专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

91. 发明专利

ES2438009B1 Alas de avión con tubos estabilizadores 未知
公开(公告)号：ES2438009B1
公开(公告)日：2014-10-28
申请号：ES201200764
申请日：2012-07-12
申请人： PORRAS VILA F JAVIER
发明人： PORRAS VILA F JAVIER
IPC分类号： B64C3/16 , B64C39/08

92. 发明专利

CA2909530A1 BRAIDED COMPOSITE SPAR 未知
公开(公告)号：CA2909530A1
公开(公告)日：2014-10-23
申请号：CA2909530
申请日：2014-04-17
申请人： AIRBUS OPERATIONS LTD
发明人： FONG TONY , AXFORD TIMOTHY
IPC分类号： B29C70/22 , B64C3/16 , B64C23/06
摘要： A braided composite spar or preform for a braided composite spar with a plurality of tubular plies of braided fibres. Each ply has a first set of fibres which wind in a clockwise direction in a first series of turns with a pitch between each adjacent pair of turns, and a second set of fibres which wind in an anti-clockwise direction in a second series of turns with a pitch between each adjacent pair of turns. The first and second sets of fibres in each ply are intertwined to form a braided structure. The spar or preform extends lengthwise from a root to a tip and has a tapered portion which tapers inwardly towards the tip. Each ply has a circumference in the tapered portion which reduces as it tapers inwardly. For at least one of the plies the pitches of the first and second sets of fibres increase continuously as the ply tapers inwardly in the tapered portion. The spar or preform can be used to provide a tubular main spar for a winglet. The winglet also has a front spar with a front spar web, an upper front spar cap, and a lower front spar cap. An upper skin of the winglet is joined to the braided spar and the upper front spar cap. A lower skin of the winglet is joined to the braided spar and the lower front spar cap.

93. 发明专利

ES2448817A2 Hélices de helicóptero y de avión, con grupos de aletas 未知
公开(公告)号：ES2448817A2
公开(公告)日：2014-03-17
申请号：ES201200934
申请日：2012-09-17
申请人： PORRAS VILA FO JAVIER
发明人： PORRAS VILA FO JAVIER
IPC分类号： B64C11/00 , B64C3/16 , B64C39/08
摘要： Las hélices de helicóptero y de avión con grupos de aletas, son el mecanismo de de avance de una aeronave, que presenta la novedad de añadir un grupo de aletas (9) en los extremos de las palas de las hélices (8) para producir un empuje doble. Las palas de las hélices (8) de un helicóptero (10) empujan el aire hacia abajo, mientras que los grupos de aletas (9), -que forman un cierto ángulo respecto de su plano de giro, tal como lo hacen las alas (2) de los aviones-, lo empujan en horizontal y crean un gran momento de fuerza que hace que el helicóptero (10) ascienda con mayor velocidad, o, que un avión avance, también, con mayor velocidad, y, que consuma menos combustible, pudiendo utilizar, así, motores de menor potencia.

94. 发明专利

FR2898582A3 SYSTEME DE STRUCTURE ARTICULEE POUR AILE DE TRACTION 未知
公开(公告)号：FR2898582A3
公开(公告)日：2007-09-21
申请号：FR0602357
申请日：2006-03-17
申请人： BALLU ARNAUD MICHEL GHYSLAIN
发明人： BALLU ARNAUD MICHEL GHYSLAIN
IPC分类号： B64C31/06 , B64C3/16 , B64C3/38
摘要： L'objet de la présente invention est un système de structure articulée pour aile de traction, notamment gonflables et utilisées dans les pratiques de glisses aérotractées, caractérisée en ce que un étranglement marque une discontinuité mécanique du bord d'attaque sensiblement au milieu de la dite aile, permettant son ouverture ou sa fermeture selon le principe d'une pince.

