東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Development of magnetorheological fl...

University of Maryland, College Park.

Linked to FindBook

Google Book

Amazon

博客來

Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation./
Author:	Hu, Wei.
Description:	221 p.
Notes:	Chair: Norman M. Wereley.
Contained By:	Dissertation Abstracts International66-12B.
Subject:	Engineering, Aerospace. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3202412
ISBN:	9780542475061

Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation.
Hu, Wei.

Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation. - 221 p.

Chair: Norman M. Wereley.

Thesis (Ph.D.)--University of Maryland, College Park, 2005.

Conventional lag dampers use passive materials, such as elastomers, to dissipate energy and provide stiffness, but their damping and stiffness levels diminish markedly as amplitude of damper motion increases. Magnetorheological (MR) fluids based dampers have controllable damping with little or no stiffness. In order to combine the advantages of both elastomeric materials and MR fluids, semi-active magnetorheological fluid elastomeric (MRFE) lag dampers are developed in this thesis. In such a damper configuration, magnetic valves are incorporated into the chamber enclosed by elastomeric layers. Preliminary MRFE damper design analysis was conducted using quasi-steady Bingham-plastic MR flow mode analysis, and MRFE damper performance was evaluated analytically. To investigate the feasibility of using a combination of magnetorheological (MR) fluids and elastomeric materials for augmentation of lag mode damping in helicopters, a semi-active linear stroke MRFE lag damper was developed as a retrofit to an existing elastomeric helicopter lag damper. Consistent with sinusoidal loading conditions for a helicopter lag damper, single frequency (lag/rev) and dual frequency (lag/rev and 1/rev) sinusoidal loading were applied to the MRFE damper. Complex modulus and equivalent damping were used to compare the characteristics of the MRFE damper with the passive elastomeric damper. The experimental damping characteristics of the MRFE damper were consistent with the analytical results obtained from the Bingham plastic analysis of the MR valve. Based on measurements, the Field-OFF MRFE characteristics are similar to the passive elastomeric damping, and controllable damping as a function of different flight conditions is also feasible as the applied current is varied in the MR valve.

ISBN: 9780542475061Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation.
LDR:03313nmm 2200277 a 45 001 875471
005 20100826
008 100826s2005 eng d
020 $a 9780542475061
035 $a (UMI)AAI3202412
035 $a AAI3202412
040 $a UMI $c UMI
100 1 $a Hu, Wei. $3 1043762
245 1 0 $a Development of magnetorheological fluid elastomeric dampers for helicopter stability augmentation.
300 $a 221 p.
500 $a Chair: Norman M. Wereley.
500 $a Source: Dissertation Abstracts International, Volume: 66-12, Section: B, page: 6749.
502 $a Thesis (Ph.D.)--University of Maryland, College Park, 2005.
520 $a Conventional lag dampers use passive materials, such as elastomers, to dissipate energy and provide stiffness, but their damping and stiffness levels diminish markedly as amplitude of damper motion increases. Magnetorheological (MR) fluids based dampers have controllable damping with little or no stiffness. In order to combine the advantages of both elastomeric materials and MR fluids, semi-active magnetorheological fluid elastomeric (MRFE) lag dampers are developed in this thesis. In such a damper configuration, magnetic valves are incorporated into the chamber enclosed by elastomeric layers. Preliminary MRFE damper design analysis was conducted using quasi-steady Bingham-plastic MR flow mode analysis, and MRFE damper performance was evaluated analytically. To investigate the feasibility of using a combination of magnetorheological (MR) fluids and elastomeric materials for augmentation of lag mode damping in helicopters, a semi-active linear stroke MRFE lag damper was developed as a retrofit to an existing elastomeric helicopter lag damper. Consistent with sinusoidal loading conditions for a helicopter lag damper, single frequency (lag/rev) and dual frequency (lag/rev and 1/rev) sinusoidal loading were applied to the MRFE damper. Complex modulus and equivalent damping were used to compare the characteristics of the MRFE damper with the passive elastomeric damper. The experimental damping characteristics of the MRFE damper were consistent with the analytical results obtained from the Bingham plastic analysis of the MR valve. Based on measurements, the Field-OFF MRFE characteristics are similar to the passive elastomeric damping, and controllable damping as a function of different flight conditions is also feasible as the applied current is varied in the MR valve.
520 $a A second key objective of the present research is to develop an analytical model to describe the nonlinear behavior demonstrated by an MRFE damper. Since the damping behavior of both elastomers and MR fluids is dominated by friction mechanisms, a rate-dependent elasto-slide element is developed to describe the friction characteristics. An MR model developed from a single elasto-slide element successfully emulated the yield behavior of the MR damper, and this model captured nonlinear amplitude and frequency dependent behavior of MR dampers using constant model parameters. (Abstract shortened by UMI.)
590 $a School code: 0117.
650 4 $a Engineering, Aerospace. $3 1018395
690 $a 0538
710 2 0 $a University of Maryland, College Park. $3 657686
773 0 $t Dissertation Abstracts International $g 66-12B.
790 $a 0117
790 1 0 $a Wereley, Norman M., $e advisor
791 $a Ph.D.
792 $a 2005
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3202412