CN106763060A - Rudder dismounting school dress pin - Google Patents

Rudder dismounting school dress pin Download PDF

Info

Publication number
CN106763060A
CN106763060A CN201611162457.8A CN201611162457A CN106763060A CN 106763060 A CN106763060 A CN 106763060A CN 201611162457 A CN201611162457 A CN 201611162457A CN 106763060 A CN106763060 A CN 106763060A
Authority
CN
China
Prior art keywords
main body
adjusting rod
rudder
dismounting
school dress
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
CN201611162457.8A
Other languages
Chinese (zh)
Inventor
何丹
申炳龙
陈怀宇
王卫忠
荣斌
刘珏伶
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.)
Nantong Huaxia Airplane Engineering Technology Co Ltd
Original Assignee
Nantong Huaxia Airplane Engineering Technology 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 Nantong Huaxia Airplane Engineering Technology Co Ltd filed Critical Nantong Huaxia Airplane Engineering Technology Co Ltd
Priority to CN201611162457.8A priority Critical patent/CN106763060A/en
Publication of CN106763060A publication Critical patent/CN106763060A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/02Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings

Abstract

The present invention relates to a kind of rudder dismounting school dress pin, including main body, one end of the main body is provided with drilling, the other end is provided with adjusting rod after forming bending section, one end of the adjusting rod is provided with external screw thread, the external screw thread is engaged with the internal thread in main body, and the section of the other end of the adjusting rod forms step-like;Warning tape is coated with the periphery of the main body;The integrally L-shaped setting of described main body.It is an advantage of the invention that:It is simple to operate, it is easy to use, improve school dress efficiency.

Description

Rudder dismounting school dress pin
Technical field
The present invention relates to a kind of rudder dismounting school dress pin.
Background technology
Existing school dress is sold and is the drawbacks of existing during being filled to rudder school:Be inconvenient to operate, complex structure, drop Low efficiency.
The content of the invention
To overcome the defect of prior art, the present invention to provide a kind of rudder dismounting school dress pin, technical scheme It is:
Rudder dismounting school dress pin, including main body, one end of the main body are provided with drilling, and the other end is provided with after forming bending section Adjusting rod, one end of the adjusting rod is provided with external screw thread, and the external screw thread is engaged with the internal thread in main body, the adjusting rod The section of the other end forms step-like;Warning tape is coated with the periphery of the main body.
The integrally L-shaped setting of described main body.
It is an advantage of the invention that:It is simple to operate, it is easy to use, improve school dress efficiency.
Brief description of the drawings
Fig. 1 is agent structure schematic diagram of the invention.
Specific embodiment
Further describe the present invention with reference to specific embodiment, advantages of the present invention and feature will be with description and It is apparent.But these embodiments are only exemplary, do not constitute any limitation to the scope of the present invention.People in the art Member to the details of technical solution of the present invention and form it should be understood that can enter without departing from the spirit and scope of the invention Row modification is replaced, but these modifications and replacement are each fallen within protection scope of the present invention.
Referring to Fig. 1, the present invention relates to a kind of rudder dismounting school dress pin, including main body 1, one end of the main body 1 is provided with Drilling 2, the other end formed bending section after adjusting rod 3 is installed, one end of the adjusting rod 3 is provided with external screw thread, the external screw thread with Internal thread in main body 1 is engaged, the mode being connected through a screw thread, and realizes the regulation of adjusting rod and the distance between main body;Institute The section 4 for stating the other end of adjusting rod 3 forms step-like;Warning tape is coated with the periphery of the main body 1(It is not shown).Such as Fig. 1 Shown, described main body integrally L-shaped setting.
Operation principle of the invention is:By in the school dress hole of the step-like section insertion pedal of adjusting rod, bottom passes through Bolt through drilling after be fixed on the base plate in cabin, by adjusting the regulation of adjusting rod and main body distance, realize pedal and Regulation between base plate.

