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61. 发明授权

US3756546A Aircrew escape system 失效
标题翻译： AIRCREW ESCAPE系统
公开(公告)号：US3756546A
公开(公告)日：1973-09-04
申请号：US3756546D
申请日：1971-11-23
申请人： US NAVY
发明人： CARSON R , LYONS J
IPC分类号： B64D25/12
CPC分类号： B64D25/12 , Y10S244/902 , Y10S244/903
摘要： An aircrew escape system comprising a capsule adapted to contain a crewmember, having attached thereto a deployable parawing controllable by the crewmember, and a deployable tractor rocket connected to the top of the capsule by a length of tow rope. Contained within the capsule is a control unit by which the crewmember, once in position, initiates the burn of the tractor rocket, initiating separation of the capsule from the aircraft and through which the crewmember can control the jettisoning of the tractor rocket and the ignition of an air-breathing powerplant mounted on the capsule. The parawing, in its deployed state, is aligned at an angle of attack relative the longitudinal axis of the capsule by preselected lengths of supporting shrouds having control shrouds attached to the trailing edge thereof terminating at a control stick in the capsule. Accordingly, when the capsule is accelerated by the tractor rocket to a velocity where the lift force of the parawing substantially balances the weight of the capsule the tractor rocket is released, the powerplant is started and the capsule is in position for controlled horizontal flight.
摘要翻译：一种空勤逃生系统，其包括适于容纳机组成员的胶囊，其附接有可由机组成员控制的可展开的解剖，以及可伸展的拖拉机火箭，其通过一定长度的牵引绳连接到胶囊的顶部。包含在胶囊内的是控制单元，通过该控制单元，机组成员一旦处于适当位置，启动拖拉机火箭的燃烧，启动胶囊与飞机的分离，并且机组成员可以通过该单元控制拖拉机火箭的放弃和点火安装在胶囊上的呼吸呼吸动力装置。处于其展开状态的解剖通过预选长度的支撑罩以相对于胶囊的纵向轴线的迎角对准，其具有附接到其后缘的控制罩，其终止于胶囊中的控制棒。因此，当胶囊被拖拉机火箭加速到速度时，其中解压的提升力基本上平衡了释放拖拉机火箭的胶囊的重量，起动动力装置并且胶囊处于适当位置以进行受控的水平飞行。

62. 发明授权

US3135483A Auxiliary boom control system for rogallo type wing aircraft 失效
标题翻译：罗格罗型翼型飞机辅助吊杆控制系统
公开(公告)号：US3135483A
公开(公告)日：1964-06-02
申请号：US21801862
申请日：1962-08-20
申请人： RYAN AERONAUTICAL CO
发明人： GIRARD PETER F
IPC分类号： B64C31/032
CPC分类号： B64C31/032 , Y10S244/901 , Y10S244/903

63. 发明授权

US2623712A Airplane with pivotally mounted sustaining wing 失效
标题翻译：飞机与枢轴安装的维持翼
公开(公告)号：US2623712A
公开(公告)日：1952-12-30
申请号：US69850346
申请日：1946-09-21
申请人： SPRATT GEORGE G
发明人： SPRATT GEORGE G
IPC分类号： B64C3/38
CPC分类号： B64C3/385 , Y10S244/903 , Y10S244/904

64. 发明授权

US2166259A Shaft bearing 失效
公开(公告)号：US2166259A
公开(公告)日：1939-07-18
申请号：US18484938
申请日：1938-01-13
申请人： FEDERAL MOGUL CORP
发明人： MEYER THEODORE F W
IPC分类号： F16C27/06 , F16F1/38
CPC分类号： F16F1/38 , F16C27/063 , Y10S244/903

65. 发明授权

US1856306A Aviation training apparatus 失效
标题翻译：航空培训仪器
公开(公告)号：US1856306A
公开(公告)日：1932-05-03
申请号：US46587430
申请日：1930-07-07
申请人： CYCLOPLANE COMPANY LTD
发明人： WOODSON OMER L , MYHRES HARRY S
IPC分类号： G09B9/12
CPC分类号： G09B9/12 , Y10S244/903

66. 发明授权

US1081420A Aeroplane. 失效
公开(公告)号：US1081420A
公开(公告)日：1913-12-16
申请号：US1912711074
申请日：1912-07-23
申请人： ALEXANDER JOSEPH E G
发明人： ALEXANDER JOSEPH E G
CPC分类号： B64C39/08 , Y10S244/903 , Y10S244/904

