CN111070156A - Dismounting device of aircraft high frequency power plug - Google Patents

Dismounting device of aircraft high frequency power plug Download PDF

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Publication number
CN111070156A
CN111070156A CN201911385455.9A CN201911385455A CN111070156A CN 111070156 A CN111070156 A CN 111070156A CN 201911385455 A CN201911385455 A CN 201911385455A CN 111070156 A CN111070156 A CN 111070156A
Authority
CN
China
Prior art keywords
cheek
frequency power
power plug
dismounting device
pincer
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
CN201911385455.9A
Other languages
Chinese (zh)
Inventor
张晟昊
佟逸辉
张明兴
董学峰
韩学剑
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.)
Dalian Changfeng Industrial Corp
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Dalian Changfeng Industrial Corp
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 Dalian Changfeng Industrial Corp filed Critical Dalian Changfeng Industrial Corp
Priority to CN201911385455.9A priority Critical patent/CN111070156A/en
Publication of CN111070156A publication Critical patent/CN111070156A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B27/00Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for
    • B25B27/02Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for for connecting objects by press fit or detaching same
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B5/00Clamps
    • B25B5/16Details, e.g. jaws, jaw attachments
    • B25B5/163Jaws or jaw attachments

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Abstract

The invention discloses a dismounting device for a high-frequency power plug of an airplane, which can be used for dismounting the high-frequency power plug positioned at a gap between a fire control radar and a certain airplane body, so that the high-frequency power plug and the periphery are not scratched, and belongs to the technical field of aviation equipment. The method comprises the following steps: the pliers cheek A, the pliers cheek B, the sawtooth head and the connecting pin; during the use, the operation end of two pincers cheek is held to the hand, with the work end of these two pincers cheek probe into required dismantlement plug place gap, with the sawtooth head to just required dismantlement plug, the operation end of two pincers cheek of centre gripping makes the work end of two pincers cheek press from both sides the tight high frequency power plug that needs of dismantling, guarantees that the sawtooth friction of sawtooth head is effective, and rotatory this dismounting device makes the high frequency plug screw out, reaches the dismantlement purpose.

