Aerial camera system
    1.
    发明授权
    Aerial camera system 有权
    空中摄像系统

    公开(公告)号:US08199197B2

    公开(公告)日:2012-06-12

    申请号:US12390186

    申请日:2009-02-20

    IPC分类号: H04N7/18 H04N9/47

    摘要: An aerial camera system including a plurality of main reels, a camera interface/safety reel and a stabilized camera head. The camera head is supported from main cables from the main reels with a safety reel cable providing power, data and video communication between the camera head and a main computer system. Each of the main reels, the camera interface/safety reel and the camera head are in communication with the main computer system, which controls the feeding and reeling in of the main cables. Further, the computer system controls the feeding and reeling in of the safety reel cable, which typically only follows the camera head as it moves in three-dimensional space, but may in emergency mode support the weight of the camera head and be used to slowly pull the camera head up and out of the way so that it does not interfere with any activity below the flight area. The aerial camera system may also include a level wind assembly that keeps the cables wound on the drum of the main reels and/or the safety reel in a controlled and consistent manner. Furthermore, the camera head of the aerial camera system may use a rotating gimbal assembly with computer controlled leveling motors for keeping the camera head level as the gimbal assembly moves.

    摘要翻译: 一种包括多个主卷轴,相机接口/安全卷轴和稳定的相机头的航空摄像机系统。 相机头由主卷轴的主电缆支撑,安全卷轴电缆提供相机头和主计算机系统之间的电源,数据和视频通信。 主卷轴,相机接口/安全卷轴和摄像头的主体与主计算机系统通信,主控制器控制主电缆的馈送和卷绕。 此外,计算机系统控制安全卷轴电缆的馈送和卷绕,其通常仅在相机头在三维空间中移动时,但可以在紧急模式下支持相机头的重量并用于缓慢 将照相机的头部向上拉出,使其不会干扰飞行区域下方的任何活动。 航空摄像机系统还可以包括水平风组件,其以受控和一致的方式将电缆缠绕在主卷轴和/或安全卷轴的滚筒上。 此外,航空摄像机系统的摄像头可以使用带有计算机控制的调平电动机的旋转万向节组件,以在万向架组件移动时保持摄像机水平。

    AERIAL CAMERA SYSTEM
    3.
    发明申请
    AERIAL CAMERA SYSTEM 有权
    空中相机系统

    公开(公告)号:US20120236148A1

    公开(公告)日:2012-09-20

    申请号:US13472089

    申请日:2012-05-15

    IPC分类号: H04N7/18

    摘要: An aerial camera system including a plurality of main reels, a camera interface/safety reel and a stabilized camera head. The camera head is supported from main cables from the main reels with a safety reel cable providing power, data and video communication between the camera head and a main computer system. Each of the main reels, the camera interface/safety reel and the camera head are in communication with the main computer system, which controls the feeding and reeling in of the main cables. Further, the computer system controls the feeding and reeling in of the safety reel cable, which typically only follows the camera head as it moves in three-dimensional space, but may in emergency mode support the weight of the camera head and be used to slowly pull the camera head up and out of the way so that it does not interfere with any activity below the flight area.

    摘要翻译: 一种包括多个主卷轴,相机接口/安全卷轴和稳定的相机头的航空摄像机系统。 相机头由主卷轴的主电缆支撑,安全卷轴电缆提供相机头和主计算机系统之间的电源,数据和视频通信。 主卷轴,相机接口/安全卷轴和摄像头的主体与主计算机系统通信,主控制器控制主电缆的馈送和卷绕。 此外,计算机系统控制安全卷轴电缆的馈送和卷绕,其通常仅在相机头在三维空间中移动时,但可以在紧急模式下支持相机头的重量并用于缓慢 将照相机的头部向上拉出,使其不会干扰飞行区域下方的任何活动。

    AERIAL CAMERA SYSTEM
    4.
    发明申请
    AERIAL CAMERA SYSTEM 有权
    空中相机系统

    公开(公告)号:US20090207250A1

    公开(公告)日:2009-08-20

    申请号:US12390186

    申请日:2009-02-20

    IPC分类号: H04N7/18 H04N5/225 G12B13/00

    摘要: An aerial camera system including a plurality of main reels, a camera interface/safety reel and a stabilized camera head. The camera head is supported from main cables from the main reels with a safety reel cable providing power, data and video communication between the camera head and a main computer system. Each of the main reels, the camera interface/safety reel and the camera head are in communication with the main computer system, which controls the feeding and reeling in of the main cables. Further, the computer system controls the feeding and reeling in of the safety reel cable, which typically only follows the camera head as it moves in three-dimensional space, but may in emergency mode support the weight of the camera head and be used to slowly pull the camera head up and out of the way so that it does not interfere with any activity below the flight area. The aerial camera system may also include a level wind assembly that keeps the cables wound on the drum of the main reels and/or the safety reel in a controlled and consistent manner. Furthermore, the camera head of the aerial camera system may use a rotating gimbal assembly with computer controlled leveling motors for keeping the camera head level as the gimbal assembly moves.

