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1. 发明申请

US20090294583A1 AIRCRAFT LANDING GEAR ASSEMBLY SHIMMY DAMPER 有权
标题翻译：飞机起落架装配减震器
公开(公告)号：US20090294583A1
公开(公告)日：2009-12-03
申请号：US12538241
申请日：2009-08-10
申请人： Paul Joseph Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
发明人： Paul Joseph Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
IPC分类号： B64C25/50
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025
摘要： An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. The assembly includes an elastomer encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment. The assembly includes a grease disposed between the outer elastomer surface and the nonelastomeric outer member frictional interface inner surface segment with the greased grooved outer elastomer surface engaging the nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating rotation.
摘要翻译：提供了一种飞行器车辆组件，其包括具有内轴向中心孔的非弹性外管状构件，其具有连接的平滑内表面段的管状圆柱形摩擦界面和具有外接合表面段的非弹性内构件。非弹性内部构件被旋转地容纳在外部构件内部轴向中心孔中，其中非弹性内支柱构件可在所述外部构件内旋转。组件包括包围非弹性内支柱构件外接合表面段的弹性体。弹性体具有内接合表面段和外槽弹性体表面，内接合表面段结合到非弹性内构件外接合表面段。组件包括设置在外弹性体表面和非弹性外部构件摩擦界面内表面段之间的润滑脂，其中润滑的槽外弹性体表面接合非弹性外构件摩擦界面内表面段并且阻止摆动旋转。

2. 发明授权

US07571876B2 Aircraft landing gear assembly shimmy damper 有权
标题翻译：飞机起落架组件摆动阻尼器
公开(公告)号：US07571876B2
公开(公告)日：2009-08-11
申请号：US11375945
申请日：2006-03-15
申请人： Paul Joseph Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
发明人： Paul Joseph Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
IPC分类号： B64C25/00 , F16F1/00
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025
摘要： An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. The assembly includes an elastomer encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment. The assembly includes a grease disposed between the outer elastomer surface and the nonelastomeric outer member frictional interface inner surface segment with the greased grooved outer elastomer surface engaging the nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating rotation.
摘要翻译：提供了一种飞行器车辆组件，其包括具有内轴向中心孔的非弹性外管状构件，其具有连接的平滑内表面段的管状圆柱形摩擦界面和具有外接合表面段的非弹性内构件。非弹性内部构件被旋转地容纳在外部构件内部轴向中心孔中，其中非弹性内支柱构件可在所述外部构件内旋转。组件包括包围非弹性内支柱构件外接合表面段的弹性体。弹性体具有内接合表面段和外槽弹性体表面，内接合表面段结合到非弹性内构件外接合表面段。组件包括设置在外弹性体表面和非弹性外部构件摩擦接口内表面段之间的润滑脂，其中润滑的带槽的外弹性体表面接合非弹性外构件摩擦接口内表面段并阻止摆动旋转。

3. 发明授权

US08534600B2 Aircraft landing gear assembly shimmy damper 有权
公开(公告)号：US08534600B2
公开(公告)日：2013-09-17
申请号：US12538241
申请日：2009-08-10
申请人： Paul J. Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
发明人： Paul J. Bachmeyer , Douglas A. Swanson , Bryan J. Pittman , Scott K. Thompson , Doug A. Hodgson
IPC分类号： B64C25/00 , F16F1/00
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025
摘要： An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. The assembly includes an elastomer encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment. The assembly includes a grease disposed between the outer elastomer surface and the nonelastomeric outer member frictional interface inner surface segment with the greased grooved outer elastomer surface engaging the nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating rotation.

