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8172176 |
Integral composite slider for aircrafts
A slider apparatus integral with a slidable member and a method for integrating the slider apparatus with the slidable member. The slider apparatus integrated with the slidable member may be...
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8167243 |
Systems and methods to provide optical enlargement of passenger interior cabin space
Systems and methods achieve an optical effect of cabin enlargement of a passenger vehicle. The optical effect creates a visual impression of a higher cabin when viewed from the forward part of the...
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8157209 |
Method for isolating a cabin wall of an aircraft or for cooling or heating of cabin air and a cabin wall suitable therefore
The present invention relates to a method for insulating an aircraft cabin 6 and for the cooling or heating of cabin air in an aircraft, respectively with the method comprising the steps of:...
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8128025 |
Providing skins for aircraft fuselages
An aircraft including a space frame fuselage structure. A plurality of panels are connected with the structure and configured to form a skin over the structure. The panels are movable relative to...
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8123164 |
Device for fixing a seat rail on a floor, and aircraft equipped with such a fixing device
A device for fixing a seat rail, designed to maintain passenger seats on a floor, wherein it includes a connecting bracket, secured to the floor and to the seat rail, the bracket being adapted to...
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8118260 |
Fitting for trimming a horizontal stabilizer of an aircraft
A fitting for trimming the horizontal stabilizer of an aircraft, made of composite material, the fitting including side walls of a torsion box as well as joining elements which join the fitting to...
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8100360 |
Light rail system for powered introduction of large loads in a structure
A device for securing installed equipment in an airplane, with one or more oblong attachment rails, one or more attachment means for securing the attachment rails to an airframe structure, and one...
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8096503 |
Structuring construction for an aircraft fuselage
A structuring construction for an aircraft fuselage is provided having an outer skin as well as a plurality of formers extending at a spacing side by side crosswise to the longitudinal direction of...
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8096092 |
Lightweight structural panel
What is described is a lightweight structural panel which comprises a planarly extended outer skin of given thickness and stiffening elements which are connected to this outer skin and are arranged...
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8094041 |
Seat cushion retention and monitoring in an aircraft
An aircraft seating system comprises a seat frame having a top side, a seat cushion having a bottom side, a plurality of conductive first sides of a hook-and-loop fastener system attached to the...
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8091828 |
Structural element and method of manufacture
In a method for manufacturing a structural element intended for aeronautical construction, at least a first and second metal block are made available, the limit of elasticity under compression of...
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8094062 |
Fore/aft looking airborne radar
An antenna system for an airborne radar system with a dorsal unit having two opposing long sides extending in a height direction (Z) and a longitudinal direction (X), and two opposing short sides...
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8082052 |
Method and apparatus for ensuring the dimensional constancy of multisegment physical structures during assembly
Methods and apparatuses for ensuring the dimensional constancy of multisegment physical structures, in particular aircraft structures, during assembly are disclosed. The method includes setting up...
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8049148 |
Missile airframe and structure comprising piezoelectric fibers and method for active structural response control
Embodiments of a missile, an airframe and a structure comprising piezoelectric fibers and a method for active structural response control are generally described herein. In some embodiments, a...
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8042767 |
Composite fabric with rigid member structure
A composite structure is provided including a first fabric and a second fabric. A substantially elongate and substantially rigid first member is spaced apart from and coupled with the first fabric...
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8043704 |
Layered, transparent thermoplastic for flammability resistance
A layered material for use in transparent, flame resistant components couples a thin, fire resistant outer polymeric film to a thicker, transparent inner polymeric material. The resultant...
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8033502 |
Modular aircraft interior configuration and methods
Modular configuration for an aircraft interior floor plan design is provided by an fuselage having starboard and port side attachment rails disposed longitudinally parallel to one another. Each of...
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8028955 |
Landing gear casing provided with a box structure
A reduced-volume landing gear casing for the landing gear of an aircraft including a box structure to which the landing gear is fixed and which takes up the loads acting thereon. The box structure...
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8016233 |
Aircraft configuration
An aircraft configuration that may reduce the level of noise, infrared radiation, sonic boom, or combination thereof directed towards the ground from an aircraft in flight. In accordance with an...
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8016230 |
Fastner-free primary structural joint for sandwich panels
Techniques for providing fastener-free primary structural joint for sandwich panels are disclosed. In one embodiment, a technique includes positioning a first panel having a first edge portion...
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7997529 |
Compliant panel for aircraft
A pressurized bulkhead or panel for an aircraft includes an energy absorbing skin that deforms in response to an object strike that imparts at least a threshold amount of impact energy to the skin....
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7997530 |
Airplane fairing panel adjustable fitting assembly, kit and method
An airplane fairing panel adjustable fitting assembly allows for installation and removal of a fairing panel from outside the fairing. Blind retention features are provided and a pivoting link...
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7987596 |
Method for installing a collapsible mobile platform interior structure
A method for installing an interior structure for a mobile platform is provided. The method includes carrying a lightweight collapsible frame through a man-door of a mobile platform while the...
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7984874 |
Flexible cable connection to monuments inside of an aircraft cabin
A flexible cable connection for connecting the monuments to an on-board supply device, which cable connection ensures that displacement of the monument in longitudinal direction of the aircraft...
