CN109668500B - Blade torsion angle measuring tool - Google Patents

Blade torsion angle measuring tool Download PDF

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Publication number
CN109668500B
CN109668500B CN201811437846.6A CN201811437846A CN109668500B CN 109668500 B CN109668500 B CN 109668500B CN 201811437846 A CN201811437846 A CN 201811437846A CN 109668500 B CN109668500 B CN 109668500B
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CN
China
Prior art keywords
blade
horizontal
frame
pointer
angle
Prior art date
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Active
Application number
CN201811437846.6A
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Chinese (zh)
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CN109668500A (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
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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
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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 blade torsion angle measuring tool which comprises a frame, an angle dial, a horizontal pointer, a push rod and the like, wherein the horizontal pointer is rotatably arranged on the frame, the horizontal pointer is controlled by an internal water column to be always in a horizontal position, an ejector rod wing section block is matched with a blade section 0-degree position, the blade section is rotated by the same angle as the frame and the dial during measurement, and the horizontal pointer is always in the horizontal position, so that the blade section angle is read. The invention is simple and convenient, and has good effect in the use process.

Description

Blade torsion angle measuring tool
Technical field:
the invention relates to the field of propeller appearance detection.
The background technology is as follows:
the shape of the propeller must be checked after the propeller is produced, wherein the most important factor affecting the aerodynamic force of the propeller is the installation angle of the blade profile.
The invention comprises the following steps:
the invention aims to: the device is convenient and quick to position the blade and can continuously measure the torsion angle of the blade surface along the blade surface.
The technical scheme is as follows: the blade torsion angle measuring tool comprises a fixed frame, a push rod, a horizontal pointer and an angle dial; the left and right rims of the frame are respectively provided with a blade front edge bracket and a blade rear edge bracket for bearing the blades; the ejector rod is in threaded fit with the top frame of the frame, and the lower end of the ejector rod is used for tightly pushing the leaf surface on the front edge bracket and the rear edge bracket of the leaf; the angle dial is fixed on the frame, the horizontal pointer is rotatably arranged on the frame, and the horizontal pointer is used for indicating the angle of the angle dial; the horizontal pointer is a strip-shaped closed transparent shell, and bubble-carrying liquid is sealed in the transparent shell to form a horizontal bubble structure; when the blade leading edge support and the blade trailing edge support are in the same horizontal position, the horizontal pointer is in the initial position or the zero scale position of the dial.
Further, a metal falling body is fixed at the center point of the horizontal pointer, so that the pointer is always in a horizontal state. Furthermore, the metal pendant is pendulum-shaped.
Further, the blade leading edge bracket and the blade trailing edge bracket are respectively matched with the blade leading edge and the blade trailing edge in a shape.
Further, a pressure head is arranged on the lower end face of the ejector rod, and the lower end face of the pressure head is matched with the cambered surface profile of the leaf surface.
Further, a rotary handle is arranged at the upper end of the ejector rod.
Fixing the blade, fixing the position of the measured section of the blade on the frame, pressing the frame by using the ejector rod, fixing the frame, reading the angle of the pointer pointing to the dial, and obtaining the torsion angle of the currently clamped position of the measured section.
The technical effects are as follows:
the invention has the advantages of convenient use, convenient reading of torsion angle and simple operation. The level gauge.
Description of the drawings:
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a schematic view of another embodiment of the present invention;
wherein: 1-fixed frame, 2-ejector rod, 3-horizontal pointer, 4-angle scale and 5-metal pendant.
The specific embodiment is as follows:
the blade torsion angle measuring tool comprises a fixed frame 1, a push rod 2, a horizontal pointer 3 and an angle dial 4; the left and right rims of the frame are respectively provided with a blade front edge bracket and a blade rear edge bracket for bearing the blades; the ejector rod is in threaded fit with the top frame of the frame, and the lower end of the ejector rod is used for tightly pushing the leaf surface on the front edge bracket and the rear edge bracket of the leaf; the angle dial 4 is fixed on the frame, the horizontal pointer is rotatably arranged on the frame, and the horizontal pointer is used for indicating the angle of the angle dial; the horizontal pointer is a strip-shaped closed transparent shell, and bubble-carrying liquid is sealed in the transparent shell to form a horizontal bubble structure; when the blade leading edge support and the blade trailing edge support are positioned at the same horizontal position, the horizontal pointer is positioned at the initial position or the zero scale position of the angle scale.

Claims (2)

1. The blade torsion angle measuring tool comprises a fixed frame, a push rod, a horizontal pointer and an angle dial; the left and right rims of the frame are respectively provided with a blade front edge bracket and a blade rear edge bracket for bearing the blades; the ejector rod is in threaded fit with the top frame of the frame, and the lower end of the ejector rod is used for tightly pushing the leaf surface on the front edge bracket and the rear edge bracket of the leaf; the blade front edge support and the blade rear edge support are respectively matched with the front edge and the rear edge of the blade in shape; the lower end face of the ejector rod is provided with a pressure head, and the lower end face of the pressure head is matched with the cambered surface profile of the leaf surface; the upper end of the ejector rod is provided with a rotary handle; the angle dial is fixed on the frame, the horizontal pointer is rotatably arranged on the frame, and the horizontal pointer is used for indicating the angle of the angle dial; the horizontal pointer is a strip-shaped closed transparent shell, and bubble-carrying liquid is sealed in the transparent shell to form a horizontal bubble structure; when the blade front edge support and the blade rear edge support are positioned at the same horizontal position, the horizontal pointer is positioned at the initial position or the zero scale position of the dial; the metal falling body is fixed at the center point of the horizontal pointer, so that the pointer is always in a horizontal state.
2. A blade twist gauge as defined in claim 1, wherein: the metal pendant body is pendulum-shaped.
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 CN109668500A (en) 2019-04-23
CN109668500B true CN109668500B (en) 2024-02-13

Family

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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

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CN (1) CN109668500B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Citations (8)

* 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
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
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 Ship propeller blade angle detection clamp

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7637026B2 (en) * 2008-03-10 2009-12-29 Ta-Sen Tu Main rotor blade calibration gauge for remote-controlled toy helicopter
US20130115093A1 (en) * 2011-11-07 2013-05-09 John E. Tharp Wide faced propeller / turbine blade assembly

Patent Citations (8)

* 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
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
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 Ship propeller blade angle detection clamp

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
发动机叶片榫头角度现场检测方法;王呈;;计测技术(04);全文 *

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