    摘要翻译: 一种包括多个主卷轴,相机接口/安全卷轴和稳定的相机头的航空摄像机系统。 相机头由主卷轴的主电缆支撑,安全卷轴电缆提供相机头和主计算机系统之间的电源,数据和视频通信。 主卷轴,相机接口/安全卷轴和摄像头的主体与主计算机系统通信,主控制器控制主电缆的馈送和卷绕。 此外,计算机系统控制安全卷轴电缆的馈送和卷绕,其通常仅在相机头在三维空间中移动时,但可以在紧急模式下支持相机头的重量并用于缓慢 将照相机的头部向上拉出,使其不会干扰飞行区域下方的任何活动。 航空摄像机系统还可以包括水平风组件,其以受控和一致的方式将电缆缠绕在主卷轴和/或安全卷轴的滚筒上。 此外,航空摄像机系统的摄像头可以使用带有计算机控制的调平电动机的旋转万向节组件,以在万向架组件移动时保持摄像机水平。

    Fatigue crack-resistant nickel base superalloy composition
    5.
    发明授权
    Fatigue crack-resistant nickel base superalloy composition 失效
    耐疲劳裂纹镍基超合金组成

    公开(公告)号:US5156808A

    公开(公告)日:1992-10-20

    申请号:US576824

    申请日:1990-09-04

    申请人: Michael F. Henry

    发明人: Michael F. Henry

    IPC分类号: C22C19/05

    CPC分类号: C22C19/056 C22C19/057

    摘要: The present invention provides an alloy having improved crack growth inhibition and having high strength at high temperatures. The composition of the alloy is essentially as follows:______________________________________ Ingredient Concentration in Weight % ______________________________________ Ni balance Co 15 Cr 10 Mo 3 Al 3.35 Ti 5.90 Ta 2.70 Nb 1.35 Zr 0.06 V 1 C 0.05 B 0.03. ______________________________________

    摘要翻译: 本发明提供一种具有改善的裂纹扩展抑制并在高温下具有高强度的合金。 合金的组成基本如下: - 重量%的浓度-Ni余量-Co 15 -Cr 10 -Mo 3 -Al 3.35 -Ti 5.90 -Ta 2.70 -Nb 1.35 -Zr 0.06 -V 1 -C 0.05 - B 0.03。 -

    Fatigue crack resistant nickel base superalloys and product formed
    6.
    发明授权
    Fatigue crack resistant nickel base superalloys and product formed 失效
    耐疲劳耐镍镍基合金和产品形成

    公开(公告)号:US5129968A

    公开(公告)日:1992-07-14

    申请号:US250204

    申请日:1988-09-28

    申请人: Michael F. Henry

    发明人: Michael F. Henry

    IPC分类号: C22F1/10 C22C19/05 C22F1/00

    CPC分类号: C22C19/057 C22C19/056

    摘要: The present invention provides an alloy having improved crack growth inhibition and having high strength at high temperatures. The composition of the alloy is essentially as follows:______________________________________ Ingredient Concentration in Weight % ______________________________________ Ni balance Co 15 Cr 10 Mo 3 Al 4.9 Ti 2.0 Ta 4.7 Nb 2.3 Zr 0.06 V 1 C 0.05 B 0.03 ______________________________________

    Fatigue crack resistant astroloy type nickel base superalloys and
product formed
    7.
    发明授权
    Fatigue crack resistant astroloy type nickel base superalloys and product formed 失效
    耐疲劳耐磨类型镍基超级合金和产品形成

