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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... |
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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,... |
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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... |
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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;... |
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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... |
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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,... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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,... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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. |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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.... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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... |
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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.... |