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公开(公告)号：US20160229518A1
公开(公告)日：2016-08-11
申请号：US14515079
申请日：2014-10-15
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
CPC classification number: B64C3/48 , B64B1/08 , B64B1/14 , B64B1/26 , B64B1/58 , B64B2201/00 , B64C3/44 , B64C3/54 , B64C39/10 , F03D9/25 , F05B2240/921 , Y02E10/725
Abstract: The present invention is a variable geometry aircraft that is capable of morphing its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.
Abstract translation: 本发明是一种可变几何飞行器，其能够将其形状从对称的横截面浮力工艺变形到非对称提升体，甚至能够对称的零提升构型。 基本结构是具有可移动隆起的半刚性飞艇。 仰角的运动调节上表面和/或下表面的弯度，以实现提升体的变化形状。 这种转变改变了飞行器的升力和阻力特性，以改变飞行特性。 转换可以在飞行器机载时完成，并且不需要任何地面支撑设备。
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公开(公告)号：US20160023747A1
公开(公告)日：2016-01-28
申请号：US14746332
申请日：2015-06-22
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
CPC classification number: B64C3/38 , B64B1/00 , B64B2201/00 , B64C3/46 , B64D27/02 , B64D2211/00
Abstract: The present invention is a variable geometry aircraft that is capable of morphing its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The aircraft may include variable span, length, and camber. The variability of the structure and the flexible envelope allows the aircraft to adjust its aspect ratio along with the camber of the upper and/or lower surfaces to achieve varying shapes. This transformation changes both the lift and drag characteristics of the craft and may be accomplished while the craft is airborne.
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公开(公告)号：US10377465B2
公开(公告)日：2019-08-13
申请号：US14515079
申请日：2014-10-15
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
IPC: B64B1/20 , B64C1/00 , B64C17/00 , B64C3/48 , B64B1/08 , B64C3/54 , B64B1/26 , B64B1/14 , B64B1/58 , B64C3/44 , F03D9/25
Abstract: The present invention is a variable geometry aircraft that is capable of morphing its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.
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公开(公告)号：US11058246B1
公开(公告)日：2021-07-13
申请号：US16659089
申请日：2019-10-21
Applicant: Scott R. Kempshall , Tina L. Dyer
Inventor： Scott R. Kempshall , Tina L. Dyer
Abstract: A bag clamp having retention arms, capable of rotating about a pivoting axis between an open and closed position. The retention arms are connected to a locking mechanism configured to prevent the retention arms from pivoting to an open configuration when the locking mechanism is in an engaged setting. The arms are shaped to create an open receiving space. The open receiving space allows the bag clamp to receive a rigid structure to clamp onto while also receiving a bag's straps.
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公开(公告)号：US09623954B2
公开(公告)日：2017-04-18
申请号：US14341184
申请日：2014-07-25
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
CPC classification number: B64C3/46 , B64B1/08 , B64B1/14 , B64B1/26 , B64B1/58 , B64B2201/00 , B64C3/48 , B64C3/54 , B64C3/546 , B64C2201/022 , B64C2201/101 , B64C2201/105 , F03D1/04 , F03D9/25 , F03D9/32 , F05B2240/921 , Y02E10/725
Abstract: The present invention is a variable geometry lighter-than-air (LTA) aircraft that is adapted to morph its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.
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Patent Agency Ranking
公开(公告)号：US10448771B1
公开(公告)日：2019-10-22
申请号：US15412235
申请日：2017-01-23
Applicant: Scott R. Kempshall , Tina L. Dyer
Inventor： Scott R. Kempshall , Tina L. Dyer
Abstract: A bag clamp having retention arms, capable of rotating about a pivoting axis between an open and closed position. The retention arms are connected to a locking mechanism configured to prevent the retention arms from pivoting to an open configuration when the locking mechanism is in an engaged setting. The arms are shaped to create an open receiving space. The open receiving space allows the bag clamp to receive a rigid structure to clamp onto while also receiving a bag's straps.
