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WO/2012/061498 |
An apparatus for making and using a fastener suitable for use in airplane manufacture or repair that is coated with a pre-mixed moisture cure sealant. The sealant layer is coated with a frangible moisture barrier that will break apart wh...
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WO/2012/056076 |
The invention relates to filler panels for aircraft fuel tank coveringings. The filler panels (45) cover the gaps between the upper and lower coverings (19, 21), stiffened by stringers (25, 25', 25"), of an airfoil of an aircraft structu...
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WO/2012/051634 |
The invention relates to a decompression unit (1) for use in a decompression opening (2) of a wall element (3) of an aircraft, having a panel (5) which can be mounted via a frame (4) in or over the decompression opening (2) which panel (...
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WO/2012/054692 |
Method of cutting and installing carpet tiles on a floor of a mass transit vehicle, particularly including aircraft. The tile lengths in an installation are the same and the tile widths are customized to a particular section of the aircr...
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WO/2012/054080 |
A cargo storage and handling system for aircraft. A rack assembly mounts in an upper portion of the fuselage to form a cargo area in the upper lobe thereof. The rack includes a series of frames that are suspended from pre-existing attach...
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WO/2012/052484 |
An insulation arrangement (12) for thermally and acoustically insulating an aircraft fuselage, which comprises at least one insulation packet (14, 16, 18, 20, 22) arranged on an exterior skin (24) of the aircraft. The insulation packet c...
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WO/2012/048855 |
The invention relates to a holding device (10) for in particular panel-shaped interior lining parts (12) of a fuselage. For a configuration that is easy and simple to mount, each holding device (10) comprises: - a supporting device (16),...
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WO/2012/045931 |
The invention relates to a secure access airlock enables the communication between several rooms of an aircraft, the secure airlock being installed in an area of the aircraft between a first room and at least one second room, characteriz...
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WO/2012/047751 |
An aerospace vehicle (100) includes a plurality of composite stiffeners (220). Each stiffener of the plurality has a stack of plies of reinforcing fibers. To increase stiffness without increased weight, at least some of the plies in the ...
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WO/2012/045871 |
The present invention creates a composite (1) for an aircraft or spacecraft, comprising: a skin portion (2); a stringer (3) which is attached to the skin portion (2); and a former (4) made from fibre composite material, which is attached...
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WO/2012/040489 |
An integrated aircraft interior module includes one or more ceiling panels, sidewall linings, decompression ventilation provisions, and overhead stowage compartments including cabin air distribution ducting, personal service units. The s...
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WO/2012/035184 |
The invention relates to an arrangement for connecting directionally reinforced parts made from a composite material, in which, in the connection area, at least one of the parts (11) is a directionally reinforced part comprising a stack ...
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WO/2012/032208 |
The invention relates to a method for the production of T-shaped stringers for an aircraft, in which the stringers comprise a web and a flange. The method includes the following steps: a first step in which a carbon fibre laminate is hot...
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WO/2012/028887 |
An assembly (10) has: a first pipe (20) being made from a composite material and having a first pipe end section (24) with a first pipe end section inner surface (28) that tapers inwardly, a first reinforcing element (30) having a first ...
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WO/2012/028374 |
In order to be able to airdrop cargo items during a flight, use is made of cargo gates which secure the cargo items and release them at a given time. The present application describes an improved cargo gate. This cargo gate for holding a...
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WO/2012/028263 |
An aircraft structural assembly (10) comprises an area element (12) which has a core (20) and an outer layer (22). A first surface (30) of the area element (12) is convexly curved, at least in certain sections, relative to an imaginary c...
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WO/2012/024023 |
A composite structure comprises stacked sets of laminated fiber reinforced resin plies and metal sheets. Edges of the resin plies and metal sheets are interleaved to form a composite-to-metal joint connecting the resin plies with the met...
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WO/2012/024051 |
A method for connecting a wing. A frame for a wing is positioned relative to a fuselage of an aircraft. The frame has bays and comprise a front spar, a rear spar, and a number of spars located between the front and rear spars. A first nu...
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WO/2012/022891 |
The invention belongs to the field of the installation of systems in aircraft. More specifically, the invention relates to the installation of avionics furniture, electrical master boxes and IFE bays. Compared with the arrangements known...
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WO/2012/019739 |
The invention relates to an aircraft interior lining component (10) consisting at least partially of a composite material, wherein the composite material comprises a matrix (24), first reinforcing fibres (26) embedded in the matrix (24) ...
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WO/2012/020078 |
A vehicle window with a primary window pane arrangement (2, 4, 8, 10, 12), a secondary window pane (14) that is spaced apart from the primary window pane arrangement and a window funnel (16) that extends between the secondary window pane...
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WO/2012/021228 |
A system for supporting a load across non-intersecting beams (12) each having a web (20) depending from an upper chord (16) with an upper surface (17) generally parallel with a chordal plane includes at least one crossing member (30) int...
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WO/2012/016900 |
The present invention provides a facing arrangement (11) for a hold (12) of an aircraft or spacecraft (13), comprising: a first and a second panel (14a-14d) which form a gap (15) between them; a first mounting part (22) which is to be at...
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WO/2012/010305 |
The invention relates to a structural component (1), comprising at least one main-load-bearing covering shell (B) and a carrier structure (T) for fixing the covering shell, wherein the covering shell (B) is designed in the form of a sand...
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WO/2012/010306 |
The invention relates to a main-load-bearing planking shell (B) for a structural component (1), wherein the planking shell (B) is designed with an outer edge section (60) having an outer edge (61) for attaching said shell to a support co...