4. 发明授权

US08434713B2 Aircraft front nose landing gear and method of making an aircraft landing gear 有权
标题翻译：飞机前鼻起落架和制造飞机起落架的方法
公开(公告)号：US08434713B2
公开(公告)日：2013-05-07
申请号：US13235832
申请日：2011-09-19
申请人： Paul Joseph Bachmeyer , Doug A. Hodgson
发明人： Paul Joseph Bachmeyer , Doug A. Hodgson
IPC分类号： B64C25/00
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025 , Y10T29/4998
摘要： An aircraft front nose landing gear having both elastomeric and nonelastomeric elements is provided along with a method of making the same. The aircraft front nose landing gear includes the ability to reduce/inhibit oscillating shimmy rotation vibrations. The method further provides for making a landing gear with a shimmy damper for further reducing oscillating rotations.
摘要翻译：提供具有弹性和非弹性元件的飞机前部起落架及其制造方法。飞机前部前起落架包括减少/禁止摆动振动旋转振动的能力。该方法进一步提供了制造具有减振器的起落架以进一步减少摆动旋转。

5. 发明申请

US20100187061A1 Aircraft front nose landing gear and method of making an aircraft landing gear 失效
标题翻译：飞机前鼻起落架和制造飞机起落架的方法
公开(公告)号：US20100187061A1
公开(公告)日：2010-07-29
申请号：US12583657
申请日：2009-08-24
申请人： Paul J. Bachmeyer , Doug A. Hodgson
发明人： Paul J. Bachmeyer , Doug A. Hodgson
IPC分类号： B64C25/50 , F16F7/06 , B23P17/00
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025 , Y10T29/4998
摘要： An aircraft vehicular front wheel landing gear assembly is provided that includes a nonelastomeric outer upper strut tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, and a nonelastomeric inner lower strut member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer strut member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer strut member. The assembly includes an elastomeric surface effect damper member encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomeric surface effect damper member has an inner bonding surface segment and an outer elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner strut member outer bonding surface segment. The assembly includes a surface effect lubricant disposed between the elastomeric surface effect damper outer elastomer surface and the nonelastomeric outer strut member frictional interface inner surface segment with the elastomeric surface effect damper outer elastomer surface engaging the nonelastomeric outer strut member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation.
摘要翻译：提供了一种飞行器车辆前轮起落架组件，其包括具有管状圆柱形摩擦接口内表面段的内轴向中心孔和具有外接合表面段的非弹性内底下支柱构件的非弹性外上支柱管构件。非弹性内部构件被旋转地容纳在外部支柱构件内部轴向中心孔中，非弹性内支柱构件可在所述外部支柱构件内旋转。组件包括包围非弹性内支柱构件外接合表面段的弹性体表面效应阻尼器构件。弹性体表面效应阻尼器构件具有内接合表面段和外弹性体表面，内接合表面段结合到非弹性内支柱构件外接合表面段。组件包括设置在弹性体表面效应阻尼器外弹性体表面和非弹性外支柱构件摩擦界面内表面段之间的表面效应润滑剂，弹性体表面效应阻尼器外弹性体表面接合非弹性外支柱构件摩擦界面内表面段并抑制振荡摇摆旋转。

6. 发明授权

US08020807B2 Aircraft front nose landing gear and method of making an aircraft landing gear 失效
标题翻译：飞机前鼻起落架和制造飞机起落架的方法
公开(公告)号：US08020807B2
公开(公告)日：2011-09-20
申请号：US12583657
申请日：2009-08-24
申请人： Paul J. Bachmeyer , Doug A. Hodgson
发明人： Paul J. Bachmeyer , Doug A. Hodgson
IPC分类号： B64C25/00
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025 , Y10T29/4998
摘要： An aircraft vehicular front wheel landing gear assembly is provided that includes a nonelastomeric outer upper strut tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, and a nonelastomeric inner lower strut member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer strut member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer strut member. The assembly includes an elastomeric surface effect damper member encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomeric surface effect damper member has an inner bonding surface segment and an outer elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner strut member outer bonding surface segment. The assembly includes a surface effect lubricant disposed between the elastomeric surface effect damper outer elastomer surface and the nonelastomeric outer strut member frictional interface inner surface segment with the elastomeric surface effect damper outer elastomer surface engaging the nonelastomeric outer strut member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation.
摘要翻译：提供了一种飞行器车辆前轮起落架组件，其包括具有管状圆柱形摩擦接口内表面段的内轴向中心孔和具有外接合表面段的非弹性内底下支柱构件的非弹性外上支柱管构件。非弹性内部构件被旋转地容纳在外部支柱构件内部轴向中心孔中，非弹性内支柱构件可在所述外部支柱构件内旋转。组件包括包围非弹性内支柱构件外接合表面段的弹性体表面效应阻尼器构件。弹性体表面效应阻尼器构件具有内接合表面段和外弹性体表面，内接合表面段结合到非弹性内支柱构件外接合表面段。组件包括设置在弹性体表面效应阻尼器外弹性体表面和非弹性外支柱构件摩擦界面内表面段之间的表面效应润滑剂，弹性体表面效应阻尼器外弹性体表面接合非弹性外支柱构件摩擦界面内表面段并抑制振荡摇摆旋转。

