CN106354961A - Rapid generating method of wire rope pulley mechanism - Google Patents

Rapid generating method of wire rope pulley mechanism Download PDF

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Publication number
CN106354961A
CN106354961A CN201610802515.2A CN201610802515A CN106354961A CN 106354961 A CN106354961 A CN 106354961A CN 201610802515 A CN201610802515 A CN 201610802515A CN 106354961 A CN106354961 A CN 106354961A
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CN
China
Prior art keywords
wire rope
rope pulley
pulley mechanism
design
platform
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
CN201610802515.2A
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Chinese (zh)
Inventor
赵喆
李林文
田剑波
姜逸民
曹丹青
孟庆堂
陆波
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.)
Commercial Aircraft Corp of China Ltd
Shanghai Aircraft Design and Research Institute Commercial Aircraft Corporation of China Ltd
Original Assignee
Commercial Aircraft Corp of China Ltd
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Filing date
Publication date
Application filed by Commercial Aircraft Corp of China Ltd filed Critical Commercial Aircraft Corp of China Ltd
Priority to CN201610802515.2A priority Critical patent/CN106354961A/en
Publication of CN106354961A publication Critical patent/CN106354961A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Ropes Or Cables (AREA)

Abstract

The invention relates to a rapid generating method of a wire rope pulley mechanism. The method includes the steps of designing input, inputting an optimization target, determining interface parameters, rapidly obtaining the optimization result of mechanism design parameters, transmitting the optimization result to a parameterization model of a CAD platform in a cross-platform mode, and automatically generating a mechanism digital model through parameterization of the CAD platform so as to rapidly optimize parts of the wire rope pulley mechanism. By means of the method, the iterative process in traditional design can be simplified, the rapid design and change of the parts of the wire rope pulley mechanism are achieved, and the optimal solution is found to meet the related system design requirements, design standards and boundary conditions.

