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JP5085560B2 |
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JP5053933B2 |
Described are hyperimmune serum-reactive antigens from a specific pathogen, a tumor, an allergen or a tissue or host prone to autoimmunity, said antigens being suited for use in a vaccine for a given type of animal or for humans.
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JP2012524692A |
An aircraft assembly comprising: a pair of covers; a spar web extending between the covers in a thickness direction, the spar web having a length which extends in a span-wise direction; and a container which extends from the spar web and...
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JP5046115B2 |
To provide a noise reduction device composed by a simple mechanism capable of appropriately reducing a noise generated between a steering wing and a body wing without deteriorating an aerodynamic performance of an aircraft in taking off ...
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JP2012521920A |
An aerofoil wing is provided, including a main aerofoil, and a high-lift flap, which is movably arranged on the wing using side-by-side adjustment mechanisms. Each adjustment mechanism includes a first adjustment lever, hinged to the mai...
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JP4980921B2 |
A system for reducing aerodynamic noise of a supplementary wing of an aircraft is provided. The supplementary wing is hinged to a main wing and is extendable when a gap region between the main wing and the supplementary wing is opened. T...
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JP4963942B2 |
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge de...
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JP4934781B2 |
A roll steering method subdivides the direction of an aircraft control surface into two elements and, during a roll control operation using ailerons, steers an upper element of the control surface in the roll direction and a lower elemen...
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JP2012504519A |
A leading edge slat arranged on the aerofoil of an aircraft. The leading edge slat is provided on the front of the main wing. The leading edge slat has a partially extended setting, with its trailing edge flat against the wing, and a fur...
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JP4820366B2 |
A compact actuator ( 20 ) is arranged to selectively move an airfoil surface ( 27 ) relative to a support ( 27 ) relative to a support ( 21 ). The actuator includes a gear reduction unit ( 24 ) mounted on the support. The gear reduction ...
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JP4820878B2 |
A rudder of a commercial aircraft is provided that is divided along its longitudinal direction in at least one region and the parts of the rudder can be spread against the air flow surrounding the aircraft by means of an actuator in orde...
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JP2011201530A |
To provide a slat disconnect sensor that detects that a slat part relatively moves from a connect condition to a disconnect condition, during an undesired condition.A first disconnect sensor 132 includes first and second arms 60, 62 pivo...
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JP2011162154A |
To provide a high lift force-generating device and a wing, which can suppress generation of aerodynamic noise while suppressing increase in body weight.A recess and projection part 20 is formed in a bottom plate 7 extending rearward in a...
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JP2011522739A |
A device for the generation of aerodynamic vortices to be arranged on the spanwise side edge of a wing, or a regulating flap adjustably arranged on the latter, which in each case have a chordwise direction and a spanwise direction, where...
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JP2011519781A |
An aircraft wing assembly comprising: a wing; a spoiler pivotally attached to the wing; and a spoiler deployment mechanism. The deployment mechanism comprises a scissor linkage mechanism comprising an upper link pivotally attached to the...
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JP2011518712A |
An aerodynamic body that can be adjusted relative to a main wing of an aircraft by an adjusting device is provided. A gap between the aerodynamic body and another aerodynamic body or a component of the fuselage or the main wing is formed...
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JP4703638B2 |
Aircraft leading edge device systems and methods for sizing such systems are disclosed. In one embodiment, a spanwise lift coefficient distribution for an airfoil corresponding to at least one design condition and at least one aircraft a...
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JP4699487B2 |
The present invention provides a high-lift device (3), a wing (1), and a noise reduction structure for high-lift devices capable of suppressing the occurrence of aerodynamic noise while restricting an increase in airframe weight. A high-...
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JP2011516804T |
It is related with a flow change device of fluid. A flow change device of the present invention is for generating a turbulent flow in the fluid, when fluid moves to the device concerned. This device has a plurality of turbulent flow gene...
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JP2011515277T |
The Surratt deployment mechanism for airplanes is provided with the following. The 1st drive member connected with Surratt at the 1st drive point, The 2nd drive member connected with the Surratt at the 2nd drive point offset from the 1st...
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JP2011512298A |
The invention relates to a panel pivoting about an axis parallel to a side of the panel, which comprises a first continuous coating (1),a main structural frame of a composite stiffener (2, 3, 4, 5, 6) connected to the coating (1) and inc...
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JP4646543B2 |
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JP2011506189A |
A high-lift system for an aircraft with a main wing and a slat that by way of an adjustment device is adjustable relative to the main wing to various adjustment states, with a gap resulting between the rear of the slat, which rear faces ...
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JP2011504149A |
The invention relates to a device for moving a trailing edge flap of an aircraft wing, in which device the trailing edge flap comprises one or several flap segments, wherein a first flap segment is movably mounted on the wing and is conn...