95. 发明专利

RU2187444C2 FLYING VEHICLE 未知
公开(公告)号：RU2187444C2
公开(公告)日：2002-08-20
申请号：RU2000109622
申请日：2000-04-14
申请人： VORON MEKH ZD , FEDERALNOE GUP
发明人： BONDAR A V , SUKHORUKOV V N , AGEEV V V , GOLOLOBOV L G , IVANOVA T S , BAL S O
IPC分类号： B64C3/16
摘要： aeronautical engineering. SUBSTANCE: proposed flying vehicle is provided with powerful engine (360hp) in rather light vehicle. Proposed flying vehicle has fuselage, outer wing panel, wing attachment unit, horizontal and vertical tails, engine with propeller, pylon for attachment of engine on center-wing section and three-wheeled undercarriage with nose and partially retractable wheels. Engine is so positioned that axis of propeller is located at distance of 1/4 of aerodynamic mean chord above wing plane; wing consists of center-wing section, two outer-wing panels at dihedral angle of lesser than 6 deg. and two wing tips located at angle lesser than 30 deg. from plane of outer-wing panels. Fuselage is provided with cabin at observation angle in vertical plane from -50 deg. to 80 deg. and in horizontal plane from -110 to 100 deg. at height, width and length of carbon of 1:2:3, respectively. EFFECT: extended functional capabilities. 2 cl, 3 dwg

96. 发明专利

DE19718228A1 Aircraft with double boat element 未知
公开(公告)号：DE19718228A1
公开(公告)日：1998-11-05
申请号：DE19718228
申请日：1997-04-30
申请人： SCHUBERT WERNER
发明人： SCHUBERT WERNER DR MED
IPC分类号： B64C3/00 , B64C3/10 , B64C3/16
摘要： Using the known propulsion principles of catamarans, aircraft have on the outer ends of the possible V-form aerofoil(2) aerodynamic containers or airbags(3,4) which are filled with helium and extend in the direction of flight. These components are symmetrical to the aircraft's longitudinal axis and are conducive to stability and flight safety. The components are made of sheet aluminium, light metal sheet, plastic, or some other airtight material.

97. 发明专利

DE19644820A1 Aircraft 未知
公开(公告)号：DE19644820A1
公开(公告)日：1998-04-23
申请号：DE19644820
申请日：1996-10-21
申请人： SCHUBERT WERNER
发明人： SCHUBERT WERNER DR MED
IPC分类号： B64C17/04 , B64D17/80 , B64D25/00 , B64C3/16 , B64C1/00 , B64C17/00 , B64D27/02
摘要： The aircraft has overhead main wings (3) sloping upwards to hollow aerodynamic cylinders at the wing tips. The tail has a cone shape to increase the airflow over the tailplane and over the rudder. The engines are mounted under the floor of the cabin and are slung from vertical supports (5) which are attached to the wings. Thruster rockets under the nose of the aircraft are used to lift the nose in an emergency eg. during crash landing. Additional lift is provided by parachutes stowed in the nose and also used to slow the aircraft when making an emergency landing.

98. 发明专利

DE29611154U1 未知
公开(公告)号：DE29611154U1
公开(公告)日：1996-08-29
申请号：DE29611154
申请日：1996-06-26
申请人： DOLCH STEFAN DIPL ING FH
IPC分类号： A63H27/18 , B64C3/14 , B64C3/16

99. 发明专利

DE4443548A1 Aircraft wing with contour in form of broad ellipse 未知
公开(公告)号：DE4443548A1
公开(公告)日：1996-06-13
申请号：DE4443548
申请日：1994-12-07
申请人： SCHUBERT WERNER
发明人： SCHUBERT WERNER DR MED
IPC分类号： B64C3/00 , B64C39/08 , B64C3/16 , B64C5/08
摘要： The wing structure is used for an aircraft. It has airflow pressure channels (7,7a) which are present on or in the undersurface (2a) of the curved, birdlike wing (2). The sidewalls (7a) of the channels taper towards the trailing edge of the wing.Aerodynamically slim stabilisation bodies (9) are fitted to the wingtips and have gyro stabilisers in the nose sections (9a). The wing is made from plastics, metal, steel, wood or a composite material.

100. 发明专利

FR2261973B1 未知
公开(公告)号：FR2261973B1
公开(公告)日：1981-08-21
申请号：FR7501389
申请日：1975-01-17
申请人： SEITZ WERKE GMBH
IPC分类号： B64C3/16 , B67C3/26 , B67C3/04

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式