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1. 发明申请

US20150000252A1 ROTATIONAL ANNULAR AIRSCREW WITH INTEGRATED ACOUSTIC ARRESTER 有权
标题翻译：具有集成声学ARRESTER的旋转环形空气
公开(公告)号：US20150000252A1
公开(公告)日：2015-01-01
申请号：US13674377
申请日：2012-11-12
申请人： Matthew D. Moore , Kelly L. Boren
发明人： Matthew D. Moore , Kelly L. Boren
IPC分类号： F02K5/00 , F02K1/44
CPC分类号： F02K5/00 , B64C11/001 , B64C11/18 , F01D1/24 , F01D5/03 , F01D5/225 , F02K1/44 , F02K1/827 , F02K3/062 , F02K3/072 , F04D29/326 , F05D2260/96 , Y02T50/672 , Y02T50/673 , Y10T137/0536
摘要： A propulsion system and methods are presented. A substantially tubular structure comprises a central axis through a longitudinal geometric center, and a first fan rotates around the central axis, and comprises a first fan hub and first fan blades. The fan hub is rotationally coupled to the substantially tubular structure, and the first fan blades are coupled to the first fan hub and increase in chord length with increasing distance from the first fan hub. A second fan is rotationally coupled to the substantially tubular structure and rotates around the central axis and contra-rotates relative to the first fan. Second fan blades are coupled to the second fan hub, and a nacelle circumscribing the first fan and the second fan is coupled to and rotates with the first fan.
摘要翻译：提出了推进系统和方法。基本上管状结构包括通过纵向几何中心的中心轴线，第一风扇围绕中心轴线旋转，并且包括第一风扇轮毂和第一风扇叶片。风扇轮毂旋转地联接到基本上管状的结构，并且第一风扇叶片联接到第一风扇轮毂并随着与第一风扇轮毂的距离增加而增加弦长。第二风扇旋转地联接到基本上管状的结构并围绕中心轴线旋转并相对于第一风扇反转。第二风扇叶片联接到第二风扇轮毂，并且包围第一风扇和第二风扇的机舱联接到第一风扇并与第一风扇一起旋转。

2. 发明申请

US20120119023A1 METHOD AND APPARATUS FOR REDUCING AIRCRAFT NOISE 有权
标题翻译：减少飞机噪音的方法和装置
公开(公告)号：US20120119023A1
公开(公告)日：2012-05-17
申请号：US12946341
申请日：2010-11-15
申请人： Matthew D. Moore , Kelly L. Boren , Justin Lan
发明人： Matthew D. Moore , Kelly L. Boren , Justin Lan
IPC分类号： B64C1/40 , B64D27/12 , B64D27/02
CPC分类号： B64D27/14 , B64D27/20 , B64D2027/005 , B64D2027/026 , Y02T50/66
摘要： An arrangement for an aircraft includes a fuselage, a wing, and a propulsor. The wing may have a wing upper surface, a rear spar and a wing trailing edge. The propulsor may include at least one rotor having a rotor diameter and a rotor axis. The propulsor may be mounted such that the rotor is located longitudinally between the rear spar and the wing trailing edge. The propulsor may also be mounted such that a lowest point of the rotor diameter is located vertically above the wing upper surface.
摘要翻译：飞机的安排包括机身，机翼和推进器。翼可以具有翼上表面，后翼梁和翼后缘。推进器可以包括具有转子直径和转子轴线的至少一个转子。推进器可以被安装成使得转子纵向定位在后翼梁和翼后缘之间。推进器也可以被安装成使得转子直径的最低点位于机翼上表面的垂直上方。

