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CN106706764A - Composite parts in-situ ultrasonic detection probe extending and positioning device - Google Patents

Composite parts in-situ ultrasonic detection probe extending and positioning device Download PDF

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Publication number
CN106706764A
CN106706764A CN201611056903.7A CN201611056903A CN106706764A CN 106706764 A CN106706764 A CN 106706764A CN 201611056903 A CN201611056903 A CN 201611056903A CN 106706764 A CN106706764 A CN 106706764A
Authority
CN
China
Prior art keywords
button
handle
spring
screw
lever
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.)
Pending
Application number
CN201611056903.7A
Other languages
Chinese (zh)
Inventor
董德秀
左一
熊瑛
朱萍
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.)
Shenyang Liming Aero Engine Group Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201611056903.7A priority Critical patent/CN106706764A/en
Publication of CN106706764A publication Critical patent/CN106706764A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22Details, e.g. general constructional or apparatus details
    • G01N29/24Probes

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  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Abstract

The invention relates to a composite parts in-situ ultrasonic detection probe extending and positioning device, which comprises a handle, a plug screw, a button, a steel pipe, a spring, a lever, a belleville spring, a probe, a spring, a first cylindrical pin, a second cylindrical pin, a nut, a screw and a marker pen, wherein the handle and the plug screw are screwed tightly through screw threads; a non-through hole is formed in the plug screw; the spring is arranged in the hole, and contacts with the button so as to ensure the button to be automatically returned to the normal position after being pressed; meanwhile, the first cylindrical pin penetrates through the button so as to be connected with the handle, so that the button can rotate around the first cylindrical pin; the second cylindrical pin is also connected with the handle, so that the second cylindrical pin blocks the button so as to prevent the button from rotating to the outside of a handle body. The composite parts in-situ ultrasonic detection probe extending and positioning device provided by the invention has the advantages that a probe can be sent to a detection part at a complete machine state of an airplane, so that in situ detection is realized. The composite partsby pass duct case in-situ ultrasonic detection probe extending and positioning device is simple in structure, convenient to operate, and lower in cost, can be used for detecting a composite partsby pass duct casetrouble location at a no-decomposed state of the airplane.