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7975958 |
Modular articulated-wing aircraft
Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are...
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7967248 |
Rib element and composite flange for aircraft
A rib element for aircraft and a composite flange for use in aircraft. The rib element (24) and the composite flange (14), manufactured from a composite material, comprise at least two elongated...
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7938362 |
Airplane floor assembly
The invention relates to airplane floor assemblies and to methods for their assembly. In one embodiment, an airplane comprises at least one fuselage section and at least one floor section. At least...
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7903019 |
Protective device and protective measure for a radar system
A protective device and protective measure for a radar system is provided that includes an active countermeasure by using passive emitter and/or decoys. Decoys are thereby utilized that function...
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7893390 |
Guided missile
A guided missile has a sensor unit, a propulsion unit, and a payload unit. A missile casing forms the outer contour, extends along a longitudinal direction, and accommodates the sensor unit, the...
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7890222 |
Mechanical flight control auxiliary power assist system
A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and an assembly for connecting the...
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7885056 |
Center instrument pedestal display
According to one embodiment, a center pedestal display includes a plurality of mounting faces, one or more display switches, and a screen. The plurality of mounting faces include a first mounting...
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7866603 |
Methods and apparatus for an aircraft lavoratory
A handicapped-accessible aircraft lavatory includes a wheelchair region, a toilet assembly adjacent to and oriented at a non-zero angle with respect to the wheelchair region, and a sink assembly...
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7854409 |
Canarded deltoid main wing aircraft
Canarded deltoid main wing aircraft idea allows for design of large supersonic civil and military aircraft with cruising speeds of up to Mach 3 at the altitude of over 25,000 meters. The fuel...
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7845594 |
Helicopter collapsible deck
A helicopter collapsible deck having at least one longitudinal member and at least one cross member, which extend respectively in a first and second direction intersecting at a point; the cross...
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7798444 |
Landing gear system and load distribution
In one embodiment, an aircraft comprises a plurality of hoop frame support members and a landing gear enclosure comprising a curved surface. The plurality of hoop frame support members abut against...
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7793884 |
Deltoid main wing aerodynamic configurations
“T-tailed Deltoid Main Wing” idea allows for design of high-subsonic passenger aircraft with a capacity between 200 and 650 passengers with outer dimensions fitting within 80 m box on class VI air...
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7792614 |
Apparatus and method suitable for measuring the global displacement or load on an aircraft component
The load on an aircraft component is measured. In one embodiment, the system is a contactless, all-weather displacement measuring system including a processing unit and a plurality of pairs of...
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7789339 |
Modular articulated-wing aircraft
Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are...
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7753312 |
Lightweight structure especially for an aircraft and method for making such a structure
A fiber reinforced strip is adhesively bonded to an outwardly facing surface of a reinforcing frame and to an inwardly facing outer skin surface. Such a strip position reduces crack propagation in...
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7740202 |
Wing structure for aircraft
In a wing structure for an aircraft, a rib extends in a chord direction for connecting spars to each other with upper and lower stringer through holes through which stringers of skins pass being...
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7682682 |
Stiffener stop with staggered slopes and panel fitted with such a stop
The object of this invention is a stiffener stop in particular for a primary structural panel of the “skin+stiffener” type for aircraft, said stop consisting of an initial slope connected to the...
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7677496 |
Stringer for an aircraft wing and a method of reinforcing thereof
The present invention relates to a stringer for an aircraft wing and a method of reinforcing such a stringer in which the stringer is formed with a substantially lambda shaped section.
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7668627 |
Mechanical flight control auxiliary power assist system
A mechanical flight control system for a rotary-wing aircraft is disclosed. The flight control system comprises an upstream portion, a downstream portion, and a booster means for connecting the...
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7657988 |
Method and apparatus for manufacturing interchangeable and replaceable parts
A manufacturing method and apparatus is disclosed, whereby a specific production process is used in conjunction with a specific tooling methodology to provide a tooling process package that is...
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7644888 |
High-speed aircraft and methods for their manufacture
A high-speed transport aircraft. In one embodiment, the aircraft includes a fuselage, delta wings, and integrated engine nacelles. The fuselage is configured to carry a payload and has a forward...
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7641146 |
Aircraft nose landing gear enclosure
In one embodiment, an aircraft comprises a plurality of hoop frame support members and a landing gear enclosure comprising a curved surface. The plurality of support frame support members abut...
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7621482 |
Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections
An aircraft fuselage includes a tubular shell having a centerline axis, opposite ends, and a cross-section having a radius R(φ), where φ is the angular coordinate of a cylindrical coordinate s...
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7618008 |
Air supply for an aircraft
Nowadays in aircraft on-board inert gas generation systems (OBIGGS) are used to generate inert gases. Cooled bleed air of engines or auxiliary turbines is fed to said OBIGGS systems. According to...
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7581697 |
Design methods and configurations for supersonic aircraft
Methods for configuring aircraft that may be implemented to integrate aircraft sonic boom constraint requirements with the design process for a supersonic aircraft, for example, to reconcile a...
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7578477 |
Internal security door for an aircraft
This door consists of: an internal structure (16) in which at least two compartments are executed;a panel (18) mounted in each of the compartments, andholding means of each panel (18) in the...
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