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1. 发明申请

US20160185446A1 TRIM ADJUSTMENT DEVICE, AIRCRAFT, AND METHOD OF PERFORMING TRIM ADJUSTMENT 有权
标题翻译： TRIM调整装置，飞机和执行TRIM调整的方法
公开(公告)号：US20160185446A1
公开(公告)日：2016-06-30
申请号：US14186281
申请日：2014-02-21
申请人： MITSUBISHI AIRCRAFT CORPORATION
发明人： Masaya MIYOSHI
IPC分类号： B64C13/08 , B64D45/00
CPC分类号： B64C13/08 , B64D45/0005
摘要： Trim adjustment devices 20, 30, 40 at least include trim control switches 21, 31, 41 for performing a trim adjustment; acquisition sections 22, 32, 42 for acquiring a designated value for a position designated through the operation of the switches 21, 31, 41; and converting sections 23, 33, 43 for converting the designated value to a converted designated value expressed in different units. The switches 21, 31, 41 operate at a changeable rate in which the designated value changes at a prescribed amount of change per unit time, the prescribed amount of change expressed in units of the designated value before the conversion. The sections 23, 33, 43 converts the designated value to the converted designated value expressed in minimum units (0.1 UNIT) based on the product of the changeable rate and a click time period required for clicking the switches 21, 31, 41 once.
摘要翻译：修剪调节装置20,30,40至少包括用于进行修整调整的修剪控制开关21,31,41。获取部分22,32,42，用于获取通过开关21,31,41的操作指定的位置的指定值; 以及用于将指定值转换成以不同单位表示的转换指定值的转换部23,33,43。开关21,31,41以指定值以每单位时间的规定变化量变化的变化率进行动作，该变更量以变换前的指定值为单位表示。部分23,33,43基于可变速率和点击开关21,31,41所需的点击时间的乘积，将指定值转换为以最小单位（0.1单位）表示的转换的指定值。

2. 发明申请

US20150175273A1 WARNING SYSTEM OF AIRCRAFT AND AIRCRAFT 有权
标题翻译：警告飞机和飞机系统
公开(公告)号：US20150175273A1
公开(公告)日：2015-06-25
申请号：US14186137
申请日：2014-02-21
申请人： Mitsubishi Aircraft Corporation
发明人： Masaya MIYOSHI
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64C13/10
摘要： A warning system 10 that warns of saturation of the control capability for the moving surface such as an elevator 4 and a rudder 8 of an aircraft has a determination section 31 that determines whether or not the control capability for the moving surface is saturated, and a display 50 that issues a warning when the determination section 31 determines that the control capability for the moving surface is saturated. The determination section 31 determines that the control capability for the elevator 4 is saturated, when a control target position of the elevator 4 by, for example, a control stick (column) is larger than a first reference position indicating an operation limit of the elevator 4, and a present position of the column is smaller than a second reference position indicating an operation limit of the column.
摘要翻译：警告系统10，其对运动面的控制能力饱和，例如飞机的电梯4和方向舵8具有确定部31，其确定移动表面的控制能力是否饱和，当确定部分31确定移动表面的控制能力饱和时发出警告的显示器50。当电梯4的控制目标位置例如控制棒（列）大于指示电梯的操作限制的第一参考位置时，确定部31确定电梯4的控制能力饱和 4，并且列的当前位置小于指示列的操作限制的第二参考位置。

3. 发明申请

US20140253348A1 WARNING SYSTEM FOR AIRCRAFT, AND AIRCRAFT 有权
标题翻译：用于飞机和飞机的警告系统
公开(公告)号：US20140253348A1
公开(公告)日：2014-09-11
申请号：US14192072
申请日：2014-02-27
申请人： Mitsubishi Aircraft Corporation
发明人： Naoto MAEDA , Masaya MIYOSHI
IPC分类号： B64D45/00
CPC分类号： B64D43/02
摘要： To provide a warning system that can issue a stall warning taking a flight environment into account. The warning system according to the present invention is a warning system for an aircraft, for issuing a warning in the case where there is a possibility of the aircraft stalling, and includes a selecting section for selecting one of two or more calculation criteria based on an icing state of the aircraft, a calculating section for calculating a stall angle based on the selected calculation criterion, and a warning section for comparing the calculated stall angle with a current angle of attack of the aircraft and issuing a stall warning if the current angle of attack exceeds the stall angle.
摘要翻译：提供一个警告系统，可以发出停车警告，考虑到飞行环境。根据本发明的警告系统是用于飞机的警告系统，用于在存在飞行器停止的可能性的情况下发出警告，并且包括：选择部，用于基于两个或多个计算标准中的一个来选择飞行器的结冰状态，用于基于所选择的计算标准计算失速角的计算部分，以及用于将所计算的失速角与当前飞行攻角相比较的警告部分，并且如果当前的角度攻击超过失速角。

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