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Document |
Document Title |
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US20150073628 |
HELICOPTER SYSTEM AND METHOD FOR INTEGRATING COLLECTIVE FLIGHT DIRECTOR CUES
A system and method are provided for integrating and displaying the collective cue and the pitch and roll cue of a helicopter display with a flight path marker providing a moving reference showing... |
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US20130325218 |
SYNTHETIC ESTIMATION OF ROTORCRAFT AIRSPEED
A method for estimating airspeed of an aircraft includes receiving values indicative of operating conditions of the aircraft along an axis; estimating a tip path plane (TPP) angle along the axis... |
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US20110029164 |
AVIATION YOKE HSI INTERFACE AND FLIGHT DECK CONTROL INDICATOR AND SELECTOR SAFETY SYSTEM
An aviation yoke HSI interface and flight deck control indicator and selector safety system enhances flight safety. The system incorporates a multi-controlled HSI with a yoke heading adjustment... |
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US20110213514 |
AVIATION YOKE HSI INTERFACE AND FLIGHT DECK CONTROL INDICATOR AND SELECTOR SAFETY SYSTEM
An aviation yoke HSI interface and flight deck control indicator and selector safety system enhances flight safety. The system incorporates a multi-controlled HSI with a yoke heading adjustment... |
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US20100332057 |
FLIGHT INFORMATION REMINDER SYSTEM AND METHOD
A flight information reminder system includes a computer system maintaining updated flight information about a flight having a duration. The computer system is adapted to issue messages to... |
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US20110160940 |
Text Flight Service Station
A method and system (i.e. Text Flight Service Station) to provide up to date weather information, pilot information and flight plan information for small aircraft pilots, particularly, those... |
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US20110121127 |
POWER PLANT, A HELICOPTER INCLUDING SUCH A POWER PLANT, AND A METHOD IMPLEMENTED BY SAID POWER PLANT
The present invention relates to a power plant (10) having a single engine (13) together with both a main gearbox (MGB) suitable for driving the rotary wing (3) of a helicopter (1) and a tail... |
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US20110208376 |
ON-BOARD FLIGHT STRATEGY EVALUATION SYSTEM ABOARD AN AIRCRAFT
The invention relates to a process and an on-board system for evaluating flight strategies aboard an aircraft, linked with a flight plan (13) of the aircraft, including: calculation means (5) for... |
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US20150012155 |
AIRCRAFT COMPRISING A MEASURING PROBE AND METHOD FOR DETERMINING FLIGHT PARAMETERS OF SUCH AN AIRCRAFT
The invention relates to an aircraft including a fuselage and a first measuring probe including means for measuring the local incidence, means for measuring the static pressure, and optionally... |
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US20110282524 |
SYSTEM AND METHOD FOR DETECTING WAKE TURBULENCE OF AN AIRCRAFT
System for detecting wake turbulence (SDWT) of a first aircraft, which can be embedded onboard a second aircraft, comprising: first means (DET1) for determining the roll (Roll2) of the second... |
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US20150219512 |
METHOD OF AND SYSTEM FOR CALCULATION AND CONSOLIDATION OF FLIGHT PARAMETERS OF AN AIRCRAFT
A method and system for calculation and consolidation of a first plurality of aircraft flight parameters including a second plurality of pressure sensors is provided. The pressure sensors are... |
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US20130218373 |
Method and System For Highlighting a Flight Path Deviation of an Aircraft
A method and system for highlighting a flight path deviation of an aircraft to a user in a multi-parameter aircraft instrument display, such as a flat panel display. A visibility attribute is... |
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US20100312421 |
DEVICE FOR ASSISTING IN PILOTING A HYBRID HELICOPTER, A HYBRID HELICOPTER PROVIDED WITH SUCH A DEVICE, AND A METHOD IMPLEMENTED BY SAID DEVICE
A piloting assistance device for a hybrid helicopter is provided with a rotary wing, two half-wings (8′, 8″) provided respectively with first and second propellers (6′, 6″), and an engine... |
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US20150142224 |
METHOD AND SYSTEM FOR DISPLAYING METEOROLOGICAL EVENTS ALONG A FLIGHT PLAN OF AN AIRCRAFT
Method and system for displaying meteorological phenomena encountered by an aircraft flying along a flight plan. The display system includes a display device configured to present on a screen a... |
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US20130046423 |
SYSTEM AND METHOD FOR AIRCRAFT THERMAL CAPACITY PREDICTION
A technique for identifying, projecting, displaying, and enhancing the thermal capacity for an aircraft is disclosed wherein the thermal capacity is defined as the amount of time or range the... |
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US20150247953 |
SYSTEMS AND METHODS FOR PREDICTING ARRIVAL OF WIND EVENT AT AEROMECHANICAL APPARATUS
A method for predicting arrival of a wind event at an aeromechanical structure includes sensing wind velocity in an atmospheric volume moving towards the aeromechanical structure to obtain a time... |
