公开(公告)号：US20050116108A1

公开(公告)日：2005-06-02

申请号：US10714276

申请日：2003-11-14

申请人： John Morgenstern ,  James Bach ,  Alan Arslan

发明人： John Morgenstern ,  James Bach ,  Alan Arslan

IPC分类号： B64C1/00 ,  B64C30/00 ,  B64D27/18 ,  B64C1/38

CPC分类号： B64C1/0009 ,  B64C30/00 ,  B64C2001/0045 ,  B64D27/18 ,  Y02T50/12 ,  Y02T50/44

摘要： A system and method for configuring an aircraft for low sonic boom supersonic flight conditions includes redistributing lift of a wing by configuring the wing with one or more areas of far-field expansion ahead of areas of far-field compression. An equivalent area distribution goal curve is scaled to account for the equivalent area reduction due to excursions below to goal curve. A relaxed constraint allows the equivalent area distribution of the aircraft to be at or below the equivalent area distribution goal curve to enable multiple parameters to be configured to meet the equivalent area distribution constraint, as well as other constraints. The system and method can be adapted to aid in the design of any type of vehicle whose surfaces are subject to supersonic fluid flow, especially to reduce sonic boom.

摘要翻译： 用于配置用于低声波超音速飞行条件的飞行器的系统和方法包括通过在远场压缩区域之前的远场扩展的一个或多个区域配置机翼来重新分配机翼的升力。 将等效区域分布目标曲线缩放以考虑由于低于目标曲线的偏移所引起的等效面积减小。 轻松的约束允许飞机的等效面积分布处于等于或低于等效区域分布目标曲线，以使得可以配置多个参数以满足等效面积分布约束以及其他约束。 该系统和方法可以适用于任何类型的车辆的设计，其表面经受超音速流体流动，特别是减少声波爆震。

公开(公告)号：US20130213951A1

公开(公告)日：2013-08-22

申请号：US13401388

申请日：2012-02-21

申请人： Stephen Boedicker ,  James Bach

发明人： Stephen Boedicker ,  James Bach

IPC分类号： H05B1/02

CPC分类号： H05B1/0263

摘要： A control system for an oven including a plurality of heating elements positioned within the cooking cavity includes a temperature sensor configured to detect an air temperature within the cooking cavity, a user interface for receiving a desired temperature set point command, and a controller operatively coupled to the temperature sensor and user interface. The controller is configured to determine a power splitting ratio between the first and second heating elements based on user-specified cooking mode and/or type of food being cooked, determine a total power command signal based on a determined error value between the detected cavity air temperature and the desired temperature set point command, and adjust a power level of each of the first and second heating elements based on the total power command and the power splitting ratio.

摘要翻译： 一种用于包括位于烹饪腔内的多个加热元件的烘箱的控制系统包括配置成检测烹饪腔内的空气温度的温度传感器，用于接收所需温度设定点命令的用户界面，以及可操作地耦合到 温度传感器和用户界面。 控制器被配置为基于用户指定的烹饪模式和/或正在烹饪的食物的类型来确定第一和第二加热元件之间的功率分配比，基于检测到的空腔空气之间的确定的误差值来确定总功率命令信号 温度和期望的温度设定点指令，并且基于总功率命令和功率分配比来调整第一和第二加热元件中的每一个的功率电平。

公开(公告)号：US09089005B2

公开(公告)日：2015-07-21

申请号：US13401388

申请日：2012-02-21

申请人： Stephen Boedicker ,  James Bach

发明人： Stephen Boedicker ,  James Bach

IPC分类号： A21B1/00 ,  H05B1/02

CPC分类号： H05B1/0263

摘要： A control system for an oven including a plurality of heating elements positioned within the cooking cavity includes a temperature sensor configured to detect an air temperature within the cooking cavity, a user interface for receiving a desired temperature set point command, and a controller operatively coupled to the temperature sensor and user interface. The controller is configured to determine a power splitting ratio between the first and second heating elements based on user-specified cooking mode and/or type of food being cooked, determine a total power command signal based on a determined error value between the detected cavity air temperature and the desired temperature set point command, and adjust a power level of each of the first and second heating elements based on the total power command and the power splitting ratio.

摘要翻译： 一种用于烤箱的控制系统，包括位于烹饪腔内的多个加热元件，包括配置成检测烹饪腔内的空气温度的温度传感器，用于接收所需温度设定点命令的用户界面，以及可操作地耦合到 温度传感器和用户界面。 控制器被配置为基于用户指定的烹饪模式和/或正在烹饪的食物的类型来确定第一和第二加热元件之间的功率分配比，基于检测到的空腔空气之间的确定的误差值来确定总功率命令信号 温度和期望的温度设定点指令，并且基于总功率命令和功率分配比来调整第一和第二加热元件中的每一个的功率电平。