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1. 发明授权

US5941478A STOL/VTOL free wing aircraft with modular wing and tail 失效
标题翻译： STOL / VTOL自由翼飞机与模块化翼和尾巴
公开(公告)号：US5941478A
公开(公告)日：1999-08-24
申请号：US66980
申请日：1998-04-28
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C1/00 , B64C3/38 , B64C29/00 , B64C39/02 , B64C39/04
CPC分类号： B64C39/04 , B64C1/00 , B64C29/0033 , B64C3/385 , B64C39/024 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/127 , B64C2201/165 , B64C2201/187
摘要： A mechanism for quickly removing and installing the free wings and/or the tail booms of a freewing aircraft to the fuselage. The fuselage includes a free wing cross tube extending transversely through the fuselage at the spanwise axis, and each of the left and right free wings includes a support tube disposed therein, also along the spanwise axis, with a portion of the wing structural tube being received within the fuselage cross tube. A quick-release pin is insertable in holes disposed in both the structural tube and the cross tube when the holes are placed in alignment. A second cross tube extends transversely through the rear end of the fuselage at the tail boom pivot axis. At least a portion of each tail boom member is disposed in surrounding relationship to the cross tube. In a preferred embodiment, a quick-release pin is insertable in holes disposed in both the tail boom member portion and the cross tube when the holes are placed in alignment.
摘要翻译：用于快速拆卸和安装自由翼的自由翼和/或尾翼到机身的机构。该机身包括横跨翼展横向穿过机身的自由翼横管，并且左右自由翼中的每一个还包括沿着翼展方向轴线设置在其中的支撑管，翼结构管的一部分被接收在机身横管内。当孔对准时，快速释放销可插入设置在结构管和横管中的孔中。第二横管在尾臂枢轴上横向延伸穿过机身的后端。每个尾臂构件的至少一部分设置成与横管的关系。在优选实施例中，当孔对准时，快速释放销可插入设置在尾梁构件部分和横管中的孔中。

2. 发明授权

US5560568A Recovery system and method for capturing and securing an air vehicle to landing platform 失效
标题翻译：用于捕获和固定飞机到达平台的恢复系统和方法
公开(公告)号：US5560568A
公开(公告)日：1996-10-01
申请号：US261901
申请日：1994-06-15
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38 , B64C29/00 , B64C29/02 , B64C39/02 , B64C39/04
CPC分类号： B64C29/02 , B64C29/0033 , B64C3/385 , B64C39/024 , B64C39/04 , B64C2201/044 , B64C2201/046 , B64C2201/084 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/187 , B64D2201/00 , Y10S446/901
摘要： Apparatus and method for recovering and arresting an aircraft on a floating platform is disclosed. The aircraft has a fuselage, a wing, and a source of propulsion for propelling the aircraft in flight. During landing approach, an inflatable cushion attached to the fuselage is deployed below the fuselage via inflation. In the inflated condition, a fastening material disposed on a downward facing surface of the cushion is thereby adapted to adhesively contact the floating platform deck so that the forward motion of the aircraft is slowed and arrested. In the preferred embodiment, the fastening material is one of male or female VELCRO.RTM. which is adapted to mate with corresponding VELCRO.RTM. material covering the platform deck.
摘要翻译：公开了一种用于在浮动平台上恢复和拦截飞行器的装置和方法。这架飞机有一个机身，一个机翼和一个推进的来源，用于在飞行中推进飞机。在着陆过程中，通过充气将附着在机身上的充气垫部署在机身的下方。在充气状态下，设置在缓冲垫的向下的表面上的紧固材料因此适于与浮动平台甲板粘合地接触，使得飞行器的向前运动变慢并且被阻止。在优选实施例中，紧固材料是男性或女性VELCRO TM之一，其适于与覆盖平台甲板的相应的VELCRO TM材料配合。