Claims (2)

1. rudder dismounting school dress is sold, it is characterised in that including main body, one end of the main body is provided with drilling, and the other end is formed Adjusting rod is installed, one end of the adjusting rod is provided with external screw thread after bending section, the external screw thread matches with the internal thread in main body Close, the section of the other end of the adjusting rod forms step-like;Warning tape is coated with the periphery of the main body.
2. rudder dismounting school dress according to claim 1 is sold, it is characterised in that the integrally L-shaped setting of described main body.
CN201611162457.8A 2016-12-15 2016-12-15 Rudder dismounting school dress pin Pending CN106763060A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611162457.8A CN106763060A (en) 2016-12-15 2016-12-15 Rudder dismounting school dress pin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611162457.8A CN106763060A (en) 2016-12-15 2016-12-15 Rudder dismounting school dress pin

Publications (1)

Publication Number Publication Date
CN106763060A true CN106763060A (en) 2017-05-31

Family

ID=58892638

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611162457.8A Pending CN106763060A (en) 2016-12-15 2016-12-15 Rudder dismounting school dress pin

Country Status (1)

Country Link
CN (1) CN106763060A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110228327A (en) * 2019-05-27 2019-09-13 南通华夏飞机工程技术股份有限公司 A kind of aero tyre installation equipment
CN110228327B (en) * 2019-05-27 2024-04-26 南通华夏飞机工程技术股份有限公司 Aircraft tire erection equipment

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2254867Y (en) * 1996-04-29 1997-05-28 王兆禄 Bicycle with length-adjustable crank during riding it
EP0801257A1 (en) * 1996-04-09 1997-10-15 Erico International Corporation Universal beam hanger
CN101893133A (en) * 2010-08-19 2010-11-24 中国航空工业第六一八研究所 Connection structure of valve element of direct drive servo valve and connecting rod
CN202646263U (en) * 2012-06-28 2013-01-02 中联重科股份有限公司 Telescopic boom and engineering machine containing same
CN203122308U (en) * 2012-12-26 2013-08-14 王圣尧 Telescopic broom
CN204093998U (en) * 2014-10-11 2015-01-14 合肥江航飞机装备有限公司 A kind of drift shedding mechanism
CN205579061U (en) * 2016-04-10 2016-09-14 李元军 User puts down and operates support that need not to look at straight screen when lying
CN106069577A (en) * 2016-08-29 2016-11-09 来安县刘莲蓬家庭农场 It is applicable to tree branch and puts the support means of pendant

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0801257A1 (en) * 1996-04-09 1997-10-15 Erico International Corporation Universal beam hanger
CN2254867Y (en) * 1996-04-29 1997-05-28 王兆禄 Bicycle with length-adjustable crank during riding it
CN101893133A (en) * 2010-08-19 2010-11-24 中国航空工业第六一八研究所 Connection structure of valve element of direct drive servo valve and connecting rod
CN202646263U (en) * 2012-06-28 2013-01-02 中联重科股份有限公司 Telescopic boom and engineering machine containing same
CN203122308U (en) * 2012-12-26 2013-08-14 王圣尧 Telescopic broom
CN204093998U (en) * 2014-10-11 2015-01-14 合肥江航飞机装备有限公司 A kind of drift shedding mechanism
CN205579061U (en) * 2016-04-10 2016-09-14 李元军 User puts down and operates support that need not to look at straight screen when lying
CN106069577A (en) * 2016-08-29 2016-11-09 来安县刘莲蓬家庭农场 It is applicable to tree branch and puts the support means of pendant

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110228327A (en) * 2019-05-27 2019-09-13 南通华夏飞机工程技术股份有限公司 A kind of aero tyre installation equipment
CN110228327B (en) * 2019-05-27 2024-04-26 南通华夏飞机工程技术股份有限公司 Aircraft tire erection equipment

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Legal Events

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PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20170531