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公开(公告)号：US10448770B1
公开(公告)日：2019-10-22
申请号：US15356077
申请日：2016-11-18
Applicant: Scott R. Kempshall , Tina L. Dyer
Inventor： Scott R. Kempshall , Tina L. Dyer
Abstract: A bag clamp having retention arms, capable of rotating about a pivoting axis between an open and closed position. The retention arms are connected to a locking mechanism configured to prevent the retention arms from pivoting to an open configuration when the locking mechanism is in an engaged setting. The arms are shaped to create an open receiving space. The open receiving space allows the bag clamp to receive a rigid structure to clamp onto while also receiving a bag's straps.
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公开(公告)号：US09526366B1
公开(公告)日：2016-12-27
申请号：US14455016
申请日：2014-08-08
Applicant: Scott R. Kempshall , Tina L. Dyer
Inventor： Scott R. Kempshall , Tina L. Dyer
CPC classification number: A47G29/083 , B65D33/34 , Y10S248/914 , Y10T24/3485 , Y10T24/3488 , Y10T24/3489
Abstract: A bag clamp having at least two coaxial retention arms, capable of rotating about a pivoting axis between an open and closed position. The retention arms are connected to a mechanism housing that has an ability to lock and release the retention arms at various degrees of rotation about the pivoting axis. The arms have a shape such that there are only two possible points of contact between the arms to create an open receiving space. The open receiving space allows the bag clamp to receive a rigid structure to clamp onto while also receiving a bag's straps.
Abstract translation: 具有至少两个同轴保持臂的袋夹具能够在打开和关闭位置之间围绕枢转轴线旋转。 保持臂连接到机构壳体，该机构壳体具有以围绕枢转轴线的不同旋转方向锁定和释放保持臂的能力。 臂具有这样的形状，使得臂之间只有两个可能的接触点以形成开放的接收空间。 打开的接收空间允许袋夹具接收刚性结构以夹持，同时还接收袋子的带子。
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公开(公告)号：US10287000B2
公开(公告)日：2019-05-14
申请号：US14746332
申请日：2015-06-22
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
Abstract: The present invention is a variable geometry aircraft that is capable of morphing its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The aircraft may include variable span, length, and camber. The variability of the structure and the flexible envelope allows the aircraft to adjust its aspect ratio along with the camber of the upper and/or lower surfaces to achieve varying shapes. This transformation changes both the lift and drag characteristics of the craft and may be accomplished while the craft is airborne.
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公开(公告)号：US20160023748A1
公开(公告)日：2016-01-28
申请号：US14341184
申请日：2014-07-25
Applicant: Scott R. Kempshall
Inventor： Scott R. Kempshall
CPC classification number: B64C3/46 , B64B1/08 , B64B1/14 , B64B1/26 , B64B1/58 , B64B2201/00 , B64C3/48 , B64C3/54 , B64C3/546 , B64C2201/022 , B64C2201/101 , B64C2201/105 , F03D1/04 , F03D9/25 , F03D9/32 , F05B2240/921 , Y02E10/725
Abstract: The present invention is a variable geometry lighter-than-air (LTA) aircraft that is adapted to morph its shape from a symmetric cross-section buoyant craft to an asymmetric lifting body and even to a symmetric zero lift configuration. The basic structure is a semi rigid airship with movable longerons. Movement of the longerons adjusts the camber of the upper and/or lower surfaces to achieve varying shapes of the lifting-body. This transformation changes both the lift and drag characteristics of the craft to alter the flight characteristics. The transformation may be accomplished while the craft is airborne and does not require any ground support equipment.
Abstract translation: 本发明是一种可变几何型轻型空中（LTA）飞机，其适于将其形状从对称横截面浮力工艺变形到非对称提升体，甚至变形成对称零升力构造。 基本结构是具有可移动隆起的半刚性飞艇。 仰角的运动调节上表面和/或下表面的弯度，以实现提升体的变化形状。 这种转变改变了飞行器的升力和阻力特性，以改变飞行特性。 转换可以在飞行器机载时完成，并且不需要任何地面支撑设备。
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