detailed explanation:
Fig. 1 is engine jet pipe diameter measuring tool measuring tool schematic diagram.
Embodiment
Embodiment 1
The invention provides a kind of engine jet pipe diameter measuring tool, it is characterized in that: described engine jet pipe diameter measuring tool, comprises scale gauge head 1, fixing hoop 2, hold-down nut 3, test probe replaceable 4, ratchet 5, ratchet 6, adjusts power bolt 7, spring 8, ratchet fast pulley 9, rotary screw 10, measuring tool housing 11;
Wherein: scale gauge head 1 is arranged on rotary screw 10 by fixing hoop 2, hold-down nut 3 is arranged on measuring tool housing 11;
Test probe replaceable 4 is fixed on measuring tool housing 11 by hold-down nut 3, rotary screw 10 is installed on measuring tool housing 11 and can be rotated, scale gauge head 1 and rotary screw 10 are threaded connection, ratchet fast pulley 9 is by radially threaded and rotary screw 10 are fixed as one, ratchet 6 is fixed on ratchet fast pulley 9 by spring 8 and the power of tune bolt 7, and ratchet 5 is connected with ratchet fast pulley 9 by ratchet 6.
Described measuring tool housing 11 is framed structure.
On described scale gauge head 1, with scale.
By rotation torsion-adjustable ratchet device, make scale gauge head protruding, when reaching the gas tension of jet pipe, torsion-adjustable ratchet structure is thrown off automatically, scale gauge head stops stretching out, and tightens the bolt on fixing hoop, and scale gauge head is fixed on to measuring tool object, prevent that scale gauge head from moving, and takes out reading by measuring tool.
Claims (3)
1. an engine jet pipe diameter measuring tool, is characterized in that: described engine jet pipe diameter measuring tool, comprises scale gauge head (1), fixing hoop (2), hold-down nut (3), test probe replaceable (4), ratchet (5), ratchet (6), tune power bolt (7), spring (8), ratchet fast pulley (9), rotary screw (10), measuring tool housing (11);
Wherein: it is upper that scale gauge head (1) is arranged on rotary screw (10) by fixing hoop (2), and hold-down nut (3) is arranged on measuring tool housing (11);
Test probe replaceable (4) is fixed on measuring tool housing (11) by hold-down nut (3), rotary screw (10) is installed measuring tool housing (11) above and can be rotated, scale gauge head (1) and rotary screw (10) are threaded connection, ratchet fast pulley (9) is by radially threaded and rotary screw (10) are fixed as one, ratchet (6) is by spring (8) and adjust power bolt (7) to be fixed on ratchet fast pulley (9) above, and ratchet (5) is connected with ratchet fast pulley (9) by ratchet (6).
2. according to engine jet pipe diameter measuring tool claimed in claim 1, it is characterized in that: described measuring tool housing (11) is framed structure.
3. according to engine jet pipe diameter measuring tool claimed in claim 1, it is characterized in that: described scale gauge head (1) is upper, with scale.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310657335.6A CN103697791B (en) | 2013-12-05 | 2013-12-05 | A kind of engine jet pipe diameter measuring tool |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310657335.6A CN103697791B (en) | 2013-12-05 | 2013-12-05 | A kind of engine jet pipe diameter measuring tool |
Publications (2)
Publication Number | Publication Date |
---|---|
CN103697791A true CN103697791A (en) | 2014-04-02 |
CN103697791B CN103697791B (en) | 2016-09-07 |
Family
ID=50359403
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310657335.6A Active CN103697791B (en) | 2013-12-05 | 2013-12-05 | A kind of engine jet pipe diameter measuring tool |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103697791B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105004246A (en) * | 2015-05-15 | 2015-10-28 | 中国航空工业集团公司沈阳发动机设计研究所 | Engine nozzle diameter measuring tool |
CN108050915A (en) * | 2017-12-14 | 2018-05-18 | 中国航发沈阳发动机研究所 | A kind of loading measuring device for being used to measure engine variable nozzle pluggage |
CN111504173A (en) * | 2020-04-27 | 2020-08-07 | 中国航空工业集团公司北京航空精密机械研究所 | Engine nozzle diameter measuring device |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH1089907A (en) * | 1996-09-20 | 1998-04-10 | Toshiba Corp | Measuring device of inner diameter |
JP2000346631A (en) * | 1999-06-02 | 2000-12-15 | Toyota Motor Corp | Hole diameter measuring apparatus |