Description

A kind of rapid generation of wire rope pulley mechanism
Technical field
The present invention relates to aircraft wire rope pulley mechanism, more particularly, to a kind of side of quickly generating of wire rope pulley mechanism Method.
Background technology
Aircraft wire rope pulley mechanism is mainly by cable wire, cable connector, pulley, sectional wheel, turnbuckle and tension compensating The parts such as device form, and are applied to rudder face control more, meet an urgent need and put manipulation, shut down the aspects such as emergency brake manipulation.
During traditional design, as shown in fig. 1, wire rope pulley mechanism design cycle comprises the following steps: designer Member proposes design according to design requirement, design specification and boundary condition;Confirm to open according to design specification and boundary condition Exhibition design calculates and scheme confirms;Draw out parts digital-to-analogue according to design;Whether checking design meets correlation sets Meter demand and boundary constraint;Meet all design requirements by iterating until design.
For complicated wire rope pulley mechanism, system design is often limited by the design constraint of many-sided close coupling, design Process generally requires to carry out iteration repeatedly and correction, and the design cycle is longer, workload is larger.Meanwhile, parts digital-to-analogue It is generally basede on design to be drawn, once design requirement or boundary condition change, design need to recalculate more Newly confirm, it is more inconvenient that the modification cycle is longer, parts digital-to-analogue draws change.
Content of the invention
In order to solve problems of the prior art, the present invention provides a kind of fast fast-growing of improved wire rope pulley mechanism One-tenth method.
The method according to the invention is capable of wire rope pulley mechanism and quickly designs, and realizes wire rope pulley parts design number According to quick transmission, realize quickly generating of wire rope pulley parts.
Specifically, the rapid generation of the wire rope pulley mechanism according to the present invention includes step:
Design input;
Input optimization aim;
Determine interface parameters;
Rapid solving goes out the optimum results of mechanism design parameter;
The cross-platform parameterized model being transferred to cad platform of described optimum results;And
Cad platform parameters automatically generate mechanism's digital-to-analogue.
Wherein, to include design specification, design requirement, boundary condition and preliminary wire rope pulley mechanism cad flat for design input The parameterized model of platform.
Wherein, described interface parameters includes the size of parts to be optimized in wire rope pulley mechanism.
Wherein, the optimum results of described mechanism design parameter are obtained in matlab based on interior point method.
Wherein, based on vb, the optimum results of described mechanism design parameter are passed to the cad platform of wire rope pulley mechanism Parameterized model.
Described cad platform is catia software, and described optimum results pass to catia parameterized model;Described cad platform Parametrization automatically generates mechanism's digital-to-analogue, specially realize in catia parameterized model wire rope pulley mechanism parts fast Fast optimization design.
With respect to traditional wire rope pulley mechanism design method, the method for the present invention can simplify the iteration mistake in traditional design Journey, realizes quick design, the change of wire rope pulley mechanism parts, seeks optimal solution to meet related system design requirement, to set Meter specification and boundary condition.
Brief description
The further feature of the present invention and advantage will be more preferable by the preferred implementation below in conjunction with accompanying drawing detailed description Ground understands, wherein:
The flow chart that Fig. 1 shows the rapid generation of the wire rope pulley mechanism according to prior art;And
The flow chart that Fig. 2 shows the rapid generation of wire rope pulley mechanism according to a preferred embodiment of the invention.
Specific embodiment
In the specific descriptions of following preferred embodiment, by the accompanying drawing with reference to appended by a composition present invention part.Institute Attached accompanying drawing has been illustrated by way of example and has been capable of specific embodiment.The embodiment of example is not intended as Limit is according to all embodiments of the present invention.It is appreciated that without departing from the scope of the present invention, it is possible to use other Embodiment is it is also possible to carry out structural or logicality modification.
The flow chart that Fig. 2 shows the rapid generation of wire rope pulley mechanism according to a preferred embodiment of the invention. The method comprising the steps of:
(1) design input
Design inputs and includes following information:
A) design specification, for example: GB, army be marked with and mechanical design handbook in relevant regulations etc.;
B) design requirement, for example: need drive system ratio of realization etc.;
C) boundary condition, for example: based on factors such as installation environment, pulley intensity requirement, actuator travel restrictions, cable wire is slided The constraint that wheel mechanism element size proposes;
D) parameterized model of preliminary wire rope pulley mechanism cad platform.Cad platform in the present invention is not limited in Catia software or proe, the cad software such as solidworks.
(2) input optimization aim
Input this suboptimization and calculate the optimization aim needing to reach.
(3) determine interface parameters
Interface parameters includes parts critical size to be optimized in wire rope pulley mechanism, based on vb, set up excel, Communication interface between the softwares such as matlab and catia, the transmission optimizing data for follow-up parts critical size is set up logical News channel.
Above-mentioned (2) and (3) step do not have sequencing.
(4) optimum results of mechanism design parameter are tried to achieve in matlab based on interior point method
According to design input, in matlab, wire rope pulley is obtained based on interior point method (interior point method) The optimum results of the mechanism design parameter of mechanism, i.e. meet the element size of the wire rope pulley mechanism of design input requirements most.
(5) optimum results of mechanism design parameter are passed to catia parameterized model
Based on vb, the optimum results of mechanism design parameter are passed to the catia model of wire rope pulley mechanism.
(6) realize wire rope pulley mechanism parts fast optimal design in catia
By the optimum results of the mechanism design parameter of the wire rope pulley obtained mechanism part size, transmitted by communication interface To catia.The parts critical size of wire rope pulley mechanism is carried out with fast velocity modulation ginseng change, thus realizing cable wire in catia The parts rapid Optimum of pulley mechanism.
With respect to traditional wire rope pulley mechanism design method, the present invention can simplify the iterative process in traditional design, realizes The quick design of wire rope pulley mechanism parts, change, seek optimal solution with meet related system design requirement, design specification and Boundary condition.
More than have revealed that the technology contents of the specific embodiment of the present invention and technical characterstic it being understood, however, that at this Under bright creative ideas, the feature that those skilled in the art can be explicitly illustrated to various features disclosed above and non-here Combination make various changes and improve, but broadly fall into protection scope of the present invention.The description of above-described embodiment be exemplary and It is not restricted, protection scope of the present invention is determined by claim.

