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US20130306796 |
OUTER FUEL TANK ACCESS COVER, WING AND AIRCRAFT DESCRIPTION
The present invention describes an outer fuel access tank cover (FTAC) of an aircraft, a wing comprising such outer FTAC of an aircraft and an aircraft. The invention belongs to the field of... |
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US20120318921 |
FIRE PROTECTION SYSTEM, AIRCRAFT OR SPACECRAFT AND A METHOD FOR CONFINING AND SUPPRESSING A FIRE
The invention provides a fire protection system, in particular in the field of aviation and aerospace, comprising a compartment which is at least partly lined with fire-retardant material, a... |
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US20150246734 |
SYSTEMS AND METHODS FOR CONTAINING IGNITION WITHIN EQUIPMENT DRY BAYS
An equipment dry bay is provided. The equipment dry bay includes at least one partition that subdivides the equipment dry bay into a plurality of compartments, wherein the at least one partition... |
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US20120273618 |
Burnthrough Protection System
A burnthrough protection system including a fire protection laminate and a foam insulation material, wherein the fire protection laminate includes a fire barrier layer and a buffer layer, the... |
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US20110079683 |
SAFETY SYSTEM FOR REDUCING THE EXPLOSION RISK OF A FUEL TANK
A safety system for reducing the explosion risk of a fuel tank comprises at least one fluid source and at least one fluid container with an inlet and an outlet for a fluid, wherein the fluid... |
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US20140252171 |
NITROGEN BUBBLER SYSTEM IN FUEL TANK AND METHOD
An assembly of fuel tank and bubbler system comprises a fuel tank defining a storage volume adapted to receive fuel therein. The fuel tank comprises at least one fuel inlet, at least one fuel... |
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US20150197346 |
LIQUID DRAINAGE INSTALLATION FOR A ROTORCRAFT ENGINE COMPARTMENT
An installation for draining liquid away from an aircraft engine compartment. Said drainage installation comprises a collector for collecting said liquid and provided with an opening putting the... |
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US20150232193 |
AIRCRAFT SAFETY DEVICE
The present invention provides an aircraft safety device which can reliably prevent explosion of a fuel tank even if an inflammable gas is ignited. A safety device for explosion-proofing a fuel... |
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US20110133033 |
INERT GAS DISTRIBUTION ARRANGEMENT
An example inert gas distribution arrangement includes a first fuel tank and a second fuel tank mountable to an aircraft outboard the first fuel tank. A distribution conduit is configured to... |
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US20140166810 |
Profiled Strip As A Fire Indication Device In An Aircraft
A door for a storage compartment of an aircraft includes a door leaf and a profiled strip connected to an edge of the door leaf. The profiled strip includes openings that provide a path for gas... |
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US20100108811 |
SYSTEM AND METHOD TO MAKE A FUEL TANK INERT
A fuel tank safety system includes an ullage cooling assembly and a system controller. The ullage cooling assembly includes a compressor configured to extract a quantity of ullage gas from the... |
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US20150246731 |
ENGINE PYLON OF AIRCRAFT AND AIRCRAFT
An engine pylon of an aircraft that is used for supporting an engine of an aircraft on a main wing, the pylon including a first drain that discharges a flammable liquid leaking from a pipe... |
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US20080061189 |
Fireproof bulkhead of a highly porous structure with intumescent coating and method for its production
The present invention provides a fireproof bulkhead, having a highly porous structure with an intumescent coating, the highly porous structure being formed as a reticulated foam or as a highly... |
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US20110042515 |
ARRANGEMENT FOR PROVIDING ACTIVE FIRE PROTECTION IN AIRCRAFT
The invention relates to an arrangement for providing active fire protection in aircraft by means of at least one protective shield. According to the invention, the at least one protective shield... |
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US20110147524 |
FIRE DETECTION SYSTEM AND METHOD FOR CONFIGURING A FIRE DETECTION SYSTEM
The invention relates to a fire detection system comprising one or several fire sensors, in which fire detection system a monitoring unit communicates with the fire sensors and by way of a... |
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US20130206910 |
EMERGENCY SUPPLY SYSTEM FOR A TRANSPORTATION MEANS, METHOD FOR SUPPLYING ELECTRICAL POWER AND FOR INHIBITING FIRE AND AIRCRAFT WITH AN EMERGENCY SUPPLY SYSTEM
An emergency supply system for a transportation means is provided. The system includes at least one fuel cell, a hydrogen tank, an oxygen tank, an extinguishing agent container, an oxidant supply... |
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US20060214056 |
Mattress for aircraft
A mattress for use in aircraft includes a lying surface and a low-flammability foam core. The foam core has, on the side facing the lying surface, a large-area recess which occupies at least 70%... |
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US20080290216 |
Method for Extinguishing Fire in Aircraft Compartment
The inventive method for extinguishing fire in an aircraft cargo compartment (3) consists in injecting a substantially pure nitrogen from high-pressure storage cylinders (12), in simultaneously... |
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US20130187004 |
Fire protection device for aircraft
