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公开(公告)号:US20160229539A1
公开(公告)日:2016-08-11
申请号:US14618052
申请日:2015-02-10
申请人: AMI INDUSTRIES, INC.
CPC分类号: B60N2/23 , B60N2/0296 , B60N2/0875 , B64D11/0639 , B64D11/064 , B64D11/0696 , F16H21/02 , F16H37/14
摘要: Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction, and the linear actuator may activate a second adjustable feature by moving in a second direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature and the second adjustable feature from the linear actuator in response to loss of power to the linear actuator.
摘要翻译: 本文公开了具有双功能线性致动器的飞机座椅的系统和方法。 线性致动器可以通过沿第一方向移动来激活第一可调特征,并且线性致动器可以通过沿第二方向移动来激活第二可调特征。 线性致动器可以包括去耦机构。 解耦机构可以响应于线性致动器的功率损失,将第一可调特征和第二可调特征与线性致动器分离。
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公开(公告)号:US20170305555A1
公开(公告)日:2017-10-26
申请号:US15643997
申请日:2017-07-07
申请人: AMI INDUSTRIES, INC.
CPC分类号: B60N2/23 , B60N2/0296 , B60N2/0875 , B64D11/0639 , B64D11/064 , B64D11/0696 , F16H21/02 , F16H37/14
摘要: Systems and methods are disclosed herein for an aircraft seat with a dual-function linear actuator. The linear actuator may activate a first adjustable feature by moving in a first direction, and the linear actuator may activate a second adjustable feature by moving in a second direction. The linear actuator may include a decoupling mechanism. The decoupling mechanism may decouple the first adjustable feature and the second adjustable feature from the linear actuator in response to loss of power to the linear actuator.
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