CN109668500A - A kind of blade torsional angle measuring tool - Google Patents

A kind of blade torsional angle measuring tool Download PDF

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Publication number
CN109668500A
CN109668500A CN201811437846.6A CN201811437846A CN109668500A CN 109668500 A CN109668500 A CN 109668500A CN 201811437846 A CN201811437846 A CN 201811437846A CN 109668500 A CN109668500 A CN 109668500A
Authority
CN
China
Prior art keywords
blade
frame
horizontal
measuring tool
edge bracket
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
Application number
CN201811437846.6A
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Chinese (zh)
Other versions
CN109668500B (en
Inventor
马新伟
鲁召朋
徐立国
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.)
AVIC Huiyang Aviation Propeller Co Ltd
Original Assignee
AVIC Huiyang Aviation Propeller Co Ltd
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 AVIC Huiyang Aviation Propeller Co Ltd filed Critical AVIC Huiyang Aviation Propeller Co Ltd
Priority to CN201811437846.6A priority Critical patent/CN109668500B/en
Publication of CN109668500A publication Critical patent/CN109668500A/en
Application granted granted Critical
Publication of CN109668500B publication Critical patent/CN109668500B/en
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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B5/00Measuring arrangements characterised by the use of mechanical techniques
    • G01B5/24Measuring arrangements characterised by the use of mechanical techniques for measuring angles or tapers; for testing the alignment of axes

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • A Measuring Device Byusing Mechanical Method (AREA)

Abstract

The invention discloses a kind of blade torsional angle measuring tools, this patent is made of frame, angle scale, horizontal pointer, mandril etc., the horizontal pointer is rotatably arranged on frame, horizontal pointer is in a horizontal position always by the control of internal water column, mandril aerofoil profile block and 0 degree of blade section location matches, blade section and frame, scale disc spins equal angular when measurement, horizontal pointer is in horizontal always, to read blade section angle.The present invention is simple and convenient, obtains good result in use.

Description

A kind of blade torsional angle measuring tool
Technical field:
The present invention relates to propeller profile measurement fields.
Background technique:
Its shape must be checked after the completion of propeller production, wherein it is aerodynamic most important to influence propeller Factor is the established angle of propeller-blade section, and this patent is a kind of measuring tool of the measurement propeller blade torsional angle of simple and convenient.
Summary of the invention:
Goal of the invention: providing a kind of conveniently locating blades, and blade face torsion can be continuously measured along blade face The device of angle.
Technical solution: a kind of blade torsional angle measuring tool, the measuring tool include fixed frame, mandril, horizontal pointer and angle scale;Institute It states and is respectively arranged with blade inlet edge bracket and trailing edge bracket on frame left and right side frame, for carrying blade;The mandril It is threadedly engaged with frame top frame, mandril lower end is used to blade face holding out against edge bracket in front of the blade and trailing edge bracket;It is described Angle scale be fixed on frame, the horizontal pointer is rotatably arranged on frame, and horizontal pointer is used to indicate angle The angle of scale;The horizontal pointer is strip Shape closed transparent shell, and band bubble liquid is sealed in transparent shell, is constituted Horizontal bubble structure;When blade inlet edge bracket and trailing edge bracket are in the same horizontal position, horizontal pointer is in dial Initial position or zero graduation position.
Further, the horizontal pointer central point is fixed with metal falling body, so that pointer is in horizontality always.More Further, metal falling body is pendulum shape.
Further, the blade inlet edge bracket and trailing edge bracket cooperate respectively at blade inlet edge and rear shape.
Further, the mandril lower end surface is provided with pressure head, pressure head lower end surface and blade face cambered surface positive.
Further, the mandril upper end is equipped with rotating handle.
Blade is fixed, the measured section position of blade is fixed on frame, and is compressed with mandril, by frame into Row is fixed, and reading pointer is directed toward the angle of dial, obtains the windup-degree of the measured section position of existing clamp.
Technical effect:
The present invention is easy to use, and windup-degree reads convenient and easy to operate.The level meter.
Detailed description of the invention:
Fig. 1 is the structural diagram of the present invention;
Fig. 2 is another structural schematic diagram of the present invention;
Wherein: 1- fixed frame, 2- mandril, the horizontal pointer of 3-, 4- angle scale, 5- metal falling body.
Specific embodiment:
A kind of blade torsional angle measuring tool is provided, which includes fixed frame 1, mandril 2, horizontal pointer 3 and angle scale 4;Institute It states and is respectively arranged with blade inlet edge bracket and trailing edge bracket on frame left and right side frame, for carrying blade;The mandril It is threadedly engaged with frame top frame, mandril lower end is used to blade face holding out against edge bracket in front of the blade and trailing edge bracket;It is described Angle scale 4 be fixed on frame, the horizontal pointer is rotatably arranged on frame, and horizontal pointer is used to indicate angle The angle of scale;The horizontal pointer is strip Shape closed transparent shell, and band bubble liquid is sealed in transparent shell, is constituted Horizontal bubble structure;When blade inlet edge bracket and trailing edge bracket are in the same horizontal position, horizontal pointer is in angle scale Initial position or zero graduation position.

