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Embraer S a patents

Recent patent applications related to Embraer S a. Embraer S a is listed as an Agent/Assignee. Note: Embraer S a may have other listings under different names/spellings. We're not affiliated with Embraer S a, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "E" | Embraer S a-related inventors

Continuous belt conveyor monitoring systems and methods

An online real-time method of measuring the thickness of a moving belt uses infrared thermography technology to continuously and noninvasively measure the thickness of rubber cover regions and detect damage. This technique solves technical problems and realizes potential gains such as increased efficiency in planning maintenance/replacements of conveyor belts; provides... Embraer S a

Automated system and method to manufacture aeronautic junction parts

Every junction part for an airplane wing is manufactured with overmaterial. Each part is measured with a laser based interferometer or other scanning technique and the “as built” measurements are compared with a model to generate a new trajectory milling program to fill or prevent gaps between parts using a... Embraer S a

Enhanced take-off system

An automatic takeoff flight control system provides takeoff speed reduction to thereby reduce the takeoff distance (TOD) and, as a consequence, increase the takeoff weight (TOW); sets the horizontal stabilizer (HSTAB) in a non-trimmed condition—named “mistrim”; and provide best beta for optimum climb at takeoff, through lateral-directional surfaces commands.... Embraer S a

Deflection mechanism of the flap panels of an aircraft

Describes a deflection mechanism of the flap panels of an aircraft, the aforesaid deflection mechanism being connected to a wing of an aircraft by means of a first fixed structure and to the flap panels by linkage points, in order to support and deflect the flap panels in desired positions,... Embraer S a

Side-facing belted aircraft seats

Side-facing belted aircraft seats include a tactile signaling unit to induce movement of the seat occupant. For such purpose, the signaling unit may be provided with a signaling lid covering a female buckle of a lap belt restraint assembly. The signaling lid is moveable between a closed position wherein engagement... Embraer S a

Aircraft air conditioning system airflow regulation

An air conditioning system for an aircraft regulates the extracted engine bleed airflow by assessing a plurality of parameters that indicate the actual aircraft operating conditions, external environment and system performance capabilities, aiming at substantially reducing the demand of extracted engine bleed air (fuel consumption reduction) and concurrently complying with... Embraer S a

Fiber metal laminate reinforced wing spar for retractable underwing mounted landing gear assemblies

Reinforced wing spars for underwing mounted retractable landing gear assemblies include a unitary (one-piece) metal wing spar having a central web and an upper spar flange, a trunnion mounted in the web of the wing spar for pivotally receiving a transverse mounting tube of a retractable landing gear strut, and... Embraer S a

Use of automatic pitch control to improve braking performance

A flight control law enhances braking efficiency through the operation of aircraft elevators (or another pitch control system) using measured longitudinal acceleration and/or pedal position as references to the control law. Through this solution, it is possible to increase the vertical load in the main landing gear and consequently enhance... Embraer S a

Short rejected takeoff system and method

The disclosed non-limiting embodiment provides important improvements in aircraft performance in short rejected takeoff systems by automatically detecting whether the speed of the aircraft does not exceed Vshort, where Vshort>V1; automatically detecting whether one of said plural engines has failed during takeoff while the aircraft is still in contact with... Embraer S a

Automated process for manufacturing items of furniture in an integrated manufacturing cell and integrated cell for manufacturing items of furniture

Patent of invention for “automated process for manufacturing items of furniture in an integrated manufacturing cell and integrated cell for manufacturing items of furniture”. There is described an automated process for manufacturing items of furniture in an integrated manufacturing cell, the process comprising the following steps: a) Initial machining of... Embraer S a

Variable angular compression seal assemblies for moveable aircraft components

Variable angular compression seal assemblies are disclosed that may usefully be employed to seal movable aircraft components, e.g., so as to seal a flap torque tube operating in a flap track cutout opening in a wing to fuselage fairing. The seal assembly may be provided so as to seal a... Embraer S a

Structural health monitoring system with the identification of the damage through a device based in augmented reality technology

An inspection system for assessing and visualizing structural damage to a structural platform comprises sensors operatively coupled to the structural platform that assess structural damage to or failure of the structural platform. A structural health monitoring processor operatively coupled to the sensors determines structural damage in response to the sensors.... Embraer S a

Quick connection assemblies especially useful for coupling aircraft antenna fairings to airframe structures

Aircraft antenna fairing assemblies include a fairing shell and connection components for positionally fixing the fairing shell to airframe structure of an aircraft. The connection components may comprise a guide assembly having a guide head and a receiver defining a guide channel for receiving the guide head therewithin, and a... Embraer S a

A mounting inserts and a device for mounting inserts

There is described a method of mounting inserts, comprising the following steps: (i) Application of an adhesive film on one of the faces of an inserts tray (223) covering a plurality of through-holes (241) and respective depressions (242); (ii) Insertion of an insert (230) in each through-hole (241) of the... Embraer S a

Asymmetry-proof multi-engine aircraft

An aircraft compensates for asymmetry of engine failure by drawing part of the energy produced by the still-operating engine to generate thrust at the tip of the opposite wing. For example, the left engine drives its own thrust on the left wing, but a portion of the energy the left... Embraer S a

Landing distance monitor

The non-limiting method and device presented herein minimizes the risks of a landing overrun and increases flight crew situational awareness. To accomplish these goals, the system actuates in the approach and landing phases returning automatic alerts to the flight crew when necessary.... Embraer S a

Lightning protection for aircraft fuselage fuel tank ventilation lines

Lightning protected vent lines associated operatively with aircraft fuselage fuel tanks (i.e., on-board fuel tanks that are not physically located in an aircraft's wing but instead are physically located within the aircraft's fuselage structure) are provided which include a vent conduit, a coupling at a proximal end of the vent... Embraer S a

Retractable self-aligning aircraft stablizer strut assembly and aircraft including the same

Self-aligning retractable strut stabilization assemblies that are ground engageable in use are provided to stabilize a vehicle, e.g., a cargo aircraft during loading/unloading operations. The strut stabilization assembly may be on-board equipment associated with an aircraft that may be actuated (e.g., via on-board hydraulic and/or electric actuation systems) by the... Embraer S a

Longitudinal lock device for cargo in aircraft, safety trigger for longitudinal lock device

There is described a longitudinal lock device for cargo in aircraft endowed with a locking box which is fastened beneath the floor of an aircraft, the longitudinal lock device for cargo in aircraft comprising a locking latch associated to the cargo and coupled to a bar mechanism disposed inside the... Embraer S a

Aircraft access door and aircraft

It further describes an aircraft provided with an access door, particularly a boarding and landing access door, arranged centrally on a fuselage portion of the aircraft and perpendicularly to a longitudinal axis of the aircraft.... Embraer S a

Composite accoustical panels especially useful for interior panel assemblies of aircraft passenger cabins

Composite acoustic panels are provided which may usefully be employed for aircraft interior panel assemblies. The composite acoustic panels may include a core member defining opposed surfaces, and a pair of exterior face sheets each attached to a respective one of the opposed surfaces of the core member. At least... Embraer S a

Optimized aircraft pylon fairing

Pylon fairings for an aircraft turbojet engine mounted below an aircraft wing are provided with inboard and outboard lateral faces which converge rearwardly to form a trailing edge of the pylon fairing and which are positioned so as to contact a portion of a cold flow exiting a fan duct... Embraer S a

Method and protecting aircraft maximum lift capability

An aircraft automatic control system protects structural parameters of an aircraft based on angle of attack protection by use of maximum allowed angle of attack values as a function of dynamic pressure or a combination of parameters that permit computation of dynamic pressure. Example techniques herein limit the wing lift... Embraer S a

Assemblies and methods for reconfiguring aircraft fuselage doors

Assemblies and methods are provided to allow a temporary alternate door (e.g., an observation door for use during search and rescue (SAR) missions) may be placed in a fuselage opening normally closed by a dedicated personnel door. The assembly may be provided with a central support pole attachable to interior... Embraer S a

Integrated environmental control controlling environmental temperature of an enclosed space

Environmental control systems and methods to control environmental temperature of an enclosed space by integrating a passive heat exchange subsystem (e.g., a loop heat pipe (LHP) heat exchange subsystem) having a closed loop heat exchange fluid circuit in heat-exchange relationship with the enclosed space for providing environmental temperature control therewithin,... Embraer S a

Aircraft engine pylon to wing mounting assembly

Pylon mounting assemblies are provided for mounting an engine (e.g., a turbojet engine) to a wing of an aircraft. The pylon mounting assemblies include an upper pylon connection member, and a lower pylon connection box, wherein the upper pylon connection member and the lower pylon connection box respectively include multiple... Embraer S a

Aircraft engine pylon to wing mounting assembly

Pylon mounting assemblies are provided for mounting an engine (e.g., a turbojet engine) to a wing of an aircraft. The pylon mounting assemblies include an upper pylon connection member, and a lower pylon connection box. The upper pylon connection member and the lower pylon connection box respectively define opposed lower... Embraer S a

Method and system for maintenance services planning and scheduling optimization

Field services management applicable to industries where the need to define, plan, schedule, coordinate and/or accomplish a number of activities, interventions and maintenance demands is present. Applications include mining, oil and gas, chemical, automotive, aeronautical and others where maintenance planning is considered a challenge. Application to services companies such as... Embraer S a

Aircraft landing gear door actuation mechanism with integrated emergency actuation assembly

Landing gear doors may be opened in an emergency event, e.g., a failure of the normal landing gear actuation system that requires a gravity free-fall deployment. The retractable aircraft landing gear door actuation mechanism will include a landing gear door and a door support bracket attached to the landing gear... Embraer S a

Structural health monitoring sensory system integrated to a self-adapting morphing system

A system and method for damage detection and for evaluating the real operation conditions for structural platforms using structural health monitoring is integrated to a system and method that permits for the platform to provide a flexible geometric control considering a self-adapting morphing which is capable of providing better operating... Embraer S a

Aircraft throttle quadrant with a gust lock lever system provided with a selectable safety stop

A gust lock lever system associated with an aircraft throttle quadrant allows flight crew to freely choose which engine to use for ground taxing operations. A stop member is connected to a crossbar of the gust lock lever system for moveable positioning into alignment with a respective one of the... Embraer S a

Airframe wing spar structures with contiguous unitary and integrally fastened upper and lower chord sections

An aircraft wing is provided having a spanwise wing spar which includes a one-piece upright central web extending in a spanwise direction between inboard and outboard ends of the wing spar, and a plurality of contiguously adjacent wing spar sections. At least a first wing spar section includes at least... Embraer S a

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This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. is not affiliated or associated with Embraer S a in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Embraer S a with additional patents listed. Browse our Agent directory for other possible listings. Page by