Matches 1 - 50 out of 389 1 2 3 4 5 6 7 8 >


Match Document Document Title
US20120018580 Insulating blanket for an aircraft and assembly integrating such a blanket  
This invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel...
US20110226901 METHOD FOR LAYING A FLOOR COVERING IN A CABIN OF A VEHICLE  
A method for laying a floor covering onto a floor in a cabin of a vehicle comprises the steps of applying a connection means to an element of a group comprising the floor covering and a floor,...
US20120286092 RECONFIGURABLE FLOORBOARD SYSTEM  
A floorboard for a reconfigurable floorboard system may include a substantially trapezoid shaped plate. An interlocking feature may be formed proximate an edge of at least three sides of the plate...
US20140367519 METHOD OF INSTALLING A FIXTURE  
A method of installing a fixture, such as a bracket, in a fuselage structure of an aircraft includes the steps of: providing or generating a three-dimensional digital model of the fixture;...
US20120104166 INNER BENT REPAIRMENT  
A method for repairing the skin of the fuselage of an airplane from the inside to be used when the skin of the fuselage has been damaged between a first stringer and a second stringer adjacent to...
US20130320140 WALL INSTALLATION SYSTEM AND METHOD  
A system for attaching a wall panel includes a wall panel and a lock strip. The wall panel has a back and a tab extending from the back. The lock strip is moveably attached to a wall frame member,...
US20120256048 Vibration Isolation System  
A vibration isolation system for attenuating vibration energy between two aircraft structures, such as between the aircraft's fuselage and interior cabin. The vibration isolation system includes a...
US20110001008 Aircraft floor of optimized compactness  
An aircraft floor portion includes crossmembers. Each crossmember comprises a top partial crossmember and a bottom crossmember, with at least one gap being left between the top partial crossmember...
US20110309187 NESTED CORE GAS TURBINE ENGINE  
An aircraft, with the ability to cruise at supersonic speeds, designed to increase cruise lift/drag ratio, reduce sonic boom and have greater downward visibility by having an ‘inverted’ nose...
US20140203143 Front aircraft sealed bottom comprising recesses for housing cockpit equipment  
A leaktight nose cone backplate for an aircraft having a first side oriented towards a radome zone intended to house a mobile antenna, and a second side opposite the first side and oriented...
US20110168836 AIRCRAFT ENGINE SUPPORTING PYLON  
Pylon (19) attached to an aircraft fuselage part (17) having a close transversal section of a curved shape comprising a skin (31) and a plurality of frames (33); its structural configuration...
US20110233336 FUSELAGE STRUCTURE FOR COMBINED FIXING OF INSULATION BLANKETS AND ITEMS OF EQUIPMENT, AIRCRAFT INCORPORATING SUCH A STRUCTURE  
An installation of systems in aircraft fuselages such as thermophonic insulation mattresses and devices such as onboard systems, and bundles of electric wires or fluid ducts (air, water, oxygen,...
US20150253117 INSTALLATION STRUCTURE OF SEEKER WINDOW AND FLYING OBJECT WITH SEEKER WINDOW  
A seeker window includes a transparent plate and a frame structure coupled to a circumference of the transparent plate. An installation structure of the seeker window has a flexible window frame...
US20110233335 IMPACT RESISTANT AND DAMAGE TOLERANT AIRCRAFT FUSELAGE  
The aircraft fuselage part (31) located in a section of an aircraft (11) having attached a propulsion system (13) by means of upstream pylons (17) that comprises: a skin (35); a plurality of...
US20110108667 Thermoplastic Composite Window Panel for Aircraft Applications  
An aircraft trim panel structure includes a thermoplastic resinated quadraxial fiberglass lay-up prepreg first open structure skin layer having at least a 28% open area. A thermoplastic resinated...
US20110297785 AIRFRAME POSITION ADJUSTING STRUCTURE  
Provided is an airframe position adjusting structure capable of adjusting the position of an airframe (A) inclined in the left-and-right direction. In the airframe position adjusting structure...
US20130092792 Method and Apparatus for Out-of-Autoclave Adhesive Shear Bonding of Structures  
The shear bonding method is configured to facilitate bonding of structures in an out-of-autoclave environment. The shear bonding method includes bonding a plurality of frame members to the...