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US20140249701 |
SYSTEM AND METHOD FOR MANAGING AN INTERVAL BETWEEN AIRCRAFT
A system and method provide situational awareness for a pilot of an ownship in managing the longitudinal interval from an aircraft from which the ownship is following and maintaining the ownship... |
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US20110295569 |
WIND ESTIMATION FOR AN UNMANNED AERIAL VEHICLE
The speed of the wind during operation of a UAV is estimated. In one example the speed of the wind is estimated by modeling an acceleration of an unmanned aerial vehicle (UAV) based on a measured... |
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US20090177343 |
SYSTEM AND METHOD FOR SELECTABLE WEATHER OBJECT DISPLAY
Systems and methods for presenting information pertaining to a weather object on a display. A process includes displaying on the aircraft display terrain information, weather reflectivity... |
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US20140067171 |
SYSTEMS AND METHODS FOR GRAPHICALLY INDICATING AIRCRAFT ASCENT AND DESCENT CAPABILITIES
Systems and methods are operable to present graphical information indicating capability of an aircraft to change altitude. An exemplary embodiment determines an altitude change capability of the... |
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US20130282207 |
Fully Parametrizable Electronic Alerts and Procedures Management System, Intended for an Aircraft
An alerts and procedures management system for an aircraft comprises a software kernel aboard the aircraft and a parameterization tool for the software kernel, which comprises a conversion module... |
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US20130289804 |
SYSTEM AND METHOD FOR ECONOMIC USAGE OF AN AIRCRAFT
The present application relates to a system and method for providing real-time indications of economic impact of aircraft operations to an aircraft operator. The system and method allow the... |
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US20130325220 |
PROCEDURE AND DEVICE FOR THE DETERMINATION OF AIRSPEEDS OF A ROTORCRAFT IN STATIONARY FLIGHT AND/OR AT LOW SPEEDS
A procedure and a device for the determination of current airspeeds [13] of a rotorcraft [2] in a stationary flight regime and/or at low speeds. A calculation system [1] incorporates two pairs of... |
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US20140330458 |
METHOD AND SYSTEM FOR DETERMINING AN AIRSPEED OF AN AIRCRAFT
A method and system for determining an airspeed of an aircraft, known as assisted aircraft, comprises: a) determining a position; b) measuring a ground speed; c) receiving a plurality of messages... |
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US20150088342 |
SYSTEM AND METHOD FOR PROCESSING AND DISPLAYING WAKE TURBULENCE
A system and method to display, when within an envelope of an ownship's flight path, a symbol representing wake turbulence from another aircraft based on aircraft type and flight parameters... |
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US20110082605 |
AIRCRAFT PILOTING ASSISTANCE METHOD AND CORRESPONDING DEVICE
An aircraft piloting assistance method and system including determining at least one flyable slope with which the aircraft is assumed to be able to fly, based on a value of at least one flight... |
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US20110098871 |
METHOD AND APPARATUS FOR UPDATING WINDS ALOFT DISPLAY AS AIRCRAFT ALTITUDE CHANGES
A method and apparatus are provided for displaying wind magnitudes and directions aloft as the aircraft (202) changes altitude. Wind magnitudes and directions at a plurality of locations (232) at... |
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US20110077804 |
AIRSPACE AWARENESS ENHANCEMENT SYSTEM AND METHOD
A display system and method for an aircraft renders various airspaces and associated airspace types on an aircraft display device. An image is selectively rendering on the aircraft display device... |
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US20150134154 |
SYSTEM FOR ACTIVATING THE DISTRESS BEACON OF AN AIRCRAFT
A system for activating the distress beacon determines a positional difference between a theoretical position of the aircraft determined from data of the flight plan and a real position of the... |
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US20080167764 |
ICE RATE METER WITH VIRTUAL ASPIRATION
A system and method of determining an actual liquid water content (Actual LWC) with an ice rate meter probe without aspiration. |
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US20150169273 |
PERIPHERAL VISION HOVER DRIFT CUEING
Peripheral vision hover drift cueing methods, systems and computer readable media are disclosed. For example, a system can include one or more sensors, and a peripheral vision hover drift cueing... |
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US20130325219 |
METHOD AND DEVICE FOR AUTOMATICALLY ESTIMATING A DEGRADATION IN FUEL CONSUMPTION AND IN DRAG OF AN AIRCRAFT
A method and device for automatically estimating a degradation in fuel consumption and in drag of an aircraft. The device comprises a device for calculating a numerical value of the effect of a... |
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US20130184902 |
PILOTING ASSISTANCE METHOD, A PILOTING ASSISTANCE DEVICE, AND AN AIRCRAFT
A piloting assistance device (5) comprising a calculation unit (10) and a display unit (20). The calculation unit (10) executes stored instructions to determine at least one thrust margin for a... |