Description

A kind of composite material parts original position ultrasonic inspection probe extension positioner
Technical field
It is more particularly to a kind of compound the present invention relates to aero-engine composite class part original position ultrasound detection field Material parts original position ultrasonic inspection probe extension positioner.
Background technology
Contain casing outside composite and employ the pressure composite manufacture of high-temperature resistance carbon fiber base layer of resin, and in engine clothes Used first during labour, in use outside composite contain casing once occurred in that by high-temperature gas burn, foreign matter wound, And vibration the problems such as cause genetic defects to extend, it is necessary to carry out situ mass monitoring using ultrasonic technology, i.e., aircraft regardless of Realized under solution state to containing casing ultrasound detection outside composite;Contain casing single-piece outside composite, using manual ultrasound detection, This technology ultrasound examination is used under aircraft not decomposing state, because accessory size is larger, there is no detecting tool, hand cannot Interior of aircraft is stretched into, single-piece manual inspection is not suitable for line.
The content of the invention
The purpose of the present invention is, in order to probe are sent into detection position in airplane complete machine state, to realize in situ detection, special There is provided a kind of composite material parts original position ultrasonic inspection probe extension positioner.
The invention provides a kind of composite material parts original position ultrasonic inspection probe extension positioner, it is characterised in that: Described composite material parts original position ultrasonic inspection probe extension positioner, including handle 1, plug screw 2, button 3, steel pipe 4, bullet Spring 5, lever 6, butterfly spring 7, probe 8, spring 9, the first straight pin 10, the second straight pin 11, nut 12, screw 15, mark Pen 16, steel wire 17, nylon wire 18;
Wherein:Handle 1 is screwed with plug screw 2 by screw thread, there is a hole for not insertion in plug screw 2, the first spring 9 put into In this hole, contacted with button 3 and ensure that button automatically returns to original position after pressing, while the first straight pin 10 passes through button 3 and handle 1 Connection, enables button 3 to be rotated around the first straight pin 10;Second straight pin 11 is same and handle 1 is connected, its act on be block by Button 3 controls it to be unlikely to outside rotation to handle main body;
There is screw thread the one end of steel pipe 4, is connected with handle 1, is locked by nut 12, and the other end is connected by gluing with spring 5, The other end of spring 5 is connected again by gluing with probe 8, it is ensured that 8 self adaptations of probe are adjacent to tested position;There is a spiral shell on probe 8 Nail, screw 14 is coupled through lever 6, butterfly spring 7, lever 6 is rotated around screw 14, the bending of the one end of lever 6, folder Firmly marker pen 16, are locked by screw 15;
Steel wire 17 is fastened with nylon wire 18, and through steel pipe 4, the one end of steel wire 17 is connected with button 3, nylon wire one end and lever 6 connections, realize button press 3, and by steel wire 17 and nylon wire 18, lever 6 is rotated, and drive the tested position of the contact of marker pen 16 to do Go out mark.
Described steel pipe 4 is bend pipe structure.
The described outside of handle 1 carries Anti-slip cover.
Advantages of the present invention:
Probe can be sent to detection position in airplane complete machine state, realize in situ detection.Contain casing outside composite in situ Ultrasonic inspection probe extension positioning device structure is simple and convenient to operate, cost is relatively low, and it is right to be realized under aircraft not decomposing state Composite casing trouble location is detected that this head extends the application of positioner, and ultrasonic wave can not only periodically supervised Control whole machine state part quality to be possibly realized, and engine depot repair cost can be saved, shorten proof cycle, while can The experience of preciousness is provided with the outfield in situ detection for other model engine crankcase class parts.
Brief description of the drawings
Below in conjunction with the accompanying drawings and implementation method the present invention is further detailed explanation:Fig. 1 is former composite material parts Position ultrasonic inspection probe extension positioning device structure schematic diagram;Fig. 2 is A to schematic diagram.
Specific embodiment
Embodiment 1
A kind of composite material parts original position ultrasonic inspection probe extension positioner is present embodiments provided, its feature exists In:Described composite material parts original position ultrasonic inspection probe extension positioner, including handle 1, plug screw 2, button 3, steel pipe 4, spring 5, lever 6, butterfly spring 7, probe 8, spring 9, the first straight pin 10, the second straight pin 11, nut 12, screw 15, Marker pen 16, steel wire 17, nylon wire 18;
