CN203148647U - Balance sleeve - Google Patents

Balance sleeve Download PDF

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Publication number
CN203148647U
CN203148647U CN2013201032829U CN201320103282U CN203148647U CN 203148647 U CN203148647 U CN 203148647U CN 2013201032829 U CN2013201032829 U CN 2013201032829U CN 201320103282 U CN201320103282 U CN 201320103282U CN 203148647 U CN203148647 U CN 203148647U
Authority
CN
China
Prior art keywords
sleeve
model
locking screw
screw holes
positioning steps
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
CN2013201032829U
Other languages
Chinese (zh)
Inventor
李强
张连河
王艳阳
陈晶源
由亮
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.)
AVIC Aerodynamics Research Institute
Original Assignee
AVIC Aerodynamics Research Institute
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 AVIC Aerodynamics Research Institute filed Critical AVIC Aerodynamics Research Institute
Priority to CN2013201032829U priority Critical patent/CN203148647U/en
Application granted granted Critical
Publication of CN203148647U publication Critical patent/CN203148647U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a balance sleeve. The balance sleeve comprises positioning steps, locking screw holes, a connecting cone and a sleeve, wherein two positioning steps are disposed on an outer wall of the sleeve; a distance between the two positioning steps is consistent with a width of a model rod head; the multiple screw holes are disposed in the left side of the sleeve; the number of the locking screw holes is consistent with the number of through holes in the model rod head; the locking screw holes are locked and connected with the through holes in the model rod head through inner hexagonal screws; and the connecting cone is disposed on the right side of the inside of the sleeve. The balance sleeve is reasonable in design, low in manufacturing cost and convenient to use, is integrally machined and molded by a forging machine, can bear a relatively large load, and has substantially improved structural strength and rigidity and prolonged service life.

Description

The balance sleeve
Technical field
The utility model belongs to model in wind tunnel support system structural design field, is specifically related to a kind of balance sleeve.
Background technology
In the model in wind tunnel support system, all need between model pole and the rod-type balance be connected by the johning knot member, the suffered strong and moment of institute of model when this johning knot member need bear wind tunnel test, comprise aerodynamic drag, lift, side force, pitching moment, rolling moment and yawing, and the coupling of multiple power and moment, force status more complicated and abominable, and this johning knot member often repeats dismounting, requires the repetitive positioning accuracy height.At present, this johning knot member generally adopts comparatively complicated composite set, this kind device repetitive positioning accuracy is poor, and composite set bulk strength and rigidity a little less than, under the design conditions of same load demand, can take bigger dimensional space, this also indirect restriction the size of the gentle model in wind tunnel in rod-type sky.In addition, composite set is then assembled for part split processing, and the processing and manufacturing cost is also higher.
Summary of the invention
For overcoming above-mentioned the deficiencies in the prior art, the purpose of this utility model is to provide a kind of balance sleeve.
The purpose of this utility model is achieved in that a kind of balance sleeve, comprise positioning step, locking screw, connect awl and sleeve, sleeve outer wall is provided with two positioning steps, the width unanimity of the distance model pole head between two positioning steps, the left side of sleeve is provided with a plurality of locking screws, the quantity of locking screw is consistent with the number of vias on the model pole head, and the locking screw is locked with the via hole on the model pole head by socket head cap screw and is connected, and the sleeve inner right side is provided with and connects awl.
The utility model is reasonable in design, and low cost of manufacture is easy to use, by forging the whole machine-shaping of material machine, has improved the structure strength and stiffness greatly; Can bear bigger load; Prolonged serviceable life.
Description of drawings
Fig. 1 is the structural representation before the use of the present utility model;
Fig. 2 is vertical view of the present utility model.
Embodiment
The invention will be further described below in conjunction with last Figure of description:
As shown in Figure 1 and Figure 2, a kind of balance sleeve, comprise positioning step 1, locking screw 2, connect awl 3 and sleeve 4, sleeve outer wall is provided with two positioning steps 1, the width unanimity of the distance model pole head between two positioning steps 1, the left side of sleeve 4 is provided with a plurality of locking screws 2, and the quantity of locking screw 2 is consistent with the number of vias on the model pole head, locking screw 2 is locked with the via hole on the model pole head by socket head cap screw and is connected, and sleeve 4 inner right side are provided with and connect awl 3.
The utility model is reasonable in design, and low cost of manufacture is easy to use, by forging the whole machine-shaping of material machine, has improved the structure strength and stiffness greatly; Can bear bigger load; Prolonged serviceable life.

Claims (1)

1. balance sleeve, comprise positioning step (1), locking screw (2), connect awl (3) and sleeve (4), it is characterized in that: sleeve outer wall is provided with two positioning steps (1), the width unanimity of the distance model pole head between two positioning steps (1), the left side of sleeve (4) is provided with a plurality of locking screws (2), the quantity of locking screw (2) is consistent with the number of vias on the model pole head, locking screw (2) is locked with the via hole on the model pole head by socket head cap screw and is connected, and sleeve (4) inner right side is provided with and connects awl (3).
CN2013201032829U 2013-03-07 2013-03-07 Balance sleeve Expired - Fee Related CN203148647U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013201032829U CN203148647U (en) 2013-03-07 2013-03-07 Balance sleeve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013201032829U CN203148647U (en) 2013-03-07 2013-03-07 Balance sleeve

Publications (1)

Publication Number Publication Date
CN203148647U true CN203148647U (en) 2013-08-21

Family

ID=48976163

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013201032829U Expired - Fee Related CN203148647U (en) 2013-03-07 2013-03-07 Balance sleeve

Country Status (1)

Country Link
CN (1) CN203148647U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103698101A (en) * 2013-12-15 2014-04-02 中国航空工业集团公司哈尔滨空气动力研究所 High-load and high-precision pneumatic force measurement device and measurement method
CN105300595A (en) * 2015-11-27 2016-02-03 中国航空工业集团公司沈阳空气动力研究所 Balance loading head with calibration of connected model and loading method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103698101A (en) * 2013-12-15 2014-04-02 中国航空工业集团公司哈尔滨空气动力研究所 High-load and high-precision pneumatic force measurement device and measurement method
CN103698101B (en) * 2013-12-15 2017-06-06 中国航空工业集团公司哈尔滨空气动力研究所 Big load high accurancy and precision aerodynamics force measurement device and measuring method
CN105300595A (en) * 2015-11-27 2016-02-03 中国航空工业集团公司沈阳空气动力研究所 Balance loading head with calibration of connected model and loading method
CN105300595B (en) * 2015-11-27 2018-06-05 中国航空工业集团公司沈阳空气动力研究所 The balance loading head and loading method of link model calibration

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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: 20130821

Termination date: 20140307