CN201810617U - Quick-connecting locking plate - Google Patents

Quick-connecting locking plate Download PDF

Info

Publication number
CN201810617U
CN201810617U CN2010201614169U CN201020161416U CN201810617U CN 201810617 U CN201810617 U CN 201810617U CN 2010201614169 U CN2010201614169 U CN 2010201614169U CN 201020161416 U CN201020161416 U CN 201020161416U CN 201810617 U CN201810617 U CN 201810617U
Authority
CN
China
Prior art keywords
locking plate
quick
locked groove
utility
quick connection
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.)
Expired - Fee Related
Application number
CN2010201614169U
Other languages
Chinese (zh)
Inventor
王晓静
王光富
王燕芳
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.)
Guizhou Aerospace Precision Products Co Ltd
Original Assignee
Guizhou Aerospace Precision Products 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 Guizhou Aerospace Precision Products Co Ltd filed Critical Guizhou Aerospace Precision Products Co Ltd
Priority to CN2010201614169U priority Critical patent/CN201810617U/en
Application granted granted Critical
Publication of CN201810617U publication Critical patent/CN201810617U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Abstract

The utility model discloses a quick-connecting locking plate, comprising a locking plate (1). The locking plate (1) is provided with a slot hole (2) and a locked groove (3) crossed with the slot hole (2). Compared with the prior art, the quick-connecting locking plate not only can adapt to the using requirements of different types of quick-release locks, meets the requirement of rapid disassembly when an airplane is in maintenance, and also ensures the reliability when the air plane is in the bad work environment. The locking plate can be widely applied to the connection of plates of a helicopter, and also play the role which can not be completed by the common fasteners. The locking plate not only can be applied on airplanes, but also can be applied to industries such as automobiles and the like, and can be promoted to wider fields.

Description

A kind of quick connection locking plate
Technical field
The utility model relates to a kind of connection locking plate, particularly relates to a kind of quick connection locking plate.
Background technique
In many sheet materials of aircraft connect,, often adopt quick ways of connecting for the ease of aircraft is safeguarded.Also require simultaneously these structures that connect fast can satisfy the aircraft bad working environment.Some present fast joint structures can not satisfy the usage requirement of dissimilar quick-release locks, and reliability is lower in bad working environment.
The model utility content
The purpose of this utility model is, a kind of quick connection locking plate is provided.It not only can adapt to the usage requirement of dissimilar quick-release locks, and the requirement of fast quick-detach when satisfying aircraft maintenance can also be guaranteed the reliability of aircraft in abominable working environment.
The technical solution of the utility model: a kind of quick connection locking plate, comprise locking plate, locking plate is provided with slotted hole and a locked groove that intersects with slotted hole.
In the above-mentioned quick connection locking plate, the angle of described slotted hole and locked groove is 45~90 °.
In the aforementioned quick connection locking plate, the degree of depth of described locked groove is greater than the radius of locked groove diameter.
In the aforementioned quick connection locking plate, described locking plate is provided with fixed hole.
In the aforementioned quick connection locking plate, described locking plate is made with the 1Cr11Ni2W2MoV stainless steel material.
Compared with prior art, it not only can adapt to the usage requirement of dissimilar quick-release locks the utility model, and the requirement of fast quick-detach when satisfying aircraft maintenance can also be guaranteed the reliability of aircraft in abominable working environment.The connection of helicopter sheet material can be widely used in, the effect that general fastening piece can't play can be played.The utility model not only can be applicable on the aircraft, also can be applicable to be generalized to field widely as automobile and other industries.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is application example figure of the present utility model;
Fig. 3 is an application process schematic representation of the present utility model.
Being labeled as in the accompanying drawing: 1-locking plate, 2-slotted hole, 3-locked groove, 4-fixed hole, 5-A plate, 6-B plate, 7-spring, 8-lock nut, 9-lock pin, 10-rivet.
Embodiment
The utility model is described in further detail below in conjunction with drawings and Examples.
Embodiment.Fig. 1 is a schematic representation of the present utility model, and a kind of quick connection locking plate comprises that locking plate 1 is provided with slotted hole 2 and a locked groove 3 that intersects with slotted hole 2 with the locking plate 1 of 1Cr11Ni2W2MoV stainless steel material extrusion moulding.Slotted hole 2 is 45~90 ° with the angle of locked groove 3, and the angle in this example is 70 degree.The degree of depth of locked groove 3 is greater than lock pin 9 radiuses that cooperate with locked groove.Described locking plate 1 is provided with fixed hole 4.
Fig. 2 is an application example schematic representation of the present utility model, and as shown in Figure 2, this example is the example that A plate 5 and B plate 6 is linked together by locking plate 1.B plate 6 is provided with lockhole, is provided with spring 7 and lock nut 8 in the lockhole, and lock nut 8 belows are provided with T-shaped lock pin 9, is through in the fixed hole 4 locking plate 1 riveting on A plate 5 with rivet 10, and during riveted joint, the opening of locked groove 3 down.During connection, lock nut on the B plate 68 is pressed, as shown in Figure 3, the direction of the slotted hole 2 of horizontal columns on locking plate 1 of lock nut 8 belows T-shaped lock pin 9 is passed, rotate lock nut 8 then and loosen lock nut 8, lock nut 8 is upspring lock nut 8 under the effect of spring 7, and the horizontal columns of lock pin 9 is stuck in the opening of locked groove 3 as shown in Figure 2, makes A plate 5 be connected and can not separate with B plate 6.

