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1. 再颁专利

USRE42217E1 Airborne electromagnetic time domain system 有权
标题翻译：机载电磁时域系统
公开(公告)号：USRE42217E1
公开(公告)日：2011-03-15
申请号：US12343321
申请日：2008-12-23
申请人： Edward Beverly Morrison , Petr Valentinovich Kuzmin , Pavel Tishin
发明人： Edward Beverly Morrison , Petr Valentinovich Kuzmin , Pavel Tishin
IPC分类号： G01V3/16 , G01V3/165 , H01Q1/30
CPC分类号： G01V3/165
摘要： An airborne time domain electromagnetic surveying system is provided. The system includes a tow assembly with a flexible support frame. The flexible support frame spaced apart from the aircraft includes a transmitter section with a transmitter loop and a receiver section with a sensor aligned with the central axis of the transmitter section. The flexible support frame has a lightweight modular structure that enables the surface area of the transmitter section to be increased and decreased to suit particular survey applications. The transmitter loop sends a pulse in an “ON” interval, and in an “OFF” interval the sensor measures the earth response to the pulse. The tow assembly also includes a sensor for generating selected survey data in the “ON” interval. A transmitter driver enables the creation of earthbound pulse. The system components are linked to a computer and control computer program linked thereto for controlling the functions thereof. The invention also includes a method for producing survey data using the tow assembly of the invention.
摘要翻译：提供了一个空中时域电磁测量系统。该系统包括具有柔性支撑框架的丝束组件。与飞行器间隔开的柔性支撑框架包括具有发射器环的发射器部分和具有与发射器部分的中心轴对准的传感器的接收器部分。柔性支撑框架具有轻便的模块化结构，能够增加和减少变送器部分的表面积，以适应特定的勘测应用。发射机回路在“ON”间隔发送一个脉冲，在“OFF”间隔，传感器测量对脉冲的地球响应。牵引组件还包括用于在“接通”间隔中产生所选择的测量数据的传感器。发射机驱动器可以创建接地脉冲。系统组件链接到与之链接的计算机和控制计算机程序，以控制其功能。本发明还包括使用本发明的丝束组件产生测量数据的方法。

2. 发明授权

US07157914B2 Airborne electromagnetic time domain system, computer product and method 有权
标题翻译：机载电磁时域系统，计算机产品及方法
公开(公告)号：US07157914B2
公开(公告)日：2007-01-02
申请号：US10716813
申请日：2003-11-20
申请人： Edward Beverly Morrison , Petr Valentinovich Kuzmin , Pavel Tishin
发明人： Edward Beverly Morrison , Petr Valentinovich Kuzmin , Pavel Tishin
IPC分类号： G01V3/16 , G01V3/165 , H01Q1/30
CPC分类号： G01V3/165
摘要： An airborne time domain electromagnetic surveying system is provided. The system includes a tow assembly with a flexible support frame. The flexible support frame spaced apart from the aircraft includes a transmitter section with a transmitter loop and a receiver section with a sensor aligned with the central axis of the transmitter section. The flexible support frame has a lightweight modular structure that enables the surface area of the transmitter section to be increased and decreased to suit particular survey applications. The transmitter loop sends a pulse in an “ON” interval, and in an “OFF” interval the sensor measures the earth response to the pulse. The tow assembly also includes a sensor for generating selected survey data in the “ON” interval. A transmitter driver enables the creation of earthbound pulse. The system components are linked to a computer and control computer program linked thereto for controlling the functions thereof. The invention also includes a method for producing survey data using the tow assembly of the invention.
摘要翻译：提供了一个空中时域电磁测量系统。该系统包括具有柔性支撑框架的丝束组件。与飞行器间隔开的柔性支撑框架包括具有发射器环的发射器部分和具有与发射器部分的中心轴对准的传感器的接收器部分。柔性支撑框架具有轻便的模块化结构，能够增加和减少变送器部分的表面积，以适应特定的勘测应用。发射机回路在“ON”间隔发送一个脉冲，在“OFF”间隔，传感器测量对脉冲的地球响应。牵引组件还包括用于在“接通”间隔中产生所选择的测量数据的传感器。发射机驱动器可以创建接地脉冲。系统组件链接到与之链接的计算机和控制计算机程序，以控制其功能。本发明还包括使用本发明的丝束组件产生测量数据的方法。

3. 发明申请

US20050001622A1 Airborne electromagnetic time domain system, computer product and method 有权
标题翻译：机载电磁时域系统，计算机产品及方法
公开(公告)号：US20050001622A1
公开(公告)日：2005-01-06
申请号：US10716813
申请日：2003-11-20
申请人： Edward Morrison , Petr Kuzmin , Pavel Tishin
发明人： Edward Morrison , Petr Kuzmin , Pavel Tishin
IPC分类号： G01V3/165 , G01V3/16
CPC分类号： G01V3/165
摘要： An airborne time domain electromagnetic surveying system is provided. The system includes a tow assembly with a flexible support frame. The flexible support frame spaced apart from the aircraft includes a transmitter section with a transmitter loop and a receiver section with a sensor aligned with the central axis of the transmitter section. The flexible support frame has a lightweight modular structure that enables the surface area of the transmitter section to be increased and decreased to suit particular survey applications. The transmitter loop sends a pulse in an “ON” interval, and in an “OFF” interval the sensor measures the earth response to the pulse. The tow assembly also includes a sensor for generating selected survey data in the “ON” interval. A transmitter driver enables the creation of earthbound pulse. The system components are linked to a computer and control computer program linked thereto for controlling the functions thereof. The invention also includes a method for producing survey data using the tow assembly of the invention.
摘要翻译：提供了一个空中时域电磁测量系统。该系统包括具有柔性支撑框架的丝束组件。与飞行器间隔开的柔性支撑框架包括具有发射器环的发射器部分和具有与发射器部分的中心轴对准的传感器的接收器部分。柔性支撑框架具有轻便的模块化结构，能够增加和减少变送器部分的表面积，以适应特定的勘测应用。发射机回路在“ON”间隔发送一个脉冲，在“OFF”间隔，传感器测量对脉冲的地球响应。牵引组件还包括用于在“接通”间隔中产生所选择的测量数据的传感器。发射机驱动器可以创建接地脉冲。系统组件链接到与之链接的计算机和控制计算机程序，以控制其功能。本发明还包括使用本发明的丝束组件产生测量数据的方法。

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