CN206001980U - A kind of anti-regulator streamed - Google Patents

A kind of anti-regulator streamed Download PDF

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Publication number
CN206001980U
CN206001980U CN201620924452.3U CN201620924452U CN206001980U CN 206001980 U CN206001980 U CN 206001980U CN 201620924452 U CN201620924452 U CN 201620924452U CN 206001980 U CN206001980 U CN 206001980U
Authority
CN
China
Prior art keywords
empennage
frame
baffle plate
journal stirrup
wing axle
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
CN201620924452.3U
Other languages
Chinese (zh)
Inventor
李文兵
郝卫红
张立博
柴华伟
赵朋
张艳军
薛新勇
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.)
Jinxi Industries Group Co Ltd
Original Assignee
Jinxi Industries 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 Jinxi Industries Group Co Ltd filed Critical Jinxi Industries Group Co Ltd
Priority to CN201620924452.3U priority Critical patent/CN206001980U/en
Application granted granted Critical
Publication of CN206001980U publication Critical patent/CN206001980U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

This utility model is related to a kind of anti-regulator streamed, and belongs to civil rocket bullet field.Regulator of the present utility model, including empennage, wing axle, spring, empennage frame, baffle plate, circlip;Wing axle, also cross an earhole of empennage and empennage frame, installs spring with empennage frame at the journal stirrup that empennage is connected, and wing axle passes through to be socketed circlip respectively in the cannelure of two ends, makes caudal wing shaft relative to empennage frame axially position;The two ends of baffle plate are fixed by screws in the positioning plane of empennage frame two ends journal stirrup, make baffle plate shelter from the wing axle insertion band between spring junction and empennage frame journal stirrup.Regulator of the present utility model achieves anti-flow perturbation design by baffle plate, by using circlip axially position at wing axle two ends, convenient processing, and flexible combination, shorten the process-cycle, improve packaging efficiency.