7. 发明申请

US20120055630A1 AIRCRAFT FRONT NOSE LANDING GEAR AND METHOD OF MAKING AN AIRCRAFT LANDING GEAR 有权
标题翻译：飞机前端索具及其制造航空器齿轮的方法
公开(公告)号：US20120055630A1
公开(公告)日：2012-03-08
申请号：US13235832
申请日：2011-09-19
申请人： Paul J. Bachmeyer , Doug A. Hodgson
发明人： Paul J. Bachmeyer , Doug A. Hodgson
IPC分类号： B32B37/14
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025 , Y10T29/4998
摘要： An aircraft front nose landing gear having both elastomeric and nonelastomeric elements is provided along with a method of making the same. The aircraft front nose landing gear includes the ability to reduce/inhibit oscillating shimmy rotation vibrations. The method further provides for making a landing gear with a shimmy damper for further reducing oscillating rotations.
摘要翻译：提供具有弹性和非弹性元件的飞机前部起落架及其制造方法。飞机前部前起落架包括减少/禁止摆动振动旋转振动的能力。该方法进一步提供了制造具有减振器的起落架以进一步减少摆动旋转。

8. 发明授权

US07578465B2 Aircraft front nose landing gear and method of making an aircraft landing gear 有权
标题翻译：飞机前鼻起落架和制造飞机起落架的方法
公开(公告)号：US07578465B2
公开(公告)日：2009-08-25
申请号：US11038851
申请日：2005-01-19
申请人： Paul J. Bachmeyer , Doug A. Hodgson
发明人： Paul J. Bachmeyer , Doug A. Hodgson
IPC分类号： B64C25/10
CPC分类号： B64C25/505 , F16F7/02 , F16F2224/025 , Y10T29/4998
摘要： An aircraft vehicular front wheel landing gear assembly is provided that includes a nonelastomeric outer upper strut tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, and a nonelastomeric inner lower strut member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer strut member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer strut member. The assembly includes an elastomeric surface effect damper member encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomeric surface effect damper member has an inner bonding surface segment and an outer elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner strut member outer bonding surface segment. The assembly includes a surface effect lubricant disposed between the elastomeric surface effect damper outer elastomer surface and the nonelastomeric outer strut member frictional interface inner surface segment with the elastomeric surface effect damper outer elastomer surface engaging the nonelastomeric outer strut member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation.
摘要翻译：提供了一种飞行器车辆前轮起落架组件，其包括具有管状圆柱形摩擦接口内表面段的内轴向中心孔和具有外接合表面段的非弹性内底下支柱构件的非弹性外上支柱管构件。非弹性内部构件被旋转地容纳在外部支柱构件内部轴向中心孔中，非弹性内支柱构件可在所述外部支柱构件内旋转。组件包括包围非弹性内支柱构件外接合表面段的弹性体表面效应阻尼器构件。弹性体表面效应阻尼器构件具有内接合表面段和外弹性体表面，内接合表面段结合到非弹性内支柱构件外接合表面段。组件包括设置在弹性体表面效应阻尼器外弹性体表面和非弹性外支柱构件摩擦界面内表面段之间的表面效应润滑剂，弹性体表面效应阻尼器外弹性体表面接合非弹性外支柱构件摩擦界面内表面段并抑制振荡摇摆旋转。

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