Claims (5)

1. one kind connects locking plate fast, and it is characterized in that: comprise locking plate (1), locking plate (1) is provided with slotted hole (2) and a locked groove (3) that intersects with slotted hole (2).
2. according to the described quick connection locking plate of claim 1, it is characterized in that: described slotted hole (2) is 45~90 ° with the angle of locked groove (3).
3. according to the described quick connection locking plate of claim 2, it is characterized in that: the degree of depth of described locked groove (3) is greater than the radius of locked groove (3) diameter.
4. according to the described quick connection locking plate of claim 1, it is characterized in that: described locking plate (1) is provided with fixed hole (4).
5. according to the described quick connection locking plate of the arbitrary claim of claim 1~4, it is characterized in that: described locking plate (1) is made with the 1Cr11Ni2W2MoV stainless steel material.
CN2010201614169U 2010-04-16 2010-04-16 Quick-connecting locking plate Expired - Fee Related CN201810617U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010201614169U CN201810617U (en) 2010-04-16 2010-04-16 Quick-connecting locking plate

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010201614169U CN201810617U (en) 2010-04-16 2010-04-16 Quick-connecting locking plate

Publications (1)

Publication Number Publication Date
CN201810617U true CN201810617U (en) 2011-04-27

Family

ID=43893559

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010201614169U Expired - Fee Related CN201810617U (en) 2010-04-16 2010-04-16 Quick-connecting locking plate

Country Status (1)

Country Link
CN (1) CN201810617U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103967898A (en) * 2014-04-21 2014-08-06 李明科 Self-locking connector for board furniture

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103967898A (en) * 2014-04-21 2014-08-06 李明科 Self-locking connector for board furniture

Similar Documents

Publication Publication Date Title
US20150016918A1 (en) Elastically averaged alignment systems and methods
CN202251309U (en) Force-bearing quick release lock
US9873186B2 (en) Connecting element
CN202118044U (en) Flat round head lock pin type quick-dismount lock
EP2564078A1 (en) Component connection and method for connecting components
CA2797195A1 (en) Composite beam chord between reinforcement plates and related method of manufacturing
EP2353997A2 (en) Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box
US20140286727A1 (en) One-piece self-locking nut
CN104417749A (en) An aircraft structure and method of manufacture
CN201810617U (en) Quick-connecting locking plate
CA2914874A1 (en) Tool and method of installing a bulkhead within a structure
US20170335876A1 (en) Fastener with retaining portion
CN104554703A (en) Joint assembly and method of assembling same
CN102168703B (en) Connecting device
CN104724277A (en) Light airplane composite material skin integral rapid connecting structure and manufacturing method thereof
CN104454871A (en) Rivet
CN103994132A (en) Buckling module and butt joint module
CN204213134U (en) Without riveting gun rivet
CN104260874B (en) The stringer card of equipment is fixed on a kind of Airbus Aircraft stringer
CN108177758B (en) Skin structure and skin mounting and dismounting method
CN102854068B (en) Container lock shearing strength detection tooling method
CN107009073B (en) A kind of column fast-positioning device and method
CN208399118U (en) Riveting tool is used in detachable detection
CN202708423U (en) Clamp structure capable of being dismantled quickly
CN110861764A (en) A folding mechanism for unmanned aerial vehicle horn

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110427

Termination date: 20160416

CF01 Termination of patent right due to non-payment of annual fee