Description

Dismounting device of aircraft high frequency power plug
Technical Field
The invention relates to a dismounting device, in particular to a dismounting device for a high-frequency power plug of an airplane, and belongs to the technical field of aviation equipment.
Background
When a certain airplane is overhauled, the high-frequency power plug needs to be detached due to troubleshooting, but the position of the high-frequency power plug is located in an installation gap between the fire control radar and the airplane body, the detaching space is narrow, and hands cannot touch the position of the high-frequency power plug. If the high-frequency power plug cannot be disassembled during troubleshooting of the airplane, the fire control radar is disassembled firstly and then troubleshooting is carried out, so that the consumption of manpower and material resources is large.
Disclosure of Invention
In view of this, the invention provides a dismounting device for a high-frequency power plug of an airplane, which ensures time and labor saving during dismounting of a high-frequency power supply, and eliminates the need of dismounting a fire control radar first and then troubleshooting, thereby saving tedious and repetitive work.
The dismounting device of the airplane high-frequency power plug comprises: the pliers cheek A, the pliers cheek B, the sawtooth head and the connecting pin; the middle parts of the pincer cheek A and the pincer cheek B are crossed and then connected through a connecting pin to serve as a main body of the dismounting device; the part, positioned at one end of the connecting pin, of the pincer cheek A and the pincer cheek B is an operating end, the other end of the connecting pin is a working end, and the pincer cheek A and the pincer cheek B can rotate around the axis of the connecting pin to realize the opening or closing of the working end;
the opposite surfaces of the working end parts of the jaw A and the jaw B are respectively provided with a sawtooth head, and the opposite surfaces of the two sawtooth heads are in sawtooth shapes.
Preferably, the sawteeth on the sawteeth head are matched with the cross-grain knurls of the high-frequency power plug required to be disassembled.
Preferably, the sawtooth head is detachably mounted on the corresponding cheek by a fastener.
Preferably, the sawtooth head is mounted on the corresponding cheek by a screw.
Preferably, the operating ends of the pincer cheek A and the pincer cheek B are handles.
Preferably, the cheek A and the cheek B are made of No. 45 steel hardened and tempered materials.
Preferably, the tooth head is made of T8A material.
Advantageous effects
(1) The dismounting device can be used for conveniently dismounting the high-frequency power plug positioned at the gap between the fire control radar and the airplane body, so that the problem of difficulty in dismounting due to the fact that the high-frequency power plug is dismounted due to narrow space and cannot be touched by hands after the fire control radar is mounted is solved; and the high-frequency power plug and the periphery are prevented from being scratched in the dismounting process.
(2) The saw tooth head is arranged to ensure that the dismounting device can clamp the power plug tightly, and the saw tooth head is connected through the screw, so that friction force can be increased, and meanwhile, the saw tooth head can be conveniently damaged and replaced.
(3) The dismounting device main body is made of No. 45 steel quenched and tempered material, the strength and the hardness are good, the mechanical performance is good, the sawtooth head is made of T8A material, the hardness is guaranteed, meanwhile, the wear resistance is improved, and the service life of the high-frequency power plug dismounting device is guaranteed.
Drawings
Fig. 1 is a schematic view of the overall structure of the dismounting device.
Wherein: 1-cheek A, 2-cheek B, 3-sawtooth head, 4-connecting pin and 5-screw
Detailed Description
The invention is described in detail below by way of example with reference to the accompanying drawings.
The embodiment provides a dismounting device for a high-frequency power plug of an airplane, and the high-frequency power plug positioned at a gap between a fire control radar and an airplane body can be dismounted by utilizing the tool, so that the use requirement of the airplane during overhaul is met; and the high-frequency power plug and the periphery are not scratched.
As shown in fig. 1, the detaching device includes: a cheek A1, a cheek B2, a sawtooth head 3 and a connecting pin 4; the pincer cheek A1 and the pincer cheek B2 are made of No. 45 steel hardening and tempering materials, the middle parts of the pincer cheek A1 and the pincer cheek B2 are assembled in an interference fit mode through a connecting pin 4 after crossing, and a scissors type structure is formed and serves as a main body of the dismounting device; one end of the pincer cheek A1 and the pincer cheek B2, which are positioned on the connecting pin 4, is an operating end, and the other end of the connecting pin is a working end, wherein the operating ends of the pincer cheek A1 and the pincer cheek B2 are handles, so that the pincer cheek A1 and the pincer cheek B2 are convenient to hold; the jaw a1 and the jaw B2 are able to rotate about the axis of the connecting pin 4, so that their working ends can be opened or closed when the control operating end is closed or opened.
The length of the working ends of the jaw A1 and the jaw B2 is set according to actual use requirements, and the problem that disassembly and assembly are difficult due to the fact that a fire control radar is installed and a high-frequency power plug is detached in a narrow space and cannot be touched by hands is solved through the working ends of the jaw A1 and the jaw B2.
Saw tooth heads 3 are arranged on the opposite surfaces of the end parts of the working ends of the jaw A1 and the jaw B2, and the saw tooth heads 3 are made of T8A materials; the opposite surfaces of the two sawtooth heads 3 are in a sawtooth shape and are matched with the cross-grain knurls of the high-frequency power plug to be disassembled, so that the high-frequency power plug can be reliably clamped; the sawtooth head 3 is fastened on the corresponding cheek through the cross-slot pan head screw 5, so that the friction force can be increased, and the sawtooth head 3 can be conveniently damaged and replaced.
When the working ends of the jaw A1 and the jaw B2 are closed, the high-frequency power plug can be clamped by the sawtooth head 3 and can be disassembled as required.
When the dismounting device is used, the operating ends of the two pincer cheeks are held by hands, the working ends of the two pincer cheeks are inserted into a gap where a plug needing to be dismounted is located, the sawtooth head 3 is aligned to the plug needing to be dismounted, the operating ends of the two pincer cheeks are clamped, the working ends of the two pincer cheeks are clamped tightly to the high-frequency power supply plug needing to be dismounted, the sawtooth friction of the sawtooth head 3 is guaranteed to be effective, and the dismounting device is rotated to enable the high-frequency plug to be screwed out, so that the dismounting purpose is achieved.
In summary, the above description is only a preferred example of the present invention, and is not intended to limit the scope of the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (7)