Wherein:Handle 1 is screwed with plug screw 2 by screw thread, there is a hole for not insertion in plug screw 2, the first spring 9 put into In this hole, contacted with button 3 and ensure that button automatically returns to original position after pressing, while the first straight pin 10 passes through button 3 and handle 1 Connection, enables button 3 to be rotated around the first straight pin 10;Second straight pin 11 is same and handle 1 is connected, its act on be block by Button 3 controls it to be unlikely to outside rotation to handle main body;
There is screw thread the one end of steel pipe 4, is connected with handle 1, is locked by nut 12, and the other end is connected by gluing with spring 5, The other end of spring 5 is connected again by gluing with probe 8, it is ensured that 8 self adaptations of probe are adjacent to tested position;There is a spiral shell on probe 8 Nail, screw 14 is coupled through lever 6, butterfly spring 7, lever 6 is rotated around screw 14, the bending of the one end of lever 6, folder Firmly marker pen 16, are locked by screw 15;
Steel wire 17 is fastened with nylon wire 18, and through steel pipe 4, the one end of steel wire 17 is connected with button 3, nylon wire one end and lever 6 connections, realize button press 3, and by steel wire 17 and nylon wire 18, lever 6 is rotated, and drive the tested position of the contact of marker pen 16 Make a mark.
Described steel pipe 4 is bend pipe structure.
The described outside of handle 1 carries Anti-slip cover.
Embodiment 2
A kind of composite material parts original position ultrasonic inspection probe extension positioner is present embodiments provided, its feature exists In:Described composite material parts original position ultrasonic inspection probe extension positioner, including handle 1, plug screw 2, button 3, steel pipe 4, spring 5, lever 6, butterfly spring 7, probe 8, spring 9, the first straight pin 10, the second straight pin 11, nut 12, screw 15, Marker pen 16, steel wire 17, nylon wire 18;
Wherein:Handle 1 is screwed with plug screw 2 by screw thread, there is a hole for not insertion in plug screw 2, the first spring 9 put into In this hole, contacted with button 3 and ensure that button automatically returns to original position after pressing, while the first straight pin 10 passes through button 3 and handle 1 Connection, enables button 3 to be rotated around the first straight pin 10;Second straight pin 11 is same and handle 1 is connected, its act on be block by Button 3 controls it to be unlikely to outside rotation to handle main body;
There is screw thread the one end of steel pipe 4, is connected with handle 1, is locked by nut 12, and the other end is connected by gluing with spring 5, The other end of spring 5 is connected again by gluing with probe 8, it is ensured that 8 self adaptations of probe are adjacent to tested position;There is a spiral shell on probe 8 Nail, screw 14 is coupled through lever 6, butterfly spring 7, lever 6 is rotated around screw 14, the bending of the one end of lever 6, folder Firmly marker pen 16, are locked by screw 15;
Steel wire 17 is fastened with nylon wire 18, and through steel pipe 4, the one end of steel wire 17 is connected with button 3, nylon wire one end and lever 6 connections, realize button press 3, and by steel wire 17 and nylon wire 18, lever 6 is rotated, and drive the tested position of the contact of marker pen 16 to do Go out mark.
Described steel pipe 4 is bend pipe structure.
Embodiment 3
A kind of composite material parts original position ultrasonic inspection probe extension positioner is present embodiments provided, its feature exists In:Described composite material parts original position ultrasonic inspection probe extension positioner, including handle 1, plug screw 2, button 3, steel pipe 4, spring 5, lever 6, butterfly spring 7, probe 8, spring 9, the first straight pin 10, the second straight pin 11, nut 12, screw 15, Marker pen 16, steel wire 17, nylon wire 18;
Wherein:Handle 1 is screwed with plug screw 2 by screw thread, there is a hole for not insertion in plug screw 2, the first spring 9 put into In this hole, contacted with button 3 and ensure that button automatically returns to original position after pressing, while the first straight pin 10 passes through button 3 and handle 1 Connection, enables button 3 to be rotated around the first straight pin 10;Second straight pin 11 is same and handle 1 is connected, its act on be block by Button 3 controls it to be unlikely to outside rotation to handle main body;
There is screw thread the one end of steel pipe 4, is connected with handle 1, is locked by nut 12, and the other end is connected by gluing with spring 5, The other end of spring 5 is connected again by gluing with probe 8, it is ensured that 8 self adaptations of probe are adjacent to tested position;There is a spiral shell on probe 8 Nail, screw 14 is coupled through lever 6, butterfly spring 7, lever 6 is rotated around screw 14, the bending of the one end of lever 6, folder Firmly marker pen 16, are locked by screw 15;
Steel wire 17 is fastened with nylon wire 18, and through steel pipe 4, the one end of steel wire 17 is connected with button 3, nylon wire one end and lever 6 connections, realize button press 3, and by steel wire 17 and nylon wire 18, lever 6 is rotated, and drive the tested position of the contact of marker pen 16 to do Go out mark.
The described outside of handle 1 carries Anti-slip cover.