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US20130073124 |
Method and Device for Protecting an Aircraft
A method and a device for protecting an aircraft in the flight phase, said aircraft exhibiting several configurations of slats and flaps, comprises the following steps: determining, for at least... |
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US20100198433 |
Flight Management System with Optimization of the Lateral Flight Plan
Flight management system for aircraft comprising computation means capable of determining a gain or a loss in terms of flight time remaining to a point of arrival, and in terms of fuel... |
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US20130066487 |
FLIGHT OPERATIONAL CONSEQUENCES SYSTEM
According to an embodiment, a method provides flight operational consequence information by receiving a status indication associated with an aircraft component at a processing device in the... |
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US20100057275 |
PRESENTING WEATHER INFORMATION ON A DISPLAY
A method is present for presenting weather information. A number of weather conditions for a geographic region is identified from weather data for the geographic region. A geometry is selected for... |
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US20130245860 |
SITUATIONAL AWARENESS PILOT BRIEFING TOOL
Embodiments of the present invention relate to a system and method for better conveying information to a pilot and/or other members of a flight crew present on the flight deck of an aircraft.... |
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US20100010695 |
HEADING REFERENCE SYSTEM WITH REMOTE-MOUNTED SENSOR
A navigation system for an aircraft includes one or more wing-mounted sensors whose outputs are effected by the flexing of the wing during flight. The navigation system corrects for these errors... |
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US20150019050 |
METHOD AND DEVICE FOR DISPLAYING IN REAL TIME A PITCH INSTRUCTION ON AN AIRCRAFT DURING MANUAL PILOTING
A device comprising a display unit which is configured to display, on a screen of the cockpit of the aircraft, a pitch bar illustrating a pitch order and means for adapting the direct gain of the... |
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US20060265110 |
Navigation system for an aircraft and associated command process
A navigation system for an aircraft, including a calculator of an estimated flight path for the aircraft; a device for determining an estimated value of a flight parameter that corresponds to an... |
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US20130211635 |
INTERACTIVE DIALOG DEVICES AND METHODS FOR AN OPERATOR OF AN AIRCRAFT AND A GUIDANCE SYSTEM OF THE AIRCRAFT
Interactive dialog devices and methods are provided for use by an operator of an aircraft with a guidance system of the aircraft. The dialog devices and methods can include an interaction on a... |
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US20140074326 |
METHOD OF DETERMINING A TURBULENT CONDITION IN AN AIRCRAFT
A method of determining a turbulent condition in an aircraft with a handheld device where the handheld device has at least one of a gyroscope, seismometer, and an accelerometer where the method... |
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US20100004803 |
Smart recovery system
This invention relates to an intelligence system on board an aircraft that detects an emergency, assesses the situation, and then acts on the situation in a pre-determined manner. |
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US20130226376 |
SYSTEM AND METHOD FOR RENDERING AN AIRCRAFT COCKPIT DISPLAY FOR USE WITH AN IN-TRAIL PROCEDURE (ITP)
A method for rendering symbology on a cockpit display of a host aircraft, relating to a proposed ITP transition, is provided. The method comprises analyzing data to predict an ITP transition that... |
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US20140324255 |
AIRCRAFT EMERGENCY SYSTEM USING ADS-B
A safety system for an aircraft using ADS-B has a touch screen device or switch interfaced with an emergency computer, wherein the emergency computer sends an emergency signal to the ADS-B system... |
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US20140039734 |
AIRCRAFT SYSTEMS AND METHODS FOR DISPLAYING WEATHER INFORMATION ALONG A FLIGHT PATH
A display system for an aircraft is provided. The system includes a processing unit configured to receive weather information associated with a flight path of a flight plan and to generate display... |
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US20080255714 |
METHODS AND APPARATUS FOR AIRCRAFT TURBULENCE DETECTION
Methods and apparatus for an in-flight air turbulence detection system. In one embodiment, a system includes an air turbulence detector and a transmitter to transmit turbulence information. In... |
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US20140046510 |
ESTIMATING A WIND VECTOR
Methods and devices for calculating an estimate of a wind vector. A maneuver of a platform may be identified as a steady-straight motion maneuver, a partial turn maneuver, or a full turn maneuver.... |
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US20100057276 |
Method of Monitoring Atmospheric Areas for an Aircraft
The invention relates to a method and a device for monitoring risky atmospheric areas. The invention relates to an onboard device connected to meteorological measurement systems making it possible... |