US20150166167 Pressurized Airplane Fuselage, Comprising A Pressure Bulkhead Movable Fixed To The Fuselage  
A pressurized aircraft fuselage includes a pressure bulkhead installed on a fuselage structure, which forms a barrier between an internal pressurized cabin area and an outside area. The edge of...
US20150183505 SUBFLOOR STRUCTURE WITH AN INTEGRAL HULL FOR A ROTARY WING AIRCRAFT  
The invention relates to a subfloor structure with an integral hull, for a rotary wing aircraft. The subfloor structure comprises an integral subfloor hull that defines in one piece, upward web...
US20150252903 SPACER AND GASKET ASSEMBLY FOR USE ON AN AIRCRAFT  
A spacer and gasket assembly is shown for receipt between a static structure having a surface and fastener holes therethrough and a removable structure having a surface and fastener holes. The...
US20120298799 SELF-SUPPORTING CABIN STRUCTURAL SEGMENT  
A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it...
US20080302913 CARGO FLOOR, SYSTEM, AND METHOD  
Embodiments provide a cargo floor, a system, and a method adapted to be made integral with or complementary of the aircraft fuselage. Cargo floor members may be adapted to be coupled with a flat...
US20120119028 FUSELAGE EMPLOYING MULTIFUNCTIONAL CROWN AND METHOD OF MAKING THE SAME  
A fuselage structure includes a fuselage body and framework for stiffening the body. The framework includes at least one frame member having a duct therein for routing a utility through the body.
US20150108272 AIRCRAFT FUSELAGE COMPRISING AN OUTER INSULATION  
An aircraft fuselage comprising a structure, a skin connected to the structure and forming a barrier between the interior and the exterior of the fuselage, an external coating being plated or...
US20150232167 INTERIOR TRIM ARRANGEMENT FOR AN AIRCRAFT CABIN  
An interior trim arrangement for an aircraft cabin, having lateral ceiling elements, and an angled element having limbs limb extending from one another, one lateral ceiling element arranged offset...
US20130032661 LOADS INTERFACE, PARTICULARLY A LOADS INTERFACE FOR A PLUG TYPE AIRCRAFT DOOR  
A loads interface (1), particularly a loads interface (1) of an aircraft door with an edge frame (13), an outer skin (15) and a beam (14). A loads transferring flange (11) is designed to transmit...
US20090166471 Fuselage Structure and Method for the Production of a Fuselage Structure  
The present invention provides a method for the production of a fuselage structure, and a fuselage structure, in particular of an aircraft or spacecraft, with an inner shell arrangement which has...
US20090121081 Composite Bulkhead and Skin Construction  
Aircraft fuselage structures have fuselage bulkheads in which the bulkhead outer caps are integrated with the skin, thereby reducing fastener count and weight. These outer caps and skin are...
US20130099056 FUSELAGE CELL FOR AN AIRCRAFT, PARTICULARLY AN AIRPLANE  
A fuselage cell for an aircraft includes at least two shell segments forming a fuselage cell. The shell segments are provided with a plurality of longitudinal and/or circumferential reinforcements...
US20120126057 FLOOR FOR AN AIRCRAFT CARGO COMPARTMENT AND METHOD FOR THE ASSEMBLY THEREOF  
In conventional aircraft cargo compartments panels or similar flat floor elements are fastened to floor beams or similar supporting elements that are installed in the body of the aircraft....
US20110095130 COMPOSITE AND STRUCTURE, PARTICULARLY IN THE AEROSPACE SECTOR  
The present invention provides a composite, in particular in the field of aviation and aerospace, comprising an omega-stringer that comprises a comb portion, and a connecting member that is...
US20130112811 AIRCRAFT WITH AN INTEGRATED ENERGY-ABSORBING DEFORMATION STRUCTURE AND AIRCRAFT WITH SUCH A FUSELAGE  
An aircraft fuselage has an integrated energy-absorbing deformation structure. The fuselage includes annular frames, longitudinal fuselage beams interconnecting the annular frames, and a covering...
US20110006158 PIVOTING EQUIPMENT CARRIER IN COMBINATION WITH A MODIFIED LUGGAGE RACK  
The present invention relates to a device for the installation of commercial components in an aircraft that features at least one equipment carrier for accommodating the components, wherein the at...
