公开(公告)号：US08640782B2

公开(公告)日：2014-02-04

申请号：US13504902

申请日：2011-10-31

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： A62C25/00 ,  A62C27/00 ,  A62C29/00

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。

公开(公告)号：US09180325B2

公开(公告)日：2015-11-10

申请号：US14340377

申请日：2014-07-24

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： A62C25/00 ,  A62C27/00 ,  A62C29/00 ,  A62C3/02 ,  B64D1/16 ,  A62C37/36

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。

公开(公告)号：US20140102732A1

公开(公告)日：2014-04-17

申请号：US14133411

申请日：2013-12-18

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： A62C3/02 ,  B64D1/16

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。

公开(公告)号：US20130199804A1

公开(公告)日：2013-08-08

申请号：US13504902

申请日：2011-10-31

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： B64D1/16

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。

公开(公告)号：US20140367128A1

公开(公告)日：2014-12-18

申请号：US14340377

申请日：2014-07-24

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： A62C3/02 ,  B64D1/16 ,  A62C37/36

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。

公开(公告)号：US08820422B2

公开(公告)日：2014-09-02

申请号：US14133411

申请日：2013-12-18

申请人： Leonard K. Parker

发明人： Leonard K. Parker

IPC分类号： A62C25/00 ,  A62C27/00 ,  A62C29/00

CPC分类号： A62C3/0242 ,  A62C3/0228 ,  A62C37/04 ,  B64D1/16

摘要： An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retardant contained in the tank. The tank includes an outlet extending through a sidewall of the aircraft's fuselage, through which retardant may be delivered to a target. The system also includes a discharge gate operative to open and close the outlet. An actuation mechanism is disposed on the exterior of the tank and operatively coupled to the at least one discharge gate. A variable flow controller controls the discharge gate open position in order to provide retardant over a desired area of terrain. A one-way flapper is disposed in the pressure opening and is operative to allow pressure in the fuselage to enter the tank while inhibiting retardant from spilling from the tank.

摘要翻译： 一种空中阻燃剂递送系统，包括可安装在飞行器的机身中的阻燃罐。 该罐包括与机身流体连通的压力开口，使得机身中的压力可以作用于容纳在容器中的阻燃剂。 该箱包括延伸穿过飞行器机身侧壁的出口，通过该出口可将阻燃剂输送到目标。 该系统还包括可操作以打开和关闭出口的排出口。 致动机构设置在罐的外部并且可操作地耦合到至少一个排出门。 可变流量控制器控制排放门打开位置，以便在所需的地形区域上提供阻滞。 单向挡板设置在压力开口中，并且操作以允许机身中的压力进入箱体，同时抑制阻挡剂从罐中溢出。