公开(公告)号：US5595359A

公开(公告)日：1997-01-21

申请号：US343812

申请日：1994-11-22

Applicant: Michael J. Meneghetti

Inventor： Michael J. Meneghetti

IPC: B64C25/50

CPC classification number: B64C25/50 ,  B64C2025/345

Abstract: A steerable landing gear for an aircraft having a six wheel, three axle truck has a steerable axle on either the rear or both forward and rear axles of the truck. A set of wheels driven about a vertical shaft utilizes a single actuator and a walking beam.The present invention relates to multi-wheel landing gear trucks or bogies for large aircraft and particularly to a method and apparatus for steering a set of wheels.

Abstract translation: 用于具有六轮三轴卡车的飞机的可操纵起落架在卡车的后部或前后轴上都具有可操纵的轴。 围绕垂直轴驱动的一组轮子使用单个致动器和步进梁。 本发明涉及用于大型飞机的多轮起落架卡车或转向架，特别涉及用于转向一组车轮的方法和装置。

公开(公告)号：US06173920B1

公开(公告)日：2001-01-16

申请号：US08821369

申请日：1997-03-20

Applicant: Michael J. Meneghetti

Inventor： Michael J. Meneghetti

IPC: B64C2500

CPC classification number: B64C25/34 ,  B64C2025/345

Abstract: Very large aircraft landing gear using single mounted eight wheel bogie on dual shock struts. A primary or main two-stage shock absorber and a semi-articulating secondary or auxiliary single-stage shock absorber, each of which are mounted using the second and third axles as pivot joints in a four axle, eight wheel truck beam.

Abstract translation: 非常大的飞机起落架使用单个安装的八轮转向架在双冲击支柱上。 一个主要或主要的两级减震器和一个半关节的二次或辅助单级减震器，每个减震器都使用第二和第三轴作为枢轴接头安装在四轴八轮车梁上。

公开(公告)号：US5613651A

公开(公告)日：1997-03-25

申请号：US352326

申请日：1994-12-08

Applicant: Michael J. Meneghetti

Inventor： Michael J. Meneghetti

IPC: B64C25/50

CPC classification number: B64C25/50 ,  B64C2025/345

Abstract: Landing gear axle steering for an aircraft having a six wheel three axle truck. A set of wheels driven about a vertical shaft utilizes a single actuator alone without a walking beam.

Abstract translation: 具有六轮三轴卡车的飞机的起落架轴转向。 围绕垂直轴驱动的一组轮子单独使用单个致动器而不用步进梁。

公开(公告)号：US08087610B2

公开(公告)日：2012-01-03

申请号：US12358007

申请日：2009-01-22

Applicant: Dennis W. Martin ,  Michael J. Meneghetti ,  William E. Luce

Inventor： Dennis W. Martin ,  Michael J. Meneghetti ,  William E. Luce

IPC: B64C25/58

CPC classification number: B64C25/60

Abstract: An aircraft shock strut includes a cylinder and a piston movable within the cylinder. A lower bearing and an upper bearing provide sliding engagement between the cylinder and the piston. The upper bearing is fixed to the cylinder and provides sliding engagement with an outer surface the piston. An upper bearing that is fixed to the cylinder facilitates use of lighter weight materials for the cylinder without sacrificing durability.

Abstract translation: 飞机冲击支柱包括可在气缸内移动的气缸和活塞。 下轴承和上轴承提供气缸和活塞之间的滑动接合。 上轴承固定在气缸上，与活塞的外表面滑动啮合。 固定在气缸上的上轴承有利于使用较轻重量的材料用于气缸，而不会牺牲耐久性。

公开(公告)号：US5743491A

公开(公告)日：1998-04-28

申请号：US352337

申请日：1994-12-08

Applicant: Michael J. Meneghetti

Inventor： Michael J. Meneghetti

IPC: B64C25/34 ,  B64C25/22 ,  B64C25/58

CPC classification number: B64C25/34 ,  B64C2025/345

Abstract: Very large aircraft landing gear using single mounted eight wheel bogie on dual shock struts. A primary or main two-stage shock absorber and a semi-articulating secondary or auxiliary single-stage shock absorber, each of which are mounted using the second and third axles as pivot joints in a four axle, eight wheel truck beam.

Abstract translation: 非常大的飞机起落架使用单个安装的八轮转向架在双冲击支柱上。 一个主要或主要的两级减震器和一个半关节的二次或辅助单级减震器，每个减震器都使用第二和第三轴作为枢轴接头安装在四轴八轮车梁上。

公开(公告)号：US20100181423A1

公开(公告)日：2010-07-22

申请号：US12358007

申请日：2009-01-22

Applicant: Dennis W. Martin ,  Michael J. Meneghetti ,  William E. Luce

Inventor： Dennis W. Martin ,  Michael J. Meneghetti ,  William E. Luce

IPC: F16F9/54

CPC classification number: B64C25/60

Abstract: An aircraft shock strut includes a cylinder and a piston movable within the cylinder. A lower bearing and an upper bearing provide sliding engagement between the cylinder and the piston. The upper bearing is fixed to the cylinder and provides sliding engagement with an outer surface the piston. An upper bearing that is fixed to the cylinder facilitates use of lighter weight materials for the cylinder without sacrificing durability.

Abstract translation: 飞机冲击支柱包括可在气缸内移动的气缸和活塞。 下轴承和上轴承提供气缸和活塞之间的滑动接合。 上轴承固定在气缸上，与活塞的外表面滑动啮合。 固定在气缸上的上轴承有利于使用较轻重量的材料用于气缸，而不会牺牲耐久性。

公开(公告)号：US06679452B1

公开(公告)日：2004-01-20

申请号：US10278633

申请日：2002-10-22

Applicant: Justin D. Cottet ,  Michael J. Meneghetti ,  Brett D. Whitmer

Inventor： Justin D. Cottet ,  Michael J. Meneghetti ,  Brett D. Whitmer

IPC: B64C2510

CPC classification number: B64C1/0009 ,  B64C1/26 ,  B64C25/04 ,  B64C25/10 ,  B64C30/00 ,  B64C2001/0027 ,  B64C2001/0045 ,  B64D9/003 ,  B64D11/00 ,  B64D27/18 ,  B64D37/04 ,  Y02T50/12 ,  Y02T50/44 ,  Y02T50/46

Abstract: Landing gear support assemblies and associated methods of installation. In one embodiment, a landing gear support assembly usable with an aircraft wing includes an aft trunnion support beam having a base portion, an aft trunnion support spaced apart from the base portion, and a shear center axis extending from the base portion toward the aft trunnion support. The aft trunnion support can be at least approximately vertically aligned with the shear center axis. The base portion can be configured to be attached at least proximate to the rear wing spar with a plurality of fuse pins configured to fail and release the aft trunnion support beam from the rear wing spar when the landing gear exerts a preselected force against the aft trunnion support.

Abstract translation: 起落架支撑组件和相关的安装方法。 在一个实施例中，可与飞行器机翼一起使用的起落架支撑组件包括：后耳轴支撑梁，其具有基部部分，与基部部分间隔开的后耳轴支撑件以及从基部部分向后耳轴延伸的剪切中心轴线 支持。 后耳轴支撑件可以至少大致垂直于剪切中心轴线对准。 基座部分可以构造成至少靠近后翼梁连接，多个保险丝销构造成当起落架对后耳轴施加预选力时，使后翼翼梁失效并释放后耳轴支撑梁 支持。