-
公开(公告)号:WO2003100284A2
公开(公告)日:2003-12-04
申请号:PCT/US2003/015913
申请日:2003-05-21
Applicant: BELL HELICOPTER TEXTRON INC. , HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
Inventor: HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
IPC: F16F
CPC classification number: F16F1/387 , B64C27/001 , B64C2027/002 , F16F2228/08 , F16F2230/18 , Y10T74/18808 , Y10T74/19633 , Y10T74/19828 , Y10T74/19907 , Y10T74/2184 , Y10T74/2186
Abstract: A variable stiffness support is disclosed. The variable stiffness support has a support housing that is configured to adjust the orientation of an internal elastomer assembly. The support housing includes an adjustment mechanism, and the elastomer assembly includes an outer ring that encircles an elastomeric material, a central bushing embedded in the elastomeric material, and a plurality of shims embedded in the elastomeric material in a parallel planar fashion.
Abstract translation: 公开了一种可变刚度支撑件。 可变刚度支撑件具有配置成调节内部弹性体组件的取向的支撑壳体。 支撑壳体包括调节机构,并且弹性体组件包括环绕弹性体材料的外圈,嵌入弹性体材料的中心衬套以及以平行平面方式嵌入弹性体材料中的多个垫片。
-
公开(公告)号:WO2003100284A3
公开(公告)日:2003-12-04
申请号:PCT/US2003/015913
申请日:2003-05-21
Applicant: BELL HELICOPTER TEXTRON INC. , HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
Inventor: HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
IPC: F16M13/00
Abstract: A variable stiffness support (111) has a support housing (113) that is configured to adjust the orientation of an internal elastomer assembly (115). The support housing (113) includes an adjustment mechanism (117), and the elastomer assembly (115) includes an outer ring (151) that encircles the elastomeric material (115), a central bushing (155) embedded in the elastomeric material (115), and a plurality of shims (159) embedded in the elastomeric material (115) in a parallel planar fashion.
-
公开(公告)号:WO2004111489A2
公开(公告)日:2004-12-23
申请号:PCT/US2003/030324
申请日:2003-09-24
Applicant: BELL HELICOPTER TEXTRON INC. , SMITH, Michael, R. , STAMPS, Frank, B. , LEE, Taeoh , HEVERLY, David, E., Jr. , PASCAL, Robert, J.
Inventor: SMITH, Michael, R. , STAMPS, Frank, B. , LEE, Taeoh , HEVERLY, David, E., Jr. , PASCAL, Robert, J.
IPC: F16F07/10
CPC classification number: B64C27/001 , B64C2027/005 , F16F7/1005 , F16F7/1034 , F16F7/108 , F16F13/08 , F16F13/24 , F16F13/26 , F16F15/005 , F16F15/027
Abstract: A tunable vibration isolator with active tuning elements having a housing, fluid chamber, and at least one tuning port. A piston is resiliently disposed within the housing. A vibration isolation fluid is disposed within the fluid chambers and the tuning ports. The tunable vibration isolator may employ either a solid tuning mass approach or a liquid tuning mass approach. The active vibration elements are preferably solid-state actuators.
Abstract translation: 具有主动调谐元件的可调节隔振器具有壳体,流体室和至少一个调谐端口。 活塞弹性地设置在壳体内。 振动隔离流体设置在流体室和调谐端口内。 可调谐隔振器可以采用固体调谐质量方法或液体调谐质量方法。 主动振动元件优选为固态致动器。
-
公开(公告)号:EP1543253A2
公开(公告)日:2005-06-22
申请号:EP03816302.8
申请日:2003-09-24
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor: SMITH, Michael, R. , STAMPS, Frank, B. , LEE, Taeoh , HEVERLY, David, E., Jr. , PASCAL, Robert, J.
IPC: F16F7/10
CPC classification number: B64C27/001 , B64C2027/005 , F16F7/1005 , F16F7/1034 , F16F7/108 , F16F13/08 , F16F13/24 , F16F13/26 , F16F15/005 , F16F15/027
Abstract: A vibration isolator comprising: a piston (1605) resiliently disposed within a housing (1603) with a first set of seals (1607); a mount plate (1609) configured for attachment to a vibrating body, the piston being connected to the mount plate; an upper fluid chamber (1611) and a lower fluid chamber (1613), each being defined by the housing, the piston, and the first set of seals; a tuning port (1620) for fluid communication between the upper fluid chamber and the lower fluid chamber; a tuning fluid disposed within the upper fluid chamber, the lower fluid chamber, and the tuning port; and a piezo piston (1619) resiliently disposed with the housing, the piezo piston being configured to be driven by at least two piezoceramic actuators (1623).
Abstract translation: 图8所示的可调振动隔离器具有有源调谐元件,该有源调谐元件具有外壳,流体室和至少一个调谐端口。 活塞弹性地设置在壳体内。 振动隔离流体设置在流体腔室和调谐端口内。 可调振动隔离器可以采用固体调谐质量方法或液体调谐质量方法。 主动振动元件优选为固态致动器。
-
公开(公告)号:EP1506353B1
公开(公告)日:2006-11-08
申请号:EP03729044.2
申请日:2003-05-21
Applicant: Bell Helicopter Textron Inc.