A joint attaching a structural element to a composite part comprising a metallic attachment, this joint being subjected to a fire source on one of its sides, the fire side. The joint comprises a... |
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US20090134276 |
Aircraft firewall
The present invention relates to an aircraft firewall (12) separating first and second compartments (1 and 2) of said aircraft, said first compartment (1) containing a plurality of elements. The... |
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US20120012709 |
FIRING PREVENTION STRUCTURE OF FUEL TANK
A firing prevention structure of a fuel tank is provided with a double sleeve to pass through a hole formed in a rib, and a supporting structure to support a pipe to pass through the double... |
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US20110121133 |
BURN THROUGH RESISTANT AIRCRAFT FUSELAGE
The invention relates to an aircraft fuselage (12) comprising at least one space arranged in the aircraft fuselage and at least one wall (16). According to the invention, the wall resists... |
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US20120148824 |
Green Aircraft Interior Panels
The present invention relates to sandwich panels used as aircraft interior parts. In addition to provide a finishing function, the sandwich panels need to have certain mechanical properties and... |
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US20100163669 |
Super aircraft structrue
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear small wings, vertical winglets, and four levels. The fuselage has a cross-section... |
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US20140138487 |
RETRACTABLE INFILL PANEL FOR HIGH-LIFT DEVICE
The present invention provides an aircraft assembly with a fixed structure and a high-lift device. The fixed structure has a spar, a forward part which provides a foremost edge of an aircraft... |
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US20100170991 |
Low Weight Carpet Tile
Low weight and non-square carpet tile suitable for use in mass transit vehicles, particularly passenger aircraft. The carpet tile preferably weighs less than about 82 ounces per square yard. The... |
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US20140353427 |
FIRE EXTINGUISHING SYSTEM FOR AN AIRCRAFT
The invention relates to a system for extinguishing and preventing a fire on board of an aircraft. According to the invention, an aircraft is equipped with an On-Board-Inert Gas Generating-System... |
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US20070164160 |
Support device for fire-detection system
The invention relates to a support device which is designed to be installed between an aircraft engine and an associated thrust reverser, said device being equipped with a support means which can... |
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US20110240798 |
Automated Fire and Smoke Detection, Isolation, and Recovery
Technologies are described herein for detecting and recovering from a fire event within an aircraft. The technologies receive sensor data from a number of sensors associated with an aircraft. A... |
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US20100253528 |
SMOKE DETECTOR WITH INCLUDED FLAME BARRIER
A smoke detector comprises a first housing to face an area in which to detect smoke, a second housing secured to the first housing, electronics to detect smoke within the area, and a flameproof... |
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US20120104162 |
PYLON ARRANGEMENT FOR OPEN STRUCTURE
An aircraft pylon is disclosed, the pylon including a strut, a modular fluid containment structure and a modular firewall. The strut presents an open structure and connects an aircraft external... |
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US20100001135 |
Retaining Device
A retaining device includes a fireproof core enclosed by a non-fireproof case, wherein a pre-tensioned fireproof device is integrated in the case and attached to the core. The fireproof device... |
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US20170166294 |
INCOMBUSTIBLE, NON-TELEGRAPHING SUBSTRATES FOR AVIATION PANEL ASSEMBLIES AND METHODS FOR INSTALLING THE INCOMBUSTIBLE, NON-TELEGRAPHING SUBSTRATE INTO AN AVIATION PANEL ASSEMBLY
An incombustible, non-telegraphing substrate for facing with a decorative aviation veneer is provided. The incombustible, non-telegraphing substrate comprises a backing layer comprising a polymer... |
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US20170073059 |
BURNTHROUGH PROTECTION SYSTEM
A burnthrough protection system including a fire protection laminate and a foam insulation material, wherein the fire protection laminate includes a fire barrier layer and a buffer layer, the... |
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US20170056694 |
METHODS, SYSTEMS AND APPARATUS FOR LINING AN AIRCRAFT CARGO COMPARTMENT
Methods, systems and apparatus for lining an aircraft cargo compartment are disclosed. An example apparatus includes a liner having a fire-resistant composite layer to provide flame-penetration... |
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US20160229548 |
INERTING SYSTEM AND METHOD FOR AN AIRCRAFT USING EXHAUST AIR
An inerting system for an aircraft includes an inert gas generation apparatus, an air supply line, a compressor and an inert gas line. The compressor supplies the inert gas generation apparatus... |
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US20160200447 |
Fuel Cell System for an Aircraft and Method for Providing an Inert Gas in an Aircraft
A fuel cell system for an aircraft includes at least one fuel cell having a first inlet for providing a fuel, a second inlet for providing an oxidant, an outlet for removing exhaust air and a... |
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US20150360795 |
Fire Seal for an Aircraft
A seal including an acute bend having a first end portion and a second end portion, a first engagement extension extending from the first end portion of the acute bend, and a second engagement... |