67. 发明授权

US06688553B2 Inflatable airfoils, and elevated and propulsion driven vehicles 失效
标题翻译：充气翼型，高架和推进驱动的车辆
公开(公告)号：US06688553B2
公开(公告)日：2004-02-10
申请号：US10200348
申请日：2002-07-23
申请人： Chih-Yu Hsia
发明人： Chih-Yu Hsia
IPC分类号： B64C330
CPC分类号： B64C3/30 , B64B2201/00 , Y10S244/903
摘要： An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.
摘要翻译：一种航空装置，该组合包括具有至少一个面板的主要翼型件，其具有上板，下板和与翼型件相关的并且纵向延伸的多个气体，所述管包括相对较大的横截面管，并且相对较小的横截面定位器被定位成稳定相对较大的横截面管。

68. 发明申请

US20030127567A1 Inflatable airfoils, and elevated and propulsion driven vehicles 失效
公开(公告)号：US20030127567A1
公开(公告)日：2003-07-10
申请号：US10200456
申请日：2002-07-23
发明人： Chih-Yu Hsia
IPC分类号： B64G001/62
CPC分类号： B64C3/30 , B64B2201/00 , B64C31/028 , B64C31/04 , Y10S244/903
摘要： An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.

69. 发明申请

US20020190157A1 Small-sized radio-controlled flying device 失效
标题翻译：小型无线电遥控飞行装置
公开(公告)号：US20020190157A1
公开(公告)日：2002-12-19
申请号：US10168588
申请日：2002-06-24
发明人： Jean Asseline , George De Noni
IPC分类号： B64C001/00 , B64C003/00 , B64C005/00 , B64C007/00
CPC分类号： A63H27/08 , A63H30/04 , B64C2201/086 , B64C2201/105 , B64C2201/107 , B64C2201/127 , B64C2201/165 , B64C2201/187 , Y10S244/902 , Y10S244/903
摘要： This invention relates to a small-sized radio controlled flying device propelled by a thermal engine (20) with pusher type airscrew (19) for remote sensing, said device enabling short take-off and landing and flying at maximum speed of 35 Km/h. The device comprises a pod and wings, the pod (1) being a rigid tricycle carriage dismountable by disengagement of substantially pyramidal jig with rear base (2) and front apex (7), lower plane (3), two lateral planes (4, 5) and an upper plane (6), the base being a welded one-piece element and comprising the engine, the airscrew, a tank and the radio control, the apex being a welded one-piece element, the lower plane and the two lateral planes comprising spars (11, 12) at least assembled at the base and at the apex, the lower plane comprising at its three end angles two rear wheels (8) and a front wheel (9), the front wheel being provided to protrude towards the front in the apex and the wheels being low pressure tires, the wings (13) being a caisson-type supple parachute, said wings being connected to the pod in an adjustable fashion by two front slings (17), two braking slings (18) acting on the two flaps/ailerons.
摘要翻译：本发明涉及一种由具有用于遥感的推进式螺旋桨（19）的热引擎（20）推进的小型无线电控制飞行装置，所述装置能够以35Km / h的最大速度进行短时起飞和着陆和飞行。该装置包括荚和翼，所述荚（1）是刚性三轮车，通过基本上棱锥形的夹具与后基部（2）和前顶点（7），下平面（3），两个侧平面（4， 5）和上平面（6），底座是焊接的整体元件，包括发动机，螺旋桨，水箱和无线电控制器，顶点是焊接的一体元件，下平面和两个包括至少在基部和顶点处组装的翼梁（11,12）的横向平面，所述下平面在其三个端角处包括两个后轮（8）和前轮（9），所述前轮设置成突出朝向顶端的前部并且车轮是低压轮胎，翼（13）是沉箱式柔软的降落伞，所述翼以可调节的方式通过两个前吊索（17），两个制动吊索（ 18）作用于两个翼片/副翼。

70. 发明申请

US20020084386A1 Inflatable airfoils, and elevated and propulsion driven vehicles 失效
公开(公告)号：US20020084386A1
公开(公告)日：2002-07-04
申请号：US10035856
申请日：2002-01-04
发明人： Chih-Yu Hsia
IPC分类号： B64G001/62
CPC分类号： B64C3/30 , B64B2201/00 , B64C31/028 , B64C31/04 , Y10S244/903
摘要： An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.

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