CN204788885U - Tulwar slider becomes angle device based on rack and pinion drive - Google Patents

Tulwar slider becomes angle device based on rack and pinion drive Download PDF

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Publication number
CN204788885U
CN204788885U CN201520548394.4U CN201520548394U CN204788885U CN 204788885 U CN204788885 U CN 204788885U CN 201520548394 U CN201520548394 U CN 201520548394U CN 204788885 U CN204788885 U CN 204788885U
Authority
CN
China
Prior art keywords
tulwar
slide block
slider
axle
device based
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
CN201520548394.4U
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Chinese (zh)
Inventor
牟伟强
卜忱
张国友
刘京藏
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
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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 CN201520548394.4U priority Critical patent/CN204788885U/en
Application granted granted Critical
Publication of CN204788885U publication Critical patent/CN204788885U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

(B, ) tulwar slider becomes angle device based on rack and pinion drive. The rotatory balance experiment of tradition manual operation degree of difficulty when becoming the angle of attack is very big to equipment cost is high. The utility model discloses the constitution includes: slider (b) (b) 7 (b) (b), the slider passes through screw (b) (b) A (b) (b) (b) (b) 1 (b) (b) and is connected with axle (b) (b) 5 (b) (b), the axle adopts the shaft hole cooperation to be connected with director mount pad (b) (b) 2 (b) (b), epaxial axle sleeve (b) (b) 3 (b) (b) and the roller director (b) (b) 4 (b) (b) of being equipped with, the roller director is laminated with the leading edge of tulwar (b) (b) 8 (b) (b), and through gasket (b) (b) 6 (b) (b) adjustment contact distance, gear shaft (b) (b) 11 (b) (b) is connected with the slider through bearing (b) (b) 14 (b) (b), fix the gear shaft on the slider through lock nut (b) (b) 12 (b) (b) and locking gasket (b) (b) 13 (b) (b), be connected with rack (b) (b) 9 (b) (b) through screw (b) (b) B (b) (b) (b) (b) 10 (b) (b) on the tulwar, fitting pin (b) (b) 17 (b) (b) is equipped with on the slider, spring (b) (b) 16 (b) (b) is equipped with on the fitting pin, butterfly nut (b) (b) 15 (b) (b) is equipped with in the fitting pin outside. The utility model is used for rotatory balance experiment. (B, )

Description

Based on the tulwar slide block variable-angle device of gear-rack drive
technical field:
the utility model relates to a kind of tulwar slide block variable-angle device based on gear-rack drive.
background technology:
tailspin is one of the most complicated state of flight of aircraft, be characterized in that the elevation angle is large, the radius of spin is little, turning rate is high, rate of sinking is fast, therefore when tailspin, the dynamic and manipulation of aircraft has a great difference with when usually flying, and as mishandling, may cause serious aircraft accident; In order to understand fully the essence of tailspin phenomenon, prevent aircraft from entering tailspin unexpectedly and guaranteeing to change safely, must further investigate the Tail chain of aircraft, due to tailspin move time, under aircraft is in large attack angle situation, effect flight force and moment is thereon nonlinear, and lengthwise movement is larger with the various sympathesiies of transverse movement, needs nonlinear mathematical model to describe; This brings very large difficulty in theory, and research is in the past subject to the restriction of experimental technique and computing technique, can only simplify mathematical model, is confined to the analysis of linear change; Current acquisition aircraft is vowing that around speed stablizing the comparatively ripe means of aerodynamic characteristic in rotary course is rotation balance test, the fundamental purpose of carrying out rotation balance test in wind-tunnel is exactly that rating model is when the different angle of attack and yaw angle, aerodynamic characteristic under wind axis makes constant speed rotation state with different rates, analysis and prediction for plane's trial spinning characteristic provides necessary Aerodynamic Coefficient, and the experiment of traditional rotary balance when becoming the angle of attack when carrying out manual operation difficulty very large, and equipment cost is high.
utility model content:
the purpose of this utility model is to provide a kind of tulwar slide block variable-angle device based on gear-rack drive.
above-mentioned object is realized by following technical scheme:
a kind of tulwar slide block variable-angle device based on gear-rack drive, its composition comprises: slide block, described slide block is connected with axle by screw A, described axle and guides mount pad adopt shaft hole matching to be connected, axle sleeve and roller guide described axle be equipped with, described roller guide and the leading edge of tulwar are fitted, and by pad adjustment contact distance, gear shaft is connected with described slide block by bearing, by set nut and lock washer, described gear shaft is fixed on described slide block, described tulwar is connected with tooth bar by screw B, described slide block is equipped with locking pin, described locking pin is equipped with spring, outside described locking pin, wing nut is housed.
the described tulwar slide block variable-angle device based on gear-rack drive, described tulwar is provided with groove, and described tooth bar is arranged in described groove; Described tulwar is provided with pin-and-hole, and described locking pin extend in described pin-and-hole under the pressure of described spring.
beneficial effect:
1. the utility model slide block remain silent inner side on, form guidance set by roller guide, axle, guides mount pad, axle sleeve, pad and screw, roller guide and tulwar medial surface are fitted, and play the guiding role in angle process; The symmetrical both sides of slide block opening, form driven unit by gear shaft, bearing, lock washer and set nut, gear shaft be arranged in tulwar groove tooth bar engage, play transmission dynamic action in angle process; Slide block opening side, forms self-locking assembly by wing nut, locking pin, spring, and locking pin is pressed into inside tulwar in pin-and-hole by spring pressure in not angle process, plays locking protective action; Wing nut on slide block is rotated clockwise, locking pin leaves the pin-and-hole on tulwar, by the gear shaft on ratchet wrench turning block mechanism driven unit, the tooth bar engaged transmission on gear shaft and tulwar, simultaneously guidance set auxiliary under realize the change in angle of attack of mechanism.
the utility model is a kind of for carrying out the special testing equipment of model aircraft rotation balance test system tulwar slide block angle in wind-tunnel, this mechanism has that compact conformation, processing charges are low, simple installation, the feature such as easy to use, is suitable for extensively promoting on rotary balance equipment.
accompanying drawing illustrates:
accompanying drawing 1 is structural representation of the present utility model.
accompanying drawing 2 is right views of accompanying drawing 1.
accompanying drawing 3 is vertical views of accompanying drawing 1.
accompanying drawing 4 is shaft side figures such as grade of accompanying drawing 1.
accompanying drawing 5 is I part partial enlarged drawings in accompanying drawing 3.
accompanying drawing 6 is II part partial enlarged drawings in accompanying drawing 3.
accompanying drawing 7 is III part partial enlarged drawings in accompanying drawing 2.
embodiment:
embodiment 1:
a kind of tulwar slide block variable-angle device based on gear-rack drive, its composition comprises: slide block 7, described slide block is connected with axle 5 by screw A1, described axle adopts shaft hole matching to be connected with guides mount pad 2, axle sleeve 3 and roller guide 4 described axle be equipped with, the leading edge of described roller guide and tulwar 8 is fitted, and adjust contact distance by pad 6, gear shaft 11 is connected with described slide block by bearing 14, by set nut 12 and lock washer 13, described gear shaft is fixed on described slide block, described tulwar is connected with tooth bar 9 by screw B10, locking pin 17 described slide block is equipped with, spring 16 described locking pin is equipped with, wing nut 15 is housed outside described locking pin.
embodiment 2:
the tulwar slide block variable-angle device based on gear-rack drive according to embodiment 1, described tulwar is provided with groove, and described tooth bar is arranged in described groove; Described tulwar is provided with pin-and-hole, and described locking pin extend in described pin-and-hole under the pressure of described spring.