3. 发明授权

US08016233B2 Aircraft configuration 有权
标题翻译：飞机配置
公开(公告)号：US08016233B2
公开(公告)日：2011-09-13
申请号：US11307271
申请日：2006-01-30
申请人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques
发明人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques
IPC分类号： B64C1/00
CPC分类号： B64D27/20 , B64C5/08 , B64C39/12
摘要： An aircraft configuration that may reduce the level of noise, infrared radiation, sonic boom, or combination thereof directed towards the ground from an aircraft in flight. In accordance with an embodiment of the present invention, an aircraft includes a tubular fuselage, two delta wings, at least one engine mounted to the aircraft and higher than the wings, and vertical stabilizers mounted on each wing outboard of the outermost engine. Each wing may include a wing strake at the leading edge of the wing and extending to the fuselage and an aft deck. The leading edge of the wing may extend forward of the intake of the engine, and the trailing edge of the aft deck may extend aft of the engine exhaust. The aft deck may include an upwardly rotatable pitch control surface at the trailing edge of the deck.
摘要翻译：一种飞行器配置，其可以降低来自飞行中的飞行器的噪声，红外辐射，声波起重臂或其组合的指向地面的水平。根据本发明的实施例，飞行器包括管状机身，两个三角翼，至少一个安装在飞行器上并且高于翼的发动机，以及安装在最外侧发动机的每个翼外侧的垂直稳定器。每个机翼可以在翼的前缘处包括翼片，并延伸到机身和后甲板上。机翼的前缘可能会延伸到发动机进气口的前方，后甲板的后缘可能会延伸到发动机排气后面。后甲板可以包括在甲板的后缘处的可向上旋转的俯仰控制表面。

4. 发明申请

US20110167785A1 INTERNAL MIXING OF A PORTION OF FAN EXHAUST FLOW AND FULL CORE EXHAUST FLOW IN AIRCRAFT TURBOFAN ENGINES 有权
标题翻译：风扇排风机内部混合和飞机涡轮发动机全芯排气
公开(公告)号：US20110167785A1
公开(公告)日：2011-07-14
申请号：US12779488
申请日：2010-05-13
申请人： Matthew D. Moore , Edward C. Marques
发明人： Matthew D. Moore , Edward C. Marques
IPC分类号： F02K3/02 , F02K1/34
CPC分类号： F02K3/02 , B64D2033/024 , F02K1/386 , F02K1/48 , F02K1/72 , F02K1/766 , F02K1/827 , F02K3/077 , Y02T50/672
摘要： An airborne mobile platform that has at least one turbofan engine assembly having a fan driven by a core engine, a short nacelle around the fan and a forward portion of the core engine, and a fan exhaust duct through the nacelle. A mixer duct shell is disposed substantially coaxial with and extending forwardly into the fan exhaust duct to provide a mixer duct between the mixer duct shell and a core engine shroud of the core engine. At least a portion of the mixer duct shell has a honeycomb core structure having an inner surface and an outer surface, with an acoustic lining on one of the inner or outer surfaces. The acoustic lining attenuates sound emanating from the turbofan engine assembly.
摘要翻译：一种具有至少一个涡轮风扇发动机组件的机载移动平台，其具有由核心发动机驱动的风扇，围绕风扇的短机舱和核心发动机的前部，以及通过机舱的风扇排气管。混合器管道壳体设置成与风扇排气管道基本同轴并向前延伸，以在混合器管道壳体和核心发动机的核心发动机护罩之间提供混合器管道。混合器管壳的至少一部分具有蜂窝芯结构，其具有内表面和外表面，在内表面或外表面中的一个上具有声衬。声学衬垫减轻了涡扇发动机组件发出的声音。

5. 外观设计

USD622653S1 Aircraft 有权
公开(公告)号：USD622653S1
公开(公告)日：2010-08-31
申请号：US29247058
申请日：2006-05-26
申请人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques
设计人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques

6. 发明授权

US5929339A Method and means for measuring dynamic and static air pressure on a ground surface beneath a lawn mower system 失效
标题翻译：用于测量割草机系统下的地面上的动态和静态空气压力的方法和装置
公开(公告)号：US5929339A
公开(公告)日：1999-07-27
申请号：US30464
申请日：1998-02-25
申请人： Matthew D. Moore , Ambar K. Mitra , J. Adin Mann, III , Jerald Vogel
发明人： Matthew D. Moore , Ambar K. Mitra , J. Adin Mann, III , Jerald Vogel
IPC分类号： G01L15/00 , G01L7/00
CPC分类号： G01L15/00
摘要： A method of measuring dynamic air pressure on a ground surface beneath a lawn mower system which is comprised of a rotatable horizontal blade with a deck unit having a closed top with side walls and an open bottom involves placing the mower on an elevated horizontal platform located in spaced relation to the deck. The blade is then rotated at a speed at which the blade normally would cut grass. Measurements are then made of the air pressure at a plurality of locations adjacent the platform to determine if the air pressure at such locations is such that a blade of grass at each location would be lifted or depressed with respect to the platform. The apparatus for performing the aforesaid method has a horizontal platform with a plurality of apertures therein. The platform is adapted to support a lawn mower deck with a rotatable horizontal blade mounted therein. A plurality of air pressure sensors are mounted in spaced locations on the platform and are located in the lower end of hollow extending tubular pressure taps. The sensors are operatively connected to a monitor to permit the dynamic air pressure to be read adjacent each aperture when a lawn mower with a deck and a rotating blade within the deck is placed on the platform over the apertures.
摘要翻译：一种测量割草机系统下面的地面上的动态空气压力的方法，该方法由具有具有侧壁和敞开底部的封闭顶部的甲板单元的可旋转水平叶片组成，包括将割草机放置在位于与甲板间隔关系。然后以刀片通常切割草的速度旋转叶片。然后测量在靠近平台的多个位置处的空气压力，以确定在这些位置处的空气压力是否使得每个位置处的草叶相对于平台被提升或压下。用于执行上述方法的装置具有在其中具有多个孔的水平平台。该平台适于支撑安装在其中的可旋转水平叶片的割草机甲板。多个空气压力传感器安装在平台上的间隔位置，并且位于中空延伸管状压力抽头的下端。当将具有甲板的草坪割草机和甲板内的旋转叶片放置在平台上的孔上时，传感器可操作地连接到监视器以允许在每个孔附近读取动态空气压力。

7. 发明授权

US08726665B2 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines 有权
标题翻译：在飞机涡扇发动机中内部混合一部分风扇排气流和全排气流
公开(公告)号：US08726665B2
公开(公告)日：2014-05-20
申请号：US12779488
申请日：2010-05-13
申请人： Matthew D. Moore , Edward C. Marques
发明人： Matthew D. Moore , Edward C. Marques
IPC分类号： F02C7/24
CPC分类号： F02K3/02 , B64D2033/024 , F02K1/386 , F02K1/48 , F02K1/72 , F02K1/766 , F02K1/827 , F02K3/077 , Y02T50/672
摘要： An airborne mobile platform that has at least one turbofan engine assembly having a fan driven by a core engine, a short nacelle around the fan and a forward portion of the core engine, and a fan exhaust duct through the nacelle. A mixer duct shell is disposed substantially coaxial with and extending forwardly into the fan exhaust duct to provide a mixer duct between the mixer duct shell and a core engine shroud of the core engine. At least a portion of the mixer duct shell has a honeycomb core structure having an inner surface and an outer surface, with an acoustic lining on one of the inner or outer surfaces. The acoustic lining attenuates sound emanating from the turbofan engine assembly.
摘要翻译：一种具有至少一个涡轮风扇发动机组件的机载移动平台，其具有由核心发动机驱动的风扇，围绕风扇的短机舱和核心发动机的前部，以及通过机舱的风扇排气管。混合器管道壳体设置成与风扇排气管道基本同轴并向前延伸，以在混合器管道壳体和核心发动机的核心发动机护罩之间提供混合器管道。混合器管壳的至少一部分具有蜂窝芯结构，其具有内表面和外表面，在内表面或外表面之一上具有声衬。声学衬垫减轻了涡扇发动机组件发出的声音。

8. 发明授权

US08393567B2 Method and apparatus for reducing aircraft noise 有权
标题翻译：减少飞机噪音的方法和装置
公开(公告)号：US08393567B2
公开(公告)日：2013-03-12
申请号：US12946341
申请日：2010-11-15
申请人： Matthew D. Moore , Kelly L. Boren , Justin Lan
发明人： Matthew D. Moore , Kelly L. Boren , Justin Lan
IPC分类号： B64D27/00
CPC分类号： B64D27/14 , B64D27/20 , B64D2027/005 , B64D2027/026 , Y02T50/66
摘要： An arrangement for an aircraft includes a fuselage, a wing, and a propulsor. The wing may have a wing upper surface, a rear spar and a wing trailing edge. The propulsor may include at least one rotor having a rotor diameter and a rotor axis. The propulsor may be mounted such that the rotor is located longitudinally between the rear spar and the wing trailing edge. The propulsor may also be mounted such that a lowest point of the rotor diameter is located vertically above the wing upper surface.
摘要翻译：飞机的安排包括机身，机翼和推进器。翼可以具有翼上表面，后翼梁和翼后缘。推进器可以包括具有转子直径和转子轴线的至少一个转子。推进器可以被安装成使得转子纵向定位在后翼梁和翼后缘之间。推进器也可以被安装成使得转子直径的最低点位于机翼上表面的垂直上方。