CN101598524A (en) * | 2008-06-04 | 2009-12-09 | 株式会社三丰 | Milscale |
CN101738159A (en) * | 2009-12-04 | 2010-06-16 | 沈阳黎明航空发动机(集团)有限责任公司 | Device and method for measuring diameter of nozzle of aircraft engine tail |
CN102080947A (en) * | 2009-11-26 | 2011-06-01 | 中国航空工业集团公司沈阳发动机设计研究所 | Measuring tool for diameter of adjustable convergence spout |
CN103075987A (en) * | 2012-12-27 | 2013-05-01 | 中国燃气涡轮研究院 | Device for dynamically measuring aeroengine nozzle diameter |
CN103162592A (en) * | 2013-03-06 | 2013-06-19 | 中国航空工业集团公司沈阳发动机设计研究所 | Plug-type axially symmetric spray pipe outlet diameter measuring tool |
-
2013
- 2013-12-05 CN CN201310657335.6A patent/CN103697791B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH1089907A (en) * | 1996-09-20 | 1998-04-10 | Toshiba Corp | Measuring device of inner diameter |
JP2000346631A (en) * | 1999-06-02 | 2000-12-15 | Toyota Motor Corp | Hole diameter measuring apparatus |
CN101598524A (en) * | 2008-06-04 | 2009-12-09 | 株式会社三丰 | Milscale |
CN102080947A (en) * | 2009-11-26 | 2011-06-01 | 中国航空工业集团公司沈阳发动机设计研究所 | Measuring tool for diameter of adjustable convergence spout |
CN101738159A (en) * | 2009-12-04 | 2010-06-16 | 沈阳黎明航空发动机(集团)有限责任公司 | Device and method for measuring diameter of nozzle of aircraft engine tail |
CN103075987A (en) * | 2012-12-27 | 2013-05-01 | 中国燃气涡轮研究院 | Device for dynamically measuring aeroengine nozzle diameter |
CN103162592A (en) * | 2013-03-06 | 2013-06-19 | 中国航空工业集团公司沈阳发动机设计研究所 | Plug-type axially symmetric spray pipe outlet diameter measuring tool |
Non-Patent Citations (1)
Title |
---|
苏金友等: "激光测距技术在高空舱内测量喷口面积试验分析", 《面向航空试验测试技术-2013年航空试验测试技术峰会暨学术交流会论文集》, 20 August 2013 (2013-08-20), pages 67 - 71 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105004246A (en) * | 2015-05-15 | 2015-10-28 | 中国航空工业集团公司沈阳发动机设计研究所 | Engine nozzle diameter measuring tool |
CN108050915A (en) * | 2017-12-14 | 2018-05-18 | 中国航发沈阳发动机研究所 | A kind of loading measuring device for being used to measure engine variable nozzle pluggage |
CN111504173A (en) * | 2020-04-27 | 2020-08-07 | 中国航空工业集团公司北京航空精密机械研究所 | Engine nozzle diameter measuring device |
Also Published As
Publication number | Publication date |
---|---|
CN103697791B (en) | 2016-09-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN203824683U (en) | Pre-tightening force testing device for bolt | |
CN104019950B (en) | A kind of pilot system of testing airplane tank vibrating fatigue performance | |
CN103697791A (en) | Spraying pipe diameter measurement tool for engine | |
CN203083802U (en) | Flow measuring and controlling experiment device practical for aviation/aerospace | |
CN104122030A (en) | Method and system for measuring air flow pressure in test room | |
CN104359448A (en) | Continuous angle measurement device of intermediate case air bleed valve | |
CN109029899B (en) | Device capable of accurately simulating flow field of nacelle of engine | |
CN106932139B (en) | Four-hole pressure leaf-shaped probe | |
CN204944736U (en) | A kind of total pressure measurement probe | |
Hoberg et al. | Characterization of test conditions in the notre dame arc-heated wind tunnel | |
CN204286304U (en) | A kind of axisymmetric nozzle throat diameter survey instrument | |
CN205157158U (en) | Hypersonic wind tunnel pressure measurement structure | |
CN202947847U (en) | Spark leak detector testing device | |
CN204493246U (en) | A kind of lift fan system for air cushion ship model performance curve gauging means | |
CN203570484U (en) | Special tool for measuring stroke of oil sprayer | |
CN205067051U (en) | Hypersonic wind tunnel temperature measurement structure | |
CN103528618B (en) | A kind of signal generating method of automobile instrument detection signal generation platform | |
CN202928632U (en) | V-shaped inner cone flowmeter | |
CN202013207U (en) | Integrated performance testboard for pneumatic accessories of aircraft | |
CN203758473U (en) | Apparatus for detecting jet cone angle of tracer gas nozzle | |
CN103075987B (en) | Device for dynamically measuring aeroengine nozzle diameter | |
CN204284083U (en) | Measure the device of oil nozzle for flow | |
CN204214599U (en) | A kind of automobile cooling fan dynamic balancing measurement instrument | |
CN202274843U (en) | Detection device for distance between segment end face and sphere center | |
CN204142414U (en) | A kind of gas meter needle deflection mechanism |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |