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2. 发明授权

US06857598B2 Integrated high-speed aircraft and associated methods of manufacture 有权
标题翻译：集成高速飞机及相关制造方法
公开(公告)号：US06857598B2
公开(公告)日：2005-02-22
申请号：US10683671
申请日：2003-10-09
申请人： Eric E. Adamson , Paul W. Dees , Edward W. Gronenthal , Walter H. Howard, Jr. , Chester P. Nelson , Mithra M. Sankrithi , Gerhard E. Seidel , V. Kenneth Stuhr
发明人： Eric E. Adamson , Paul W. Dees , Edward W. Gronenthal , Walter H. Howard, Jr. , Chester P. Nelson , Mithra M. Sankrithi , Gerhard E. Seidel , V. Kenneth Stuhr
IPC分类号： B64C1/00 , B64C1/26 , B64C25/04 , B64C25/10 , B64C30/00 , B64D9/00 , B64D11/00 , B64D27/18 , B64D37/04 , B64D27/16
CPC分类号： B64C1/0009 , B64C1/26 , B64C25/04 , B64C25/10 , B64C30/00 , B64C2001/0027 , B64C2001/0045 , B64D9/003 , B64D11/00 , B64D27/18 , B64D37/04 , Y02T50/12 , Y02T50/44 , Y02T50/46
摘要： Integrated high-speed aircraft, such as high-speed transport aircraft, and associated methods of manufacture. In one embodiment, a high-speed transport aircraft includes a fuselage having a first fuselage portion and a second fuselage portion positioned aft of the first fuselage portion. The first fuselage portion can have a first cross-sectional area and the second fuselage portion can have a second cross-sectional area that is less than the first cross-sectional area. The high-speed transport aircraft can further include a wing and a propulsion system. The wing can extend outwardly from the fuselage at least proximate to the second fuselage portion and can include a leading edge region and a trailing edge region. The propulsion system can include an engine nacelle fixedly attached to the wing and laterally aligned with the second fuselage portion. In one aspect of this embodiment, the engine nacelle can include an air inlet positioned aft of the leading edge region of the wing and an exhaust gas outlet positioned aft of the trailing edge region of the wing.
摘要翻译：集成高速飞机，如高速运输飞机及相关制造方法。在一个实施例中，高速运输飞机包括具有第一机身部分的机身和位于第一机身部分后方的第二机身部分。第一机身部分可以具有第一横截面积，并且第二机身部分可以具有小于第一横截面积的第二横截面面积。高速运输机可以进一步包括机翼和推进系统。机翼可以从机身至少靠近第二机身部分向外延伸，并且可以包括前缘区域和后缘区域。推进系统可以包括固定地附接到机翼并与第二机身部分横向对齐的发动机机舱。在该实施例的一个方面，发动机舱可以包括位于翼的前缘区域后方的空气入口和位于翼的后缘区域后方的排气出口。

3. 外观设计

USD477561S1 Supersonic aircraft 失效
公开(公告)号：USD477561S1
公开(公告)日：2003-07-22
申请号：US29155232
申请日：2002-02-05
申请人： Chester P. Nelson
设计人： Chester P. Nelson

4. 外观设计

USD479501S1 High-speed aircraft 失效
标题翻译：高速飞机
公开(公告)号：USD479501S1
公开(公告)日：2003-09-09
申请号：US29168026
申请日：2002-09-24
申请人： Chester P. Nelson
设计人： Chester P. Nelson

5. 发明授权

US06575406B2 Integrated and/or modular high-speed aircraft 失效
公开(公告)号：US06575406B2
公开(公告)日：2003-06-10
申请号：US09815390
申请日：2001-03-22
申请人： Chester P. Nelson
发明人： Chester P. Nelson
IPC分类号： B64C100
CPC分类号： B64C1/0009 , B64C1/26 , B64C3/10 , B64C3/32 , B64C30/00 , B64C39/12 , B64C2001/0045 , B64C2211/00 , B64D27/18 , B64D29/02 , B64D2033/026 , Y02T50/12 , Y02T50/44
摘要： An integrated and/or modular high-speed aircraft and method of design and manufacture. The aircraft can have a supersonic or near-sonic cruise Mach number. In one embodiment, the aircraft can include an aft body integrated with a delta wing and a rearwardly tapering fuselage to define a smooth forward-to-rear area distribution. A propulsion system, including an engine, inlet, and exhaust nozzle can be integrated into the aft body to be at least partially hidden behind the wing. In one embodiment, the entrance of the inlet can be positioned beneath the wing, and the exit of the nozzle can be positioned at or above the wing. An S-shaped inlet duct can deliver air to the aft-mounted, integrated engine. The aircraft can include aft-mounted elevators, wing-mounted elevons, and forward-mounted canards for pitch control. The construction of the aircraft can be modular to take advantage of commonalties between near-sonic and supersonic structures.

7. 发明授权

US06938854B2 Integrated and/or modular high-speed aircraft 有权
标题翻译：集成和/或模块化高速飞机
公开(公告)号：US06938854B2
公开(公告)日：2005-09-06
申请号：US10394550
申请日：2003-03-21
申请人： Chester P. Nelson
发明人： Chester P. Nelson
IPC分类号： B64C7/00 , B64C1/00 , B64C1/26 , B64C3/10 , B64C3/32 , B64C30/00 , B64C39/12 , B64D27/02 , B64D27/18 , B64D29/02 , B64D27/00
CPC分类号： B64C1/0009 , B64C1/26 , B64C3/10 , B64C3/32 , B64C30/00 , B64C39/12 , B64C2001/0045 , B64C2211/00 , B64D27/18 , B64D29/02 , B64D2033/026 , Y02T50/12 , Y02T50/44
摘要： An integrated and/or modular high-speed aircraft and method of design and manufacture. The aircraft can have a supersonic or near-sonic cruise Mach number. In one embodiment, the aircraft can include an aft body integrated with a delta wing and a rearwardly tapering fuselage to define a smooth forward-to-rear area distribution. A propulsion system, including an engine, inlet, and exhaust nozzle can be integrated into the aft body to be at least partially hidden behind the wing. In one embodiment, the entrance of the inlet can be positioned beneath the wing, and the exit of the nozzle can be positioned at or above the wing. An S-shaped inlet duct can deliver air to the aft-mounted, integrated engine. The aircraft can include aft-mounted elevators, wing-mounted elevons, and forward-mounted canards for pitch control. The construction of the aircraft can be modular to take advantage of commonalties between near-sonic and supersonic structures.
摘要翻译：集成和/或模块化高速飞机及其设计和制造方法。飞机可以有超音速或近声波巡航马赫数。在一个实施例中，飞机可以包括与三角翼和向后渐缩的机身一体化的后体，以限定顺利的前后区域分布。包括发动机，入口和排气喷嘴的推进系统可以集成到后体中至少部分地隐藏在机翼后面。在一个实施例中，入口的入口可以定位在机翼的下方，并且喷嘴的出口可以定位在机翼处或上方。 S形入口管道可以将空气输送到后部安装的集成发动机。飞机可以包括安装在后面的电梯，机翼安装的电梯和用于俯仰控制的前置安装的卡车。飞机的构造可以是模块化的，以利用近声和超音速结构之间的共同点。

8. 发明授权

US06929216B2 Method and apparatus for installing and actuating movable airfoils, including canards 失效
标题翻译：用于安装和致动可移动翼片（包括挡板）的方法和装置
公开(公告)号：US06929216B2
公开(公告)日：2005-08-16
申请号：US10689972
申请日：2003-10-20
申请人： David L. Bath , Salvatore Carta , Kelly T. Jones , Brian J. Kramer , Chester P. Nelson , Pieter S. Penhall , Joseph R. Pineda , Andrew Sheppard
发明人： David L. Bath , Salvatore Carta , Kelly T. Jones , Brian J. Kramer , Chester P. Nelson , Pieter S. Penhall , Joseph R. Pineda , Andrew Sheppard
IPC分类号： B64C1/00 , B64C1/26 , B64C3/38 , B64C5/04 , B64C5/12 , B64C5/16 , B64C9/02 , B64C13/00 , B64C13/30 , B64C13/32 , B64C39/12 , F16C19/50
CPC分类号： F16C19/50 , B64C1/26 , B64C3/38 , B64C3/385 , B64C5/04 , B64C5/16 , B64C9/02 , B64C13/30 , B64C13/32 , B64C39/12 , F16C2326/43 , Y02T50/44 , Y10T29/49545 , Y10T29/49638 , Y10T29/49643 , Y10T29/4973
摘要： Methods and apparatuses for installing and actuating movable airfoils, such as canards. A canard in one embodiment of the invention includes an airfoil positioned external to an aircraft fuselage. The airfoil can include a first portion and a second portion (such as a flight control surface) movable relative to the first portion. A connecting portion depends from the airfoil portion and has an attachment portion configured to attach to an aircraft internal to the aircraft fuselage. A connecting portion can include first and second load paths to carry corresponding first and second load portions between the airfoil portion and the attachment portion. The connecting portion can be rotatable about a rotation axis positioned between the first and second loads paths. Accordingly, the connecting portion can be relatively compact so as to reduce the impact of the connecting portion and the volume of the fuselage.
摘要翻译：用于安装和致动可移动翼型件的方法和装置，例如卡车。在本发明的一个实施例中的鸭子包括位于飞机机身外部的翼型件。翼型件可以包括可相对于第一部分移动的第一部分和第二部分（例如飞行控制表面）。连接部分从翼型件部分中取出并且具有被配置为附接到飞行器机身内部的飞行器的附接部分。连接部分可以包括第一和第二负载路径，以在机翼部分和附接部分之间承载对应的第一和第二负载部分。连接部分可以围绕位于第一和第二负载路径之间的旋转轴线旋转。因此，连接部分可以相对紧凑，以减少连接部分的冲击和机身的体积。

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