    公开(公告)号:US5124123A

    公开(公告)日:1992-06-23

    申请号:US248754

    申请日:1988-09-26

    申请人: Michael F. Henry

    发明人: Michael F. Henry

    IPC分类号: C22F1/10 C22C19/05 C22F1/00

    CPC分类号: C22C19/056

    摘要: The present invention provides an alloy having improved crack growth inhibition and having high strength at high temperatures. The composition of the alloy is essentially as follows:______________________________________ Ingredient Concentration in Weight % ______________________________________ Ni balance Co 10 Cr 15 Mo 4 Al 4 Ti 3.5 Ta 2.5 Nb 1.25 Zr 0.06 C 0.05 B 0.03 ______________________________________

    Fatigue crack resistant IN-100 type nickel base superalloys
    8.
    发明授权
    Fatigue crack resistant IN-100 type nickel base superalloys 失效
    耐疲劳裂纹IN-100型镍基超级合金

    公开(公告)号:US4867812A

    公开(公告)日:1989-09-19

    申请号:US103996

    申请日:1987-10-02

    申请人: Michael F. Henry

    发明人: Michael F. Henry

    IPC分类号: C22C19/05

    CPC分类号: C22C19/056 C22C19/057

    摘要: The present invention provides an alloy having improved crack growth inhibition and having high strength at high temperatures. The composition of the alloy is essentially as follows:______________________________________ Ingredient Concentration in weight % ______________________________________ Ni balance Co 15 Cr 10 Mo 3 Al 4 Ti 3.55 Ta 1.50 Nb 4 Zr 0.06 V 1 C 0.05 B 0.03 ______________________________________

    Method of heat treating .gamma./.gamma.'-.alpha. eutectic nickel-base
superalloy body
    9.
    发明授权
    Method of heat treating .gamma./.gamma.'-.alpha. eutectic nickel-base superalloy body 失效
    热处理方法{65 / {65 {40- {60 {0共晶镍基超级合金体

    公开(公告)号:US4161412A

    公开(公告)日:1979-07-17

    申请号:US854975

    申请日:1977-11-25

    申请人: Michael F. Henry

    发明人: Michael F. Henry

    IPC分类号: C30B33/00 C22F1/10

    CPC分类号: C30B33/00 C30B29/52

    摘要: A method of improving the mechanical properties of a .gamma./.gamma.'-.alpha. eutectic nickel-base superalloy body containing a .gamma.-phase, a .gamma.'-phase, and an aligned molybdenum fiber .alpha.-phase which comprises the steps (a) heating the body to a temperature at which at least a portion of the .gamma.'-phase will transform to a .gamma.-phase, (b) maintaining the heated body at said temperature to allow transformation of at least a portion of said .gamma.'-phase to a .gamma.-phase, and (c) cooling the transformed body to a temperature at which at least a portion of the .gamma.-phase precipitates as a modified .gamma.'-phase.

    摘要翻译: 一种改善包含γ相,γ'相和对准的钼纤维α-相的γ/γ'-α共晶镍基超级合金体的机械性能的方法,其包括以下步骤(a)加热 身体到至少一部分γ'相转变为γ相的温度,(b)将加热的身体保持在所述温度以允许将至少一部分所述γ'相转变为 γ相,和(c)将转化体冷却至至少一部分γ-相析出的温度作为改性γ'相。

    Method for reducing abnormal grain growth in Ni-base superalloys
    10.
    发明授权
    Method for reducing abnormal grain growth in Ni-base superalloys 失效
    减少Ni基超级合金晶粒生长异常的方法

    公开(公告)号:US5556484A

    公开(公告)日:1996-09-17

    申请号:US429506

    申请日:1995-04-26

    IPC分类号: C22F1/10 C23C8/20

    CPC分类号: C22F1/10 C23C8/20

    摘要: A method of forging Ni-base superalloys is described which avoids the growth of abnormally large grains in the surface region of a forged article. The method involves forging and/or annealing a Ni-base superalloy in a carburizing environment. Forging and/or annealing in a carburizing environment is done to maintain the carbon concentration in the surface region at a level that is sufficient to prevent the depletion of carbides and carbonitrides. The carburizing environment may also be selected so that it is non-oxidizing with respect to aluminum, in order to prevent the depletion of aluminum and the reduction of the .gamma.' phase in the surface region.

    摘要翻译: 描述了锻造Ni基超级合金的方法,其避免了锻造制品的表面区域中异常大的颗粒的生长。 该方法包括在渗碳环境中锻造和/或退火Ni基超级合金。 进行渗碳环境中的锻造和/或退火以将表面区域中的碳浓度维持在足以防止碳化物和碳氮化物消耗的水平。 也可以选择渗碳环境使其相对于铝是非氧化的,以便防止铝的消耗和表面区域中的γ'相的减少。