3. 发明授权

US5509623A Free wing aircraft having a free wing used as an air brake to shorten roll-out following touchdown 失效
标题翻译：具有自由翼的自由翼飞机用作空气制动器，以在触地之后缩短推出
公开(公告)号：US5509623A
公开(公告)日：1996-04-23
申请号：US261902
申请日：1994-06-15
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38
CPC分类号： B64C3/385
摘要： A free wing aircraft including a free wing pivotally supported about a spanwise axis for flight in a free wing mode of operation with respect to the fuselage is disclosed. The free wing is capable of being deflected into a nose down configuration sufficient to create an aerodynamic braking effect to decrease air speed after landing upon roll-out. This aerodynamic braking effect can also be sufficient to create negative lift that plants the aircraft firmly down, increasing the coefficient of friction and allowing the aircraft brakes to be more effective relative to a fixed wing aircraft at touchdown.
摘要翻译：公开了一种自由翼飞机，其包括围绕翼展方向轴线枢转地支撑的自由翼，用于以相对于机身的自由翼操作模式飞行。自由翼能够被偏转到足以产生空气动力学制动效果的下降构型，以降低在推出之后着陆时的空气速度。这种空气动力学制动效果也可以足以产生使飞机稳固地下降的负升力，增加摩擦系数，并允许飞机制动器在触地时相对于固定翼飞机更有效。

4. 发明授权

US5340057A Thrust vectoring free wing aircraft 失效
标题翻译：推力矢量自由翼飞机
公开(公告)号：US5340057A
公开(公告)日：1994-08-23
申请号：US850913
申请日：1992-03-13
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38 , B64C29/00 , B64C29/02 , B64C39/02 , B64C39/04
CPC分类号： B64C39/024 , B64C29/0033 , B64C29/02 , B64C3/385 , B64C39/04 , B64C2201/044 , B64C2201/046 , B64C2201/084 , B64C2201/088 , B64C2201/104 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64D2201/00
摘要： The VTOL aircraft includes a free wing having wings on opposite sides of the fuselage connected to one another for joint free rotation and for differential pitch settings under pilot, computer or remote control. On vertical launch, pitch, yaw and roll control is effected by the elevators, rudder and the differential pitch settings of the wings, respectively. At launch, the elevator pitches the fuselage nose downwardly to alter the thrust vector and provide horizontal speed to the aircraft whereby the free wing freely rotates relative to the fuselage into a generally horizontal orientation to provide lift during horizontal flight. Transition from horizontal to vertical flight is achieved by the reverse process and tile aircraft may be gently recovered in or on a resilient surface such as a net.
摘要翻译：垂直起落架飞机包括一个自由翼，在机身的相对两侧具有彼此连接的翼，用于联合自由旋转，并在飞行员，计算机或遥控器下进行差距俯仰设置。在垂直发射时，俯仰，偏航和侧倾控制分别由电梯，方向舵和翼的差距俯仰设置来实现。在发射时，升降机将机身鼻部向下倾斜以改变推力矢量并向飞行器提供水平速度，由此自由翼相对于机身自由旋转成大致水平的方向以在水平飞行期间提供升力。从水平飞行到垂直飞行的过渡是通过相反的过程实现的，瓦片飞机可以在诸如网络的弹性表面中或其上轻轻地回收。