9. 发明申请

US20120091270A1 AIRCRAFT CONFIGURATION 有权
标题翻译：飞机配置
公开(公告)号：US20120091270A1
公开(公告)日：2012-04-19
申请号：US13093596
申请日：2011-04-25
申请人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques , Justin Lan
发明人： Matthew D. Moore , Kelly L. Boren , Edward C. Marques , Justin Lan
IPC分类号： B64C1/40 , F02K1/00 , B23P11/00 , B64C23/00 , B64D29/04
CPC分类号： B64C5/08 , B64C39/12 , B64D27/20
摘要： An aircraft configuration that may reduce the level of roaring jet exhaust noise, infrared radiation, sonic boom, or combination thereof directed towards the ground from an aircraft in flight. The aircraft's nacelles are mounted to the aircraft higher than the wings, with substantially vertical stabilizers outboard of the outermost engine. Noise shifting means are provided such as, for each nacelle, primary chevrons at the core nozzle, secondary chevrons at the fan nozzle, a partial bypass mixer, a long duct full flow mixer, or a combination thereof to provide a shift in spectrum distribution of jet exhaust noise from lower to higher frequency. Variable geometry chevrons may be used with increased immersion to provide such a shift just during noise-restricted portions of an aircraft flight profile. The aircraft aerodynamic structural surfaces serve as noise shielding barriers that more effectively block or redirect the frequency shifted noise up and away from communities.
摘要翻译：一种飞行器配置，其可以降低来自飞行中的飞行器的朝向地面的咆哮的喷气排气噪声，红外辐射，声波起伏或其组合的水平。飞机的发动机舱安装在飞机高于机翼的位置，在最外面的发动机外侧具有大致垂直的稳定器。提供噪声移动装置，例如，对于每个机舱，在核心喷嘴处的主要人字形，在风扇喷嘴处的副人字形，部分旁路混合器，长管道全流量混合器或其组合以提供频谱分布的偏移喷气排气噪声从低频到高频。可变几何人字形可以与增加的浸入使用，以在飞机飞行剖面的噪声限制部分期间提供这种移动。飞机空气动力学结构表面用作噪声屏蔽屏障，可以更有效地阻挡或重定向频率偏移的噪声向上和远离社区。

10. 发明申请

US20110167786A1 INTERNAL MIXING OF A PORTION OF FAN EXHAUST FLOW AND FULL CORE EXHAUST FLOW IN AIRCRAFT TURBOFAN ENGINES 有权
标题翻译：风扇排风机内部混合和飞机涡轮发动机全芯排气
公开(公告)号：US20110167786A1
公开(公告)日：2011-07-14
申请号：US12779517
申请日：2010-05-13
申请人： Edward C. Marques , Matthew D. Moore
发明人： Edward C. Marques , Matthew D. Moore
IPC分类号： F02K3/02 , F02K1/34
CPC分类号： F02K1/386 , B64D2033/024 , F02K1/48 , F02K1/72 , F02K1/766 , F02K3/077 , Y02T50/672
摘要： An integrated, single piece mixer-center body ventilation apparatus is disclosed for use with a turbofan jet engine. The apparatus may incorporate a circumferential forward body portion adapted to be coupled to an aft end of a core engine turbine case of the jet engine, and a center body tube portion integrally formed with the forward body portion and having an axially opening vent exit. The forward body portion may have a plurality of inner mixer flow paths in communication with scalloped projecting portions. The inner mixer flow paths direct a pressurized core exhaust flow through the mixer device and mix the pressurized core exhaust flow with a portion of a pressurized fan exhaust flow, to thus significantly cool the pressurized core exhaust flow.
摘要翻译：公开了一种用于涡轮风扇喷气发动机的集成的单件混合器 - 中心体通气装置。该装置可以包括适于联接到喷气发动机的核心发动机涡轮机壳体的后端的周向前部主体部分和与前部主体部分一体形成并具有轴向开口排气口的中心主体管部分。前身部分可以具有与扇形突出部分连通的多个内部混合器流动路径。内部混合器流动路径将加压的核心排气流引导通过混合器装置，并将加压的核心排气流与加压的风扇排气流的一部分混合，从而显着地冷却加压的核心排气流。

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