Claims (6)

1. a kind of rapid generation of wire rope pulley mechanism is it is characterised in that include step:
Design input;
Input optimization aim;
Determine interface parameters;
Rapid solving goes out the optimum results of mechanism design parameter;
The cross-platform parameterized model being transferred to cad platform of described optimum results;And
Cad platform parameters automatically generate mechanism's digital-to-analogue.
2. the rapid generation of wire rope pulley mechanism according to claim 1 is it is characterised in that design input inclusion sets Meter specification, the parameterized model of design requirement, boundary condition and preliminary wire rope pulley mechanism cad platform.
3. the rapid generation of wire rope pulley mechanism according to claim 1 is it is characterised in that described interface parameters bag Include the size of parts to be optimized in wire rope pulley mechanism.
4. the rapid generation of wire rope pulley mechanism according to claim 1 is it is characterised in that be based in matlab Interior point method obtains the optimum results of described mechanism design parameter.
5. the rapid generation of wire rope pulley mechanism according to claim 1 is it is characterised in that based on vb by described machine The optimum results of structure design parameter pass to the parameterized model of the cad platform of wire rope pulley mechanism.
6. the rapid generation of the wire rope pulley mechanism according to any one of claim 1-5 is it is characterised in that described Cad platform is catia software;
Described optimum results pass to catia parameterized model;
It is to realize wire rope pulley mechanism in catia parameterized model that described cad platform parameters automatically generate mechanism's digital-to-analogue The fast optimal design of parts.
CN201610802515.2A 2016-09-05 2016-09-05 Rapid generating method of wire rope pulley mechanism Pending CN106354961A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610802515.2A CN106354961A (en) 2016-09-05 2016-09-05 Rapid generating method of wire rope pulley mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610802515.2A CN106354961A (en) 2016-09-05 2016-09-05 Rapid generating method of wire rope pulley mechanism

Publications (1)

Publication Number Publication Date
CN106354961A true CN106354961A (en) 2017-01-25

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Application Number Title Priority Date Filing Date
CN201610802515.2A Pending CN106354961A (en) 2016-09-05 2016-09-05 Rapid generating method of wire rope pulley mechanism

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107945246A (en) * 2017-11-07 2018-04-20 中船黄埔文冲船舶有限公司 Method, apparatus, terminal device and the storage medium of Parametric Drawing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101980227A (en) * 2010-11-25 2011-02-23 中南大学 CAD system for composite type earth pressure shield cutter head
CN102054106A (en) * 2010-12-31 2011-05-11 吴晓军 Structure optimization design method and system
CN102184285A (en) * 2011-05-03 2011-09-14 三一集团有限公司 Digital prototyping design integrated development method and system
CN103870634A (en) * 2014-02-24 2014-06-18 上海宇航系统工程研究所 Quick design optimization method for large structure

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101980227A (en) * 2010-11-25 2011-02-23 中南大学 CAD system for composite type earth pressure shield cutter head
CN102054106A (en) * 2010-12-31 2011-05-11 吴晓军 Structure optimization design method and system
CN102184285A (en) * 2011-05-03 2011-09-14 三一集团有限公司 Digital prototyping design integrated development method and system
CN103870634A (en) * 2014-02-24 2014-06-18 上海宇航系统工程研究所 Quick design optimization method for large structure

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
刘焕进等: "《MATLAB从零到进阶》", 31 December 2012 *
闻邦: "《产品的制造性能及可视优化设计:基于系统工程的产品综合设计理论与方法》", 31 January 2010 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107945246A (en) * 2017-11-07 2018-04-20 中船黄埔文冲船舶有限公司 Method, apparatus, terminal device and the storage medium of Parametric Drawing

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Application publication date: 20170125