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WO/2012/010304 |
The invention relates to a structural component (1) of a flow body, comprising at least one lining shell (B) that carries a main load, said lining shell having a core layer (33) that absorbs shear load and that comprises a plurality of c...
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WO/2012/010882 |
The invention provides an arrangement and methods for thermally insulating aircraft, particularly but not exclusively for when the aircraft is operating in extremely hot or cold conditions, and describes an aircraft skin construction com...
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WO/2012/007449 |
A beam (20) comprising first and second flanges (23, 24), the beam (20) having a first region (28, 30) extending between the flanges (23, 24) and a second region (26) extending between the flanges. The first region (28, 30) is designed t...
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WO/2012/004490 |
The subject of the invention is a method for producing a central wing box comprising an upper panel (32), a lower panel (34), a front spar (36) and a rear spar (38), the upper edges of said spars (36, 38), which are approximately paralle...
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WO/2012/001205 |
Aircraft component which comprises at least one panel (11) of composite material, formed by a skin (13) and a plurality of stiffening stringers (15) which are configured with a core (17) and a base (19) of width (A), said stiffening stri...
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WO/2012/001207 |
Aircraft fuselage made out with composite material and manufacturing processes. The structure of the fuselage (1 1 ) comprises a skin (13), a plurality of frames (17) positioned transversely to the longitudinal axis (9) of the fuselage (...
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WO/2012/001206 |
Reinforcement structure (1) for an opening (10) in the primary structure of an aircraft, said structure comprising a skin (2), frame members (3) which are transverse with respect to the flying direction of the aircraft, and stringers (4)...
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WO/2011/163453 |
A door apparatus (100) includes a door (102), actuating mechanism (104), and tie rod mechanism (126,128), the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mec...
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WO/2011/163453 |
A door apparatus (100) includes a door (102), actuating mechanism (104), and tie rod mechanism (126,128), the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mec...
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WO/2011/158015 |
An aircraft wing box spanwise joint (2), comprising a rib having a web, and a pair of rib fittings joined together, each rib fitting forming a closed loop around the periphery of the rib, wherein the rib is integrally formed with one of ...
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WO/2011/154582 |
Procedure for the manufacture of large parts of composite material, controlling the thickness of the edges thereof. It relates to the manufacture of a part (11) possessing edge zone (11) in an aeronautical structure through a join with j...
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WO/2011/145972 |
The invention relates to the field of aircraft construction. The aircraft fuselage comprises consecutive frames (1) with an outer skin (2) secured thereto, stringers (3) connected to the skin (2) and the frames (1), passenger floor cross...
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WO/2011/145291 |
Provided is an occluding member for an opening with which a lightning protection function can be reliably maintained. The occluding member is provided with a first insulator (63) and a second insulator (65) between a door body (30) and a...
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WO/2011/146194 |
A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, including a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having...
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WO/2011/146543 |
A radome comprise a substrate having a first material and an outer layer having a second material, which is positioned adjacent to the substrate. The first material of the radome can comprise a generally rigid polymeric material. The gen...
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WO/2011/141647 |
The invention relates to an aluminum-based alloy comprising, in % by weight, 2.1 to 2.4% of Cu, 1.3 to 1.6% of Li, 0.1 to 0.51% of Ag, 0.2 to 0.6% of Mg, 0.05 to 0.15% of Zr, 0.1 to 0.5% of Mn, 0.01 to 0.12% of Ti, optionally at least on...
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WO/2011/134917 |
The invention relates to an aircraft fuselage structure comprising a circumferential reinforcing frame (2) and a plurality of stringers (3) substantially perpendicular to the frame. The frame comprises a mechanically weakened area capabl...
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WO/2011/134640 |
The invention relates to a rail system (10) which can be used for mounting a component in an aircraft. Said rail system comprises a first rail element (12) provided with a securing device (22) in order to detachably secure the first rail...
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WO/2011/135245 |
The aim of the invention is to reduce the multiple costs of manufacture, assembly, use, and upkeep connected with the assembly of window coaming on aircraft fuselages. To this end, the invention provides a particular shape for the coamin...
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WO/2011/135134 |
Internal structure for aircraft, comprising a skin (1) of composite material, stringers (2) of composite material integrated into the interior of the aforementioned skin (1), and frames (3) of composite material, the skin (1) comprising ...
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WO/2011/131290 |
An aircraft interior equipment component (10) with a frame (12) which comprises two rigid frame sections (14a-h) and a joint (16a-h) connecting the rigid frame sections (14a-h) to one another, and with a sheetlike section (18) which is s...
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WO/2011/131492 |
The invention relates to sound absorption in cabins of aircraft. The invention relates in particular to an aircraft cabin panel absorber for sound absorption, to a device for sound absorption in an aircraft cabin, and to an aircraft comp...
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WO/2011/132349 |
Disclosed are an aircraft, and an aircraft cockpit window onto which an electromagnetic shield film for preventing electromagnetic noise can be installed reliably, easily, and at a low cost. An electromagnetic shield film (27) is install...
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WO/2011/127899 |
An aircraft fuselage with an integrated energy-absorbing deformation structure, wherein the fuselage (1) has annular frames (10; 110; 210) and the frames (10; 110; 210) have interconnecting longitudinal fuselage beams (12) and a casing (...
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WO/2011/128858 |
The present invention relates to an acoustic insulation device having at least two panels equipped with resonators intended to acoustically insulate two environments outside these panels, and to a method for manufacturing this device. Th...
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