US20110001006 Process for making an aircraft having a floor  
The method of fabricating an aircraft comprises the following steps: fastening two lateral floor portions, each firstly to a fuselage element and secondly to supports that are connected to the...
US20080164372 Method of optimizing stiffened panels under stress  
The subject of the disclosed embodiments is a method of optimizing stiffened panels under stress. In particular, the method makes it possible to determine the stress distribution in stiffened...
US20120187245 FUSELAGE SEGMENT, AND METHOD FOR THE PRODUCTION OF A FUSELAGE SEGMENT  
A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are...
US20120132749 TAIL-CONE OF AN AIRCRAFT WITH MOVABLE FAIRING  
A tail-cone of an aircraft includes a skin provided with a movable fairing which, by a swing articulated mechanism, is supported on the skin in order to allow the opening/closing of the movable...
US20130032660 LOADS INTERFACE, PARTICULARLY LOADS INTERFACE OF AN AIRCRAFT STRUCTURE AND APPLICATION OF SAID LOADS INTERFACE  
A loads interface (1) of an aircraft structure with an edge member (6) and a background structure both preferably made from fiber reinforced plastics. A loads transferring flange (2) is adapted...
US20080302912 Bladderless Mold Line Conformal Hat Stringer  
Apparatus and techniques for providing a closed hat stringer are disclosed. In one embodiment, a closed hat stringer for stiffening a composite structure includes opposing cavity walls situated...
US20120248247 AIRCRAFT FUSELAGE WITH HIGH STRENGTH FRAMES  
Fuselage section of an aircraft whose structure comprises a skin (10), a plurality of frames (30) positioned transversely to the longitudinal axis of the fuselage and a plurality of longitudinal...
US20120267478 AIRCRAFT INCLUDING AN INTERNAL PARTITION  
The aircraft includes a structural portion such as a fuselage, a wing, or a tail, the structural portion including a wall separating the inside from the outside of the portion and including...
US20150232166 AIRCRAFT CABIN ARRANGEMENT  
An aircraft cabin arrangement is disclosed which extends in a rectilinear manner along a cabin axis, having a ceiling trim arrangement which delimits the cabin interior upwardly from the cabin...
US20090020645 Method for Frabricating an Aircraft Fuselage in Composite Material  
A method for manufacturing an aircraft fuselage includes an internal framework surrounded by an external skin made of composite material, in which the internal framework at least partially...
US20140231586 HIGH-WING-AIRCRAFT FUSELAGE SUPPORT STRUCTURE  
A structural support assembly for a high-wing aircraft may include a plurality of columns extending through a passenger compartment of the aircraft having a pair of wings mounted proximate a top...
US20110011978 FLOOR SYSTEM FOR A FUSELAGE AIRFRAME OF AN AIRCRAFT  
A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as...
US20110186683 METHOD AND A DEVICE FOR THE MANUFACTURE OF A STIFFENING STRUCTURE FOR AN AIRCRAFT FUSELAGE SEGMENT, AND ALSO A STIFFENING STRUCTURE  
A method for stiffening a skin field of an aircraft fuselage includes providing a skin field for an aircraft fuselage, manufacturing an integral lattice-shaped stiffening structure including a...
US20130221156 AIRCRAFT NOSE STRUCTURE AND CORRESPONDING AIRCRAFT  
This aircraft nose structure comprises frames (2, 4, 6), a lower windshield frame member (12) and an upper windshield frame member (14) which are adapted to receive a windshield. The lower...
US20110068228 CABLE WAY FOR AIRCRAFT WITH A STRUCTURE MADE OF COMPOSITE MATERIAL  
A retention device, in the form of a trunking with a substantially U-shaped section, for retaining at least one cable running along the structure of an aircraft, fastened to said structure by a...
US20080265093 Integrated multispar torsion box of composite material  
The invention relates to an integrated multispar torsion box structure of composite material for aircraft, comprising a lower skin (12), an upper skin (11), several spars (9), each of which...
US20080210817 Energy-absorbing Square Tube Composite Stanchion  
An energy absorbing structural strut employs a composite tube bonded to an end fitting with the bond being slightly lower in strength than the crushing strength of the tube in axial compression....

Matches 1 - 50 out of 389 1 2 3 4 5 6 7 8 >