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JP4571953B2 |
A guiding device (4), which serves as a slide, is adjustable in the form of a straight landing flap carrier (3). The slide is connected to the landing flap and extends and retracts the landing flap guided along the flap carrier through g...
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JP2009545478T5 |
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JP4550835B2 |
A 2-D correction system uses intermittent deployment of aerodynamic surfaces to control a spin or fin stabilized projectile in flight; correcting both crossrange and downrange impact errors. Intermittent surface deployment develops rotat...
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JP4531066B2 |
The invention relates to a leading edge mobile flap (16) for a main wing of an aircraft, this flap including an aerodynamic skin (18) that has a bird impact-sensitive frontal area (24), and a rear skin (28) integral with the aerodynamic ...
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JP4478509B2 |
To provide a high lift generator capable of effectively generating high lift by realizing the circulation control by the Coanda effect while considerably reducing the manufacturing cost and the maintenance cost and considerably reducing ...
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JP2010512274A |
A wing of an aircraft has a mainplane, which has an upper face, a lower face and an aerodynamically shaped area. The wing has an additional airfoil which is articulated on the mainplane and can be extended from a retracted state with a s...
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JP2010509118A |
A high-lift system on the wing of an aircraft and a method for its operation are described. High-lift flaps (2) which are arranged on the wing (1) are extended from a retracted position in order to increase the lift, and a slot (3) throu...
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JP4405704B2 |
Improving convertible aircraft of the aforementioned type mainly in terms of the active control of vibrations, while at the same time avoiding the addition of significant additional masses for essentially countering the excitations cause...
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JP2009545478A |
High-lift system for an aircraft comprising a main wing (1), a high-lift flap (2) which is coupled to the main wing (1) by a track rear link kinematics comprising a carriage (9) to which the flap is rotationally coupled via a first joint...
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JP2009298392A |
To adjust a lift in an area larger than ever concerning an aircraft.The larger adjusting area of the lift is acquired by collectively using small wings on the aircraft.
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JP2009538773A |
The invention concerns an apparatus for and a method of producing aerodynamic resistance on an aircraft, comprising at least one braking flap, wherein the at least one braking flap can be extended into the airflow around the aircraft. In...
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JP4349771B2 |
Disclosed is an aircraft, configured to have a wide range of flight speeds, consuming low levels of power for an extended period of time, while supporting a communications platform with an unobstructed downward-looking view. The aircraft...
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JP4319004B2 |
The assembly (60) has a reaction link (90) with an anchoring end (94) pivotally coupled to one end (30) of an extendable actuator (24) and a driving end (92) pivotally coupled to a portion (78) of a drive member (74). The extendable actu...
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JP4319003B2 |
The assembly (60) has a reaction link (90) with an anchoring end (94) pivotally coupled to one end (30) of an extendable actuator (24) and a driving end (92) pivotally coupled to a portion (78) of a drive member (74). The extendable actu...
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JP4314116B2 |
A joint arrangement connects a longitudinal edge of a first component with an upper surface of a second component. At least two cooperating bands are secured with their first ends respectively on opposite sides of the first component, an...
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JP4310034B2 |
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JP4310033B2 |
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JP2009527405A |
A high-lift flap of an aircraft is provided having a device for influencing the flap vortex as well as a device for influencing the flap vortex at the lateral edge of the aerodynamic high-lift flap, which can be achieved effectively and ...
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JP2009523184A |
The present invention relates to a method of adhering a first element (2) and a second element (3) using an adhesive body (4). The present invention particularly relates to a method of bonding large area elements of an aircraft having a ...
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JP4270738B2 |
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JP4270724B2 |
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JP4266347B2 |
A joint for the connection of components (T 1 , T 2 ) that are movable relative to one another, on respective longitudinal sides (L 1 , L 2 ), includes at least two cooperating bands, which are secured with their first ends (E 1 ) respec...
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JP2009518219A |
With a device for error detection of adjustable flaps on aircraft wings, it is proposed that each flap is provided with a tube as a transmission element arranged in the wing span. The tube is connected fixedly at one end with the flap an...
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JP2009515750A |
Described is a brake flap for an aircraft, which brake flap, for the purpose of delaying the aircraft, can be set at an angle relative to the airstream flowing around it, wherein the flap (20) comprises a free edge (21) which when set at...
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JP2009511314A |
An aircraft landing flap includes a flap member having an abrasion-resistant coating coated on an abrasion region exposed to mechanical rubbing contacts with an aircraft spoiler. The coating comprises a polyurethane matrix based on aliph...
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JP4235469B2 |
One or more layers of fiber material (5) are braided or wound around a two part tool core. One part (3) of the core is then removed and the wound fiber structure(6) remaining on the other half is compressed to create a preform (7). The p...
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