Inventor: HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
IPC: F16F1/00
CPC classification number: F16F1/387 , B64C27/001 , B64C2027/002 , F16F2228/08 , F16F2230/18 , Y10T74/18808 , Y10T74/19633 , Y10T74/19828 , Y10T74/19907 , Y10T74/2184 , Y10T74/2186
Abstract: A variable stiffness support (111) has a support housing (113) that is configured to adjust the orientation of an internal elastomer assembly (115). The support housing (113) includes an adjustment mechanism (117), and the elastomer assembly (115) includes an outer ring (151) that encircles the elastomeric material (115), a central bushing (155) embedded in the elastomeric material (115), and a plurality of shims (159) embedded in the elastomeric material (115) in a parallel planar fashion.
-
公开(公告)号:EP1334289B1
公开(公告)日:2008-07-09
申请号:EP01973531.5
申请日:2001-09-26
Applicant: Bell Helicopter Textron Inc.
Inventor: SMITH, Michael, R. , STAMPS, Frank, B. , PASCAL, Robert, J.
CPC classification number: F16F7/10 , B64C27/001 , B64C2027/005
Abstract: A tunable vibration isolator (451, 551, 651, 681, 691, 721, 801, 901, 973) with active tuning elements (473, 475, 573, 673, 675, 689, 705, 707, 745, 747, 747, 819a, 819b) having a housing which defines fluid chambers. A piston (455, 555, 655, 695, 725, 805, 970) is disposed within the housing. A vibration isolation fluid is disposed within the fluid chambers. A passage (463, 563, 663, 735, 881, 904) having a predetermined diameter extends through the piston to permit the vibration isolation fluid to flow from one fluid chamber to the other. The tunable vibration isolator may employ either a solid tuning mass approach or a liquid tuning mass approach. In either case, active tuning elements, or actuators, are disposed in the fluid chambers to selectively tune the vibration isolator.
-
公开(公告)号:EP1334289A1
公开(公告)日:2003-08-13
申请号:EP01973531.5
申请日:2001-09-26
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor: SMITH, Michael, R. , STAMPS, Frank, B. , PASCAL, Robert, J.
IPC: F16F7/10
CPC classification number: F16F7/10 , B64C27/001 , B64C2027/005
Abstract: A tunable vibration isolator (451, 551, 651, 681, 691, 721, 801, 901, 973) with active tuning elements (473, 475, 573, 673, 675, 689, 705, 707, 745, 747, 747, 819a, 819b) having a housing which defines fluid chambers. A piston (455, 555, 655, 695, 725, 805, 970) is disposed within the housing. A vibration isolation fluid is disposed within the fluid chambers. A passage (463, 563, 663, 735, 881, 904) having a predetermined diameter extends through the piston to permit the vibration isolation fluid to flow from one fluid chamber to the other. The tunable vibration isolator may employ either a solid tuning mass approach or a liquid tuning mass approach. In either case, active tuning elements, or actuators, are disposed in the fluid chambers to selectively tune the vibration isolator.
-
公开(公告)号:EP1543253B1
公开(公告)日:2009-09-09
申请号:EP03816302.8
申请日:2003-09-24
Applicant: Bell Helicopter Textron Inc.
Inventor: SMITH, Michael, R. , STAMPS, Frank, B. , LEE, Taeoh , HEVERLY, David, E., Jr. , PASCAL, Robert, J.
CPC classification number: B64C27/001 , B64C2027/005 , F16F7/1005 , F16F7/1034 , F16F7/108 , F16F13/08 , F16F13/24 , F16F13/26 , F16F15/005 , F16F15/027
Abstract: A vibration isolator comprising: a piston (1605) resiliently disposed within a housing (1603) with a first set of seals (1607); a mount plate (1609) configured for attachment to a vibrating body, the piston being connected to the mount plate; an upper fluid chamber (1611) and a lower fluid chamber (1613), each being defined by the housing, the piston, and the first set of seals; a tuning port (1620) for fluid communication between the upper fluid chamber and the lower fluid chamber; a tuning fluid disposed within the upper fluid chamber, the lower fluid chamber, and the tuning port; and a piezo piston (1619) resiliently disposed with the housing, the piezo piston being configured to be driven by at least two piezoceramic actuators (1623).
-
公开(公告)号:EP1506353A2
公开(公告)日:2005-02-16
申请号:EP03729044.2
申请日:2003-05-21
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor: HAYNES, David, F. , WILLIAMS, David, L. , SMITH, Michael, R. , PASCAL, Robert, J.
IPC: F16F1/00
CPC classification number: F16F1/387 , B64C27/001 , B64C2027/002 , F16F2228/08 , F16F2230/18 , Y10T74/18808 , Y10T74/19633 , Y10T74/19828 , Y10T74/19907 , Y10T74/2184 , Y10T74/2186
Abstract: A variable stiffness support (111) has a support housing (113) that is configured to adjust the orientation of an internal elastomer assembly (115). The support housing (113) includes an adjustment mechanism (117), and the elastomer assembly (115) includes an outer ring (151) that encircles the elastomeric material (115), a central bushing (155) embedded in the elastomeric material (115), and a plurality of shims (159) embedded in the elastomeric material (115) in a parallel planar fashion.
-
-
-
-
-
-
-
-