5. 发明授权

US5863013A STOL/VTOL free wing aircraft with improved shock dampening and absorbing means 失效
标题翻译： STOL / VTOL自由翼飞机具有改进的减震和吸收手段
公开(公告)号：US5863013A
公开(公告)日：1999-01-26
申请号：US467107
申请日：1995-06-06
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38 , B64C29/00 , B64C39/02 , B64C39/04
CPC分类号： B64C39/04 , B64C29/0033 , B64C3/385 , B64C39/024 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/146 , B64C2201/165 , B64C2201/187
摘要： An improved VTOL/STOL free wing aircraft providing damping and absorption of shock landing loads upon landing. A pair of resilient struts is provided, projecting forwardly from the trailing edge of either side of the fuselage when the fuselage is tilted. Preferably, the aircraft includes a pair of articulated tail booms, the strut being a portion of the tail boom extending forward from the pivot axis of the tail boom. Landing wheels are disposed on the strut in tandem spaced relationship. The resiliency of the strut causes the strut to act as a leaf spring and thus dampen shock landing loads. Operatively secured to the bottom surface of the fixed wing portions and the forward portion of the landing gear struts is a pair of dashpots for absorbing the shock landing loads.
摘要翻译：改进的VTOL / STOL自由翼飞机在着陆时提供减震和吸收冲击着陆载荷。当机身倾斜时，提供一对弹性支柱，从机身任一侧的后缘向前突出。优选地，飞行器包括一对铰接的尾臂，支柱是从尾臂的枢转轴线向前延伸的尾臂的一部分。着陆轮以串联间隔的关系设置在支柱上。支柱的弹性导致支柱作为板簧，从而抑制冲击着陆载荷。操作地固定到固定翼部分的底表面和起落架支柱的前部是用于吸收冲击着陆载荷的一对减震器。

6. 发明授权

US5765777A STOL/VTOL free wing aircraft with variable pitch propulsion means 失效
标题翻译：具有变桨距推进装置的STOL / VTOL自由翼飞机
公开(公告)号：US5765777A
公开(公告)日：1998-06-16
申请号：US468397
申请日：1995-06-06
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38 , B64C29/00 , B64C39/02 , B64C39/04 , B64C3/42 , B64C27/28 , B64C27/52
CPC分类号： B64C3/385 , B64C29/0033 , B64C39/024 , B64C39/04 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/146 , B64C2201/165 , B64C2201/187
摘要： A VTOL/STOL free wing aircraft includes a free wing having wings on opposite sides of a fuselage connected to one another respectively for free rotation about a spanwise access. Improved control upon landing of the aircraft is achieved by utilizing a variable pitch propulsion system, enabling the pitch of the propeller to be varied corresponding to the speed of the aircraft and angle of approach upon descent.
摘要翻译：一架VTOL / STOL自由翼飞机包括一个自由翼，在机身的相对两侧分别连接一个翅膀，分别用于围绕翼展向的自由旋转。通过利用可变桨距推进系统来实现对飞机着陆的改进的控制，使得能够根据飞行器的速度和下降时的接近角来改变螺旋桨的桨距。

7. 发明授权

US5280863A Lockable free wing aircraft 失效
标题翻译：可锁定的自由翼飞机
公开(公告)号：US5280863A
公开(公告)日：1994-01-25
申请号：US795329
申请日：1991-11-20
申请人： Hugh Schmittle
发明人： Hugh Schmittle
IPC分类号： B64C3/38 , B64C29/00 , B64C29/02 , B64C39/02 , B64C39/04
CPC分类号： B64C39/04 , B64C29/0033 , B64C29/02 , B64C3/385 , B64C39/024
摘要： The aircraft includes a free wing freely pivotally supported about a spanwise axis for flight in a free wing mode and lockable in selected predetermined, fixed angles of incidence with respect to a fuselage for flight in a fixed wing mode. The predetermined angle of incidence in the fixed wing flight mode is selected to provide sufficient lift for flying the aircraft at low speeds as necessary for takeoff and landing. The aircraft can be converted in flight between the free wing or conventional fixed wing aircraft flight modes. A control system is provided for selectively enabling or disabling the elevators on the horizontal stabilizer and the wing flaps.
摘要翻译：该飞行器包括一个自由枢转地支撑在翼展方向轴上的自由翼，用于以自由翼模式飞行，并以相对于机身在固定翼模式中飞行的选定的预定的固定入射角被锁定。选择固定翼飞行模式中的预定入射角，以提供足够的升降机，以便起飞和着陆所需的低速飞行飞机。飞机可以在自由翼或常规固定翼飞行器飞行模式之间飞行转换。提供一种控制系统，用于选择性地启用或禁用水平稳定器和翼襟翼上的电梯。

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