1. A device for removing a high-frequency power plug from an aircraft, comprising: the clamp cheek-type combined pliers comprise a clamp cheek A (1), a clamp cheek B (2), a sawtooth head (3) and a connecting pin (4); the middle parts of the pincer cheek A (1) and the pincer cheek B (2) are crossed and then connected through a connecting pin (4) to serve as a main body of the dismounting device; the part, located at one end of the connecting pin (4), of the pincer cheek A (1) and the pincer cheek B (2) is an operating end, the other end of the connecting pin is a working end, and the pincer cheek A (1) and the pincer cheek B (2) can rotate around the axis of the connecting pin (4) to realize the opening or closing of the working end;
the opposite surfaces of the working end parts of the cheek A (1) and the cheek B (2) are respectively provided with a sawtooth head (3), and the opposite surfaces of the sawtooth heads (3) are sawtooth-shaped.
2. The aircraft high-frequency power plug dismounting device as claimed in claim 1, wherein the saw teeth on the saw-tooth head (3) are matched with the cross-grain knurling of the high-frequency power plug to be dismounted.
3. The dismounting device for high-frequency power plugs of airplanes as claimed in claim 1, wherein the sawtooth head (3) is detachably mounted on the corresponding jaw by fasteners.
4. A dismounting device for high-frequency power plugs of airplanes as claimed in claim 3, wherein said serrated head (3) is mounted on the corresponding jaw by means of screws (5).
5. The dismounting device for the high-frequency power plug of the airplane as claimed in claim 1, wherein the operating ends of the pincer cheek A (1) and the pincer cheek B (2) are handles.
6. The dismounting device of the aircraft high-frequency power plug as claimed in claim 1, wherein the cheek A (1) and the cheek B (2) are made of a hardened and tempered material of No. 45 steel.
7. The aircraft high-frequency power plug removal device of claim (1), wherein the tine (3) is made of T8A material.
CN201911385455.9A 2019-12-29 2019-12-29 Dismounting device of aircraft high frequency power plug Pending CN111070156A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911385455.9A CN111070156A (en) 2019-12-29 2019-12-29 Dismounting device of aircraft high frequency power plug

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911385455.9A CN111070156A (en) 2019-12-29 2019-12-29 Dismounting device of aircraft high frequency power plug

Publications (1)

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CN111070156A true CN111070156A (en) 2020-04-28

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CN201911385455.9A Pending CN111070156A (en) 2019-12-29 2019-12-29 Dismounting device of aircraft high frequency power plug

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112157620A (en) * 2020-08-17 2021-01-01 韶关高尔德防雷科技有限公司 Utilize lever principle to dismantle tool of module
CN114374131A (en) * 2022-01-14 2022-04-19 上海御渡半导体科技有限公司 Auxiliary disassembling tool for plug-in radio frequency connector

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104117948A (en) * 2014-07-16 2014-10-29 江苏永钢集团有限公司 Device for detaching roller ring locking nut
CN104759996A (en) * 2015-04-24 2015-07-08 张甲进 Pliers special for trimming steel wire butt welding spot
CN204597208U (en) * 2015-05-22 2015-08-26 国网冀北电力有限公司廊坊供电公司 Netting twine head plug pincers
WO2017049774A1 (en) * 2015-09-25 2017-03-30 张家港玉成精机股份有限公司 Machining device for machining plier jaw on plier workpiece
CN212044469U (en) * 2019-12-29 2020-12-01 大连长丰实业总公司 Dismounting device of aircraft high frequency power plug

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104117948A (en) * 2014-07-16 2014-10-29 江苏永钢集团有限公司 Device for detaching roller ring locking nut
CN104759996A (en) * 2015-04-24 2015-07-08 张甲进 Pliers special for trimming steel wire butt welding spot
CN204597208U (en) * 2015-05-22 2015-08-26 国网冀北电力有限公司廊坊供电公司 Netting twine head plug pincers
WO2017049774A1 (en) * 2015-09-25 2017-03-30 张家港玉成精机股份有限公司 Machining device for machining plier jaw on plier workpiece
CN212044469U (en) * 2019-12-29 2020-12-01 大连长丰实业总公司 Dismounting device of aircraft high frequency power plug

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112157620A (en) * 2020-08-17 2021-01-01 韶关高尔德防雷科技有限公司 Utilize lever principle to dismantle tool of module
CN112157620B (en) * 2020-08-17 2024-01-23 广东高尔德集团有限公司 Jig for disassembling module by utilizing lever principle
CN114374131A (en) * 2022-01-14 2022-04-19 上海御渡半导体科技有限公司 Auxiliary disassembling tool for plug-in radio frequency connector

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