Description

A kind of anti-regulator streamed
Technical field
This utility model is related to a kind of anti-regulator streamed, and belongs to civil rocket bullet field.
Background technology
Regulator is to ensure that the vitals that body reliably flies, and particularly with foldable empennage, sends out to adapt to cartridge type The needs penetrated, part placement is quite compact.Traditional structure regulator is symmetrical structure, as shown in figure 1, between empennage and empennage frame There is chain connection at 2~3, wing axle is elongate rod, and two ends are all formed with screw thread.Wing axle sequentially passes through empennage stand hole, empennage journal stirrup Kong Hou, two groups of hex nuts, plain cushion, spring washers from both direction, wing axle are fixed on empennage frame respectively.The problem existing It is:Wing axle is high-fineness ratio rod member, manufactures screw thread and causes the process-cycle long, and axiality is difficult to ensure;On wing axle, spring connects There is long and narrow, the banding communicating structure of large area between place and empennage frame journal stirrup, easily form interference in air flow source, impact is stable The work efficiency of device.In particular for guided rocket, when empennage goes to certain angle, the gap between empennage and bomb body adds Greatly, loss of lift will be made to increase, control efficiency reduces further.
Utility model content
The purpose of this utility model is in order to the air turbulence solving to bring traditional structure regulator, aerodynamic configuration do not flow Freely, for the problem that control efficiency after guided munition is low, reduce assembling difficulty simultaneously.
The purpose of this utility model is achieved through the following technical solutions:
A kind of anti-regulator streamed of the present utility model, including empennage, wing axle, spring, empennage frame, baffle plate, elasticity gear Circle;
The dorsal part plate face of empennage frame two ends journal stirrup is machined with positioning plane;
Wing axle is logical direct light axle, and two side walls are machined with cannelure;
Baffle plate be length and empennage frame two ends journal stirrup positioning plane spacing match, width and empennage frame journal stirrup height phase The rectangular thin plate of coupling;
Wing axle, also cross an earhole of empennage and empennage frame, installs spring at the journal stirrup that empennage is connected with empennage frame, Wing axle passes through to be socketed circlip respectively in the cannelure of two ends, makes caudal wing shaft relative to empennage frame axially position;The two ends of baffle plate It is fixed by screws in the positioning plane of empennage frame two ends journal stirrup, make baffle plate shelter from spring junction and empennage on wing axle Insertion band between frame journal stirrup.
Beneficial effect
Regulator of the present utility model achieves anti-flow perturbation design by baffle plate, by using elasticity at wing axle two ends Back-up ring axially position, convenient processing, flexible combination, shorten the process-cycle, improve packaging efficiency.
Brief description
Fig. 1 is the structural representation of conventional stabilizer;
Fig. 2 is the structural representation of this utility model regulator;
Fig. 3 is this utility model regulator empennage junction profile;
Fig. 4 is this utility model regulator wing axial end connection diagram;
In figure, 1- screw;2- baffle plate;3- empennage;4- wing axle;5- spring;6- empennage frame;7- circlip.
Specific embodiment
With reference to the accompanying drawings and examples content of the present utility model is further described.
Embodiment
A kind of anti-regulator streamed of the present utility model, as shown in Fig. 2 include empennage 3, wing axle 4, spring 5, empennage frame 6th, baffle plate 2, circlip 7;
The dorsal part plate face of empennage frame 6 two ends journal stirrup is machined with positioning plane;
Wing axle 4 is logical direct light axle, and two side walls are machined with cannelure;
The spacing that baffle plate 2 positions plane for length with empennage frame 6 two ends journal stirrup matches, width and empennage frame 6 journal stirrup are high Spend the rectangular thin plate matching;
Wing axle 4, also cross an earhole of empennage 3 and empennage frame 6, is installed at the journal stirrup that empennage 3 is connected with empennage frame 6 Spring 4, wing axle 4 passes through to be socketed circlip 7 respectively in the cannelure of two ends, makes caudal wing shaft relative to empennage frame axially position, such as Shown in Fig. 4;The two ends of baffle plate 2 are fixed in the positioning plane of empennage frame 6 two ends journal stirrup by screw 1, so that baffle plate 2 is sheltered from Insertion band between spring junction and empennage frame journal stirrup on wing axle, as shown in Figure 3.

Claims (1)

1. a kind of anti-regulator streamed, is characterized in that:Including empennage, wing axle, spring, empennage frame, baffle plate, circlip;
The dorsal part plate face of empennage frame two ends journal stirrup is machined with positioning plane;
Wing axle is logical direct light axle, and two side walls are machined with cannelure;
Baffle plate is that the spacing that length positions plane with empennage frame two ends journal stirrup matches, width and empennage frame journal stirrup highly match Rectangular thin plate;
Wing axle, also cross an earhole of empennage and empennage frame, installs spring, wing axle with empennage frame at the journal stirrup that empennage is connected By being socketed circlip respectively in the cannelure of two ends, make caudal wing shaft relative to empennage frame axially position;The two ends of baffle plate are passed through Screw is fixed in the positioning plane of empennage frame two ends journal stirrup, makes baffle plate shelter from spring junction and empennage frame on wing axle and props up Insertion band between ear.
CN201620924452.3U 2016-08-23 2016-08-23 A kind of anti-regulator streamed Expired - Fee Related CN206001980U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620924452.3U CN206001980U (en) 2016-08-23 2016-08-23 A kind of anti-regulator streamed

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620924452.3U CN206001980U (en) 2016-08-23 2016-08-23 A kind of anti-regulator streamed

Publications (1)

Publication Number Publication Date
CN206001980U true CN206001980U (en) 2017-03-08

Family

ID=58196748

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620924452.3U Expired - Fee Related CN206001980U (en) 2016-08-23 2016-08-23 A kind of anti-regulator streamed

Country Status (1)

Country Link
CN (1) CN206001980U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111189363A (en) * 2020-01-19 2020-05-22 中北大学 Straight wing flight stabilizer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111189363A (en) * 2020-01-19 2020-05-22 中北大学 Straight wing flight stabilizer

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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: 20170308