Claims (2)

1. the tulwar slide block variable-angle device based on gear-rack drive, its composition comprises: slide block, it is characterized in that: described slide block is connected with axle by screw A, described axle and guides mount pad adopt shaft hole matching to be connected, axle sleeve and roller guide described axle be equipped with, described roller guide and the leading edge of tulwar are fitted, and by pad adjustment contact distance, gear shaft is connected with described slide block by bearing, by set nut and lock washer, described gear shaft is fixed on described slide block, described tulwar is connected with tooth bar by screw B, described slide block is equipped with locking pin, described locking pin is equipped with spring, outside described locking pin, wing nut is housed.
2. the tulwar slide block variable-angle device based on gear-rack drive according to claim 1, it is characterized in that: described tulwar is provided with groove, described tooth bar is arranged in described groove; Described tulwar is provided with pin-and-hole, and described locking pin extend in described pin-and-hole under the pressure of described spring.
CN201520548394.4U 2015-07-27 2015-07-27 Tulwar slider becomes angle device based on rack and pinion drive Expired - Fee Related CN204788885U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520548394.4U CN204788885U (en) 2015-07-27 2015-07-27 Tulwar slider becomes angle device based on rack and pinion drive

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520548394.4U CN204788885U (en) 2015-07-27 2015-07-27 Tulwar slider becomes angle device based on rack and pinion drive

Publications (1)

Publication Number Publication Date
CN204788885U true CN204788885U (en) 2015-11-18

Family

ID=54528905

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520548394.4U Expired - Fee Related CN204788885U (en) 2015-07-27 2015-07-27 Tulwar slider becomes angle device based on rack and pinion drive

Country Status (1)

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CN (1) CN204788885U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105136424A (en) * 2015-07-27 2015-12-09 中国航空工业集团公司哈尔滨空气动力研究所 Bent blade sliding block angle change device driven by gear and rack and angle change method
CN105352703A (en) * 2015-11-26 2016-02-24 中国航空工业集团公司哈尔滨空气动力研究所 Curved knife slide block angle-varying mechanism based on bevel pulley guiding and angle-varying method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105136424A (en) * 2015-07-27 2015-12-09 中国航空工业集团公司哈尔滨空气动力研究所 Bent blade sliding block angle change device driven by gear and rack and angle change method
CN105136424B (en) * 2015-07-27 2018-03-06 中国航空工业集团公司哈尔滨空气动力研究所 Tulwar sliding block variable-angle device and angle changing method based on gear-rack drive
CN105352703A (en) * 2015-11-26 2016-02-24 中国航空工业集团公司哈尔滨空气动力研究所 Curved knife slide block angle-varying mechanism based on bevel pulley guiding and angle-varying method
CN105352703B (en) * 2015-11-26 2018-03-06 中国航空工业集团公司哈尔滨空气动力研究所 The tulwar sliding block angle shift mechanism and angle changing method being oriented to based on cone pulley

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

Granted publication date: 20151118

Termination date: 20160727