Claims (3)

1. a kind of composite material parts original position ultrasonic inspection probe extends positioner, it is characterised in that:Described composite Part original position ultrasonic inspection probe extension positioner, including handle (1), plug screw (2), button (3), steel pipe (4), spring (5), Lever (6), butterfly spring (7) is popped one's head in (8), spring (9), the first straight pin (10), the second straight pin (11), nut (12), spiral shell Nail (15), marker pen (16), steel wire (17), nylon wire (18);
Wherein:Handle (1) is screwed with plug screw (2) by screw thread, there is a hole for not insertion in plug screw (2), spring (9) put into In this hole, contacted with button (3) and ensure that button automatically returns to original position after pressing, while the first straight pin (10) is through button (3) It is connected with handle (1), button (3) is rotated around the first straight pin (10);Second straight pin (11) is same and handle (1) connects Connect, its effect is to block button (3) to control it to be unlikely to outside rotation to handle main body;
There is screw thread steel pipe (4) one end, is connected with handle (1), is locked by nut (12), and the other end is by gluing and spring (5) Connection, spring (5) other end is connected again by gluing with probe (8), it is ensured that probe (8) self adaptation is adjacent to tested position;Visit There is a screw hole on head (8), screw (14) is coupled through lever (6), butterfly spring (7), make the lever (6) can be around screw (14) rotate, marker pen (16) is clamped in the bending of lever (6) one end, is locked by screw (15);
Steel wire (17) is fastened with nylon wire (18), and through steel pipe (4), steel wire (17) one end is connected with button (3), nylon wire one end It is connected with lever (6), realizes button press (3), by steel wire (17) and nylon wire (18), lever (6) is rotated, and drives marker pen (16) tested position is contacted to make a mark.
2. according to the composite material parts original position ultrasonic inspection probe extension positioner described in claim 1, it is characterised in that: Described steel pipe (4) is bend pipe structure.
3. according to the composite material parts original position ultrasonic inspection probe extension positioner described in claim 1, it is characterised in that: Anti-slip cover is carried outside described handle (1).
CN201611056903.7A 2016-11-25 2016-11-25 Composite parts in-situ ultrasonic detection probe extending and positioning device Pending CN106706764A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611056903.7A CN106706764A (en) 2016-11-25 2016-11-25 Composite parts in-situ ultrasonic detection probe extending and positioning device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611056903.7A CN106706764A (en) 2016-11-25 2016-11-25 Composite parts in-situ ultrasonic detection probe extending and positioning device

Publications (1)

Publication Number Publication Date
CN106706764A true CN106706764A (en) 2017-05-24

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CN201611056903.7A Pending CN106706764A (en) 2016-11-25 2016-11-25 Composite parts in-situ ultrasonic detection probe extending and positioning device

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108088911A (en) * 2017-11-15 2018-05-29 中国航发沈阳黎明航空发动机有限责任公司 A kind of diskware dovetail groove original position ultrasonic inspection probe

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0357441A (en) * 1989-07-27 1991-03-12 Olympus Optical Co Ltd Ultrasonic endoscope
US6076407A (en) * 1998-05-15 2000-06-20 Framatome Technologies, Inc. Pipe inspection probe
CN102278938A (en) * 2010-04-23 2011-12-14 赫尔穆特费希尔有限责任公司电子及测量技术研究所 Measuring probe for non-destructive measuring of the thickness of thin layers
CN203290906U (en) * 2013-04-24 2013-11-20 徐州市凯信电子设备有限公司 Animal transrectal probe extension handle
CN203564276U (en) * 2013-11-29 2014-04-30 山东省立医院 Automatic mucosa marking biopsy forceps
CN204177773U (en) * 2014-11-21 2015-02-25 沈阳黎明航空发动机(集团)有限责任公司 A kind of delay probe of compound substance original position Ultrasonic Detection

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0357441A (en) * 1989-07-27 1991-03-12 Olympus Optical Co Ltd Ultrasonic endoscope
US6076407A (en) * 1998-05-15 2000-06-20 Framatome Technologies, Inc. Pipe inspection probe
CN102278938A (en) * 2010-04-23 2011-12-14 赫尔穆特费希尔有限责任公司电子及测量技术研究所 Measuring probe for non-destructive measuring of the thickness of thin layers
CN203290906U (en) * 2013-04-24 2013-11-20 徐州市凯信电子设备有限公司 Animal transrectal probe extension handle
CN203564276U (en) * 2013-11-29 2014-04-30 山东省立医院 Automatic mucosa marking biopsy forceps
CN204177773U (en) * 2014-11-21 2015-02-25 沈阳黎明航空发动机(集团)有限责任公司 A kind of delay probe of compound substance original position Ultrasonic Detection

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108088911A (en) * 2017-11-15 2018-05-29 中国航发沈阳黎明航空发动机有限责任公司 A kind of diskware dovetail groove original position ultrasonic inspection probe

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Application publication date: 20170524

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