Claims (6)

1. a kind of blade torsional angle measuring tool, which includes fixed frame, mandril, horizontal pointer and angle scale;Described frame or so Blade inlet edge bracket and trailing edge bracket are respectively arranged on frame, for carrying blade;The mandril and frame top frame It is threadedly engaged, mandril lower end is used to blade face holding out against edge bracket in front of the blade and trailing edge bracket;The angle scale is solid It is scheduled on frame, the horizontal pointer is rotatably arranged on frame, and horizontal pointer is used to indicate the angle of angle scale; The horizontal pointer is strip Shape closed transparent shell, and band bubble liquid is sealed in transparent shell, constitutes horizontal bubble structure; When blade inlet edge bracket and trailing edge bracket are in the same horizontal position, horizontal pointer be in dial initial position or Zero graduation position.
2. a kind of blade torsional angle measuring tool as described in claim 1, it is characterised in that: the horizontal pointer central point is fixed with gold Belong to falling body, so that pointer is in horizontality always.
3. a kind of blade torsional angle measuring tool as claimed in claim 2, it is characterised in that: metal falling body is pendulum shape.
4. a kind of blade torsional angle measuring tool as claimed in claim 1 or 2, it is characterised in that: after stating blade inlet edge bracket and blade Edge bracket cooperates respectively at blade inlet edge and rear shape.
5. a kind of blade torsional angle measuring tool as claimed in claim 1 or 2, it is characterised in that: the mandril lower end surface is provided with pressure Head, pressure head lower end surface and blade face cambered surface positive.
6. a kind of blade torsional angle measuring tool as claimed in claim 1 or 2, it is characterised in that: the mandril upper end is equipped with rotating handle.
CN201811437846.6A 2018-11-28 2018-11-28 Blade torsion angle measuring tool Active CN109668500B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811437846.6A CN109668500B (en) 2018-11-28 2018-11-28 Blade torsion angle measuring tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811437846.6A CN109668500B (en) 2018-11-28 2018-11-28 Blade torsion angle measuring tool

Publications (2)

Publication Number Publication Date
CN109668500A true CN109668500A (en) 2019-04-23
CN109668500B CN109668500B (en) 2024-02-13

Family

ID=66143286

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811437846.6A Active CN109668500B (en) 2018-11-28 2018-11-28 Blade torsion angle measuring tool

Country Status (1)

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CN (1) CN109668500B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110823072A (en) * 2019-11-19 2020-02-21 中国航发贵州黎阳航空动力有限公司 Turbofan rectifier casing detection method and device

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2716889A (en) * 1952-11-25 1955-09-06 Doman Helicopters Inc Method of determining and adjusting the aerodynamic pitching moment of a full-sized aerodynamic member and apparatus therefor
DE202009007037U1 (en) * 2009-04-09 2009-07-23 Daewoo Shipbuilding & Marine Engineering Co., Ltd. Oars for ships
US20090223073A1 (en) * 2008-03-10 2009-09-10 Ta-Sen Tu Main rotor blade calibration gauge for remote-controlled toy helicopter
CN201693927U (en) * 2009-11-27 2011-01-05 中国直升机设计研究所 Chord line drawing tool for helicopter blade
KR20130026226A (en) * 2011-09-05 2013-03-13 (주)다리온 Fire volume damper
US20130115093A1 (en) * 2011-11-07 2013-05-09 John E. Tharp Wide faced propeller / turbine blade assembly
CN202974145U (en) * 2012-12-05 2013-06-05 浙江海洋学院 Propeller pitch measuring instrument
CN104476453A (en) * 2014-12-23 2015-04-01 洛阳双瑞风电叶片有限公司 Wind power blade web plate perpendicularity regulating tooling and regulating method
CN104501690A (en) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 Tool for measuring chord length of paddle
CN108844442A (en) * 2018-06-26 2018-11-20 南通理工学院 A kind of propeller blades angle detection fixture

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2716889A (en) * 1952-11-25 1955-09-06 Doman Helicopters Inc Method of determining and adjusting the aerodynamic pitching moment of a full-sized aerodynamic member and apparatus therefor
US20090223073A1 (en) * 2008-03-10 2009-09-10 Ta-Sen Tu Main rotor blade calibration gauge for remote-controlled toy helicopter
DE202009007037U1 (en) * 2009-04-09 2009-07-23 Daewoo Shipbuilding & Marine Engineering Co., Ltd. Oars for ships
CN201693927U (en) * 2009-11-27 2011-01-05 中国直升机设计研究所 Chord line drawing tool for helicopter blade
KR20130026226A (en) * 2011-09-05 2013-03-13 (주)다리온 Fire volume damper
US20130115093A1 (en) * 2011-11-07 2013-05-09 John E. Tharp Wide faced propeller / turbine blade assembly
CN202974145U (en) * 2012-12-05 2013-06-05 浙江海洋学院 Propeller pitch measuring instrument
CN104501690A (en) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 Tool for measuring chord length of paddle
CN104476453A (en) * 2014-12-23 2015-04-01 洛阳双瑞风电叶片有限公司 Wind power blade web plate perpendicularity regulating tooling and regulating method
CN108844442A (en) * 2018-06-26 2018-11-20 南通理工学院 A kind of propeller blades angle detection fixture

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王呈;: "发动机叶片榫头角度现场检测方法", 计测技术, no. 04 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110823072A (en) * 2019-11-19 2020-02-21 中国航发贵州黎阳航空动力有限公司 Turbofan rectifier casing detection method and device
CN110823072B (en) * 2019-11-19 2021-01-22 中国航发贵州黎阳航空动力有限公司 Turbofan rectifier casing detection method and device

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