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217 results about "Aircraft safety" patented technology

Aircraft Drive

ActiveUS20070282491A1Additional precision in guidingPreventing an aircraft from overbalancingAircraft stabilisationDigital data processing detailsFlight vehicleNose
The present invention describes a drive system for an aircraft involving one or more nose wheel motors. Data regarding the nose wheel rotation is used to control the ground travel of the aircraft, to predict potential problems, to provide more precise control over the aircraft, and to improve aircraft safety.
Owner:BOREALIS TECH LTD

Apparatus, system and method for aircraft security and anti-hijacking intervention

A system and method for operating an aircraft such that any hostile persons taking over the cockpit, for instance, terrorists or a disgruntled pilot, cannot control the flight path of the aircraft to enter restricted airspace, such as ‘no fly’ zones, or any authorized pilots while operating an aircraft cannot unintentionally enter any no fly zone areas.
Owner:ARNOUSE DIGITAL DEVICES

Aircraft braking early warning system

A method provides alert information, regarding an aircraft wheel braking system, to an operator of an aircraft during an aircraft landing. An input of a target deceleration rate for the landing aircraft is received prior to the aircraft having landed on a ground surface. At least one sensor electronically collects information relevant to a real-time deceleration rate of the aircraft after the aircraft has landed on the ground surface, and the real-time deceleration rate of the aircraft is calculated. The target deceleration rate is compared to the calculated deceleration rate to determine an effectiveness of the aircraft wheel braking system. A visual, audible, or tactile alert is optionally provided to the operator of the aircraft, and data from this system could also be used as an input for various other aircraft safety systems. A system for performing the method is also provided.
Owner:3RD MILLENNIUM SOLUTIONS

Integrated system for aircraft vortex safety

The invention relates to systems for preventing off-normal situations when there is a possibility that an aircraft penetrates into a dangerous area of the vortex shedding of a vortex generator. The inventive system consists of information sub-systems for recording and storing information on the expected relative position of the aircraft and trailing vortex areas in line with danger criteria which are specified by a user and concern dangerous aerodynamic forces and torques effecting the aircraft and induced by the trailing vortex of vortex generators, and for conveying said information to said user, who can be the aircraft crew and / or flight attendants, at a preventive distance from the aircraft and at a forecast moment. Said information can be visualised in a human-readable form and in a volume sufficient for forming a directive signal for carrying out a flight manoeuvre by the aircraft in order to move away from the dangerous trailing vortex area.
Owner:SPETABTEKHNIKA +1

Flight deck communication and display system

A flight deck communication and display system (100) for displaying a modified flight plan transmitted to an aircraft (224) is described including a processor (104) adapted to receive (i) data representative of a current aircraft flight plan (218, 228) and (ii) a textual message representative of the modified flight plan (218′, 228′) and operable, in response thereto, to supply a flight plan display command, and a modified flight plan display command, and comparing the textual clearance message with factors affecting aircraft safety to supply an alert message display command (204). A display (108) coupled to receive the flight plan display command, the modified flight plan display command, the alert message display command is operable, in response thereto, to substantially simultaneously display (308) (i) an image representative of the current aircraft flight plan, (ii) the textual clearance message, (iii) the modified flight plan, and (iv) an alert message indicating whether there are any safety concerns related to the textual air traffic modified flight plan.
Owner:HONEYWELL INT INC

Combination child seat and travel safety vest for wheeled luggage

An improved lightweight, portable and compact combination seat and serape' for travel ease and safety while traveling with a small child. The device is releasably attached to the telescoping handle upon wheeled luggage, is disposable in an unfolded position for use wherein it functions as a seat and when used as a serape' for travel safety is draped over the head and shoulders of the juvenile to be secured with the parent into the airline seatbelt, and when in its storage condition is separated from and compactly contained within the luggage for carry-on in an airliner or other public transportation.
Owner:MCFARLAND DAVID S +2

System and method for facilitating target aiming and aircraft control using aircraft displays

ActiveUS20060227012A1Facilitating target aimingFacilitating aircraft controlAnalogue computers for trafficNavigation instrumentsControl signalDisplay device
An improved system and method are disclosed for facilitating target aiming and aircraft control by flight crews using electronic displays. For example, an aircraft display system is disclosed that includes a database for storing target location and boundary data, a processing unit, a position and direction determination unit for use in determining the position of an aiming symbol on a display, a graphics display generator, and a visual display. The processing unit determines whether or not a selected target to be displayed is obscured or covered by the aiming symbol to be displayed. If any portion of the target is obscured or covered by the aiming symbol, then the processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of the portions of the aiming symbol that obscure or cover the target. Notably, the transparency of any symbol (or portion of a symbol) can be increased if that symbol obscures or covers a target being displayed or viewed. Thus, the visibility of targets viewed using onboard visual displays is significantly enhanced, whereby the targets are obscured by the symbols used to aim and control the aircraft. Advantageously, target aiming and aircraft control are facilitated, which reduces pilot workload and navigation errors, and thus results in increased aircraft safety.
Owner:HONEYWELL INT INC

2D + 3D large aircraft shape defect detection and analysis method based on deep learning

The invention discloses a 2D + 3D large aircraft shape defect detection and analysis method based on deep learning, and the method is characterized in that the method comprises the steps of collectinga multi-view 2D image and 3D point cloud data; obtaining a complete aircraft point cloud model through registration; extracting feature points of the image and the point cloud, and performing 2D-3D correspondence according to feature matching; estimating the pose of the camera according to the 2D-3D corresponding relation; according to the camera pose, realizing assignment from the texture colorof the 2D image to the 3D point cloud; determining point cloud semantic segmentation according to the point cloud color and the coordinate information; and detecting and analyzing aircraft appearancedefects according to the point cloud semantic segmentation. The invention discloses the 2D + 3D large aircraft shape defect detection and analysis method based on deep learning. Vision sensor equipment and an optical three-dimensional detection system measurement technology are used for processing and analyzing collected 2D + 3D data, shape defects on a large aircraft can be accurately and effectively detected and extracted, the conception is reasonable, and in practice, automatic application can be achieved in aircraft safety inspection and other scenes.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Aircraft safety system

A system for enabling the safe landing of an aircraft during an in-flight emergency is provided. The system includes a plurality of onboard devices for releasably securing a plurality of wings to a fuselage, and a non-electric module for activating said onboard devices. Said onboard devices are released to separate said wings from the fuselage.
Owner:MANFREDI DARIO P +1

Aircraft safety seat

An aircraft safety seat that has a supporting structure and a bucket seat supported by the structure, the bucket seat has a seat and a back which are lined together, the back being installed on the structure so as to slide generally downwards, wherein at least one connection rod connected by its first end to the support and by its other end to the seat, the connecting rod being generally horizontal when in normal use, and being suited for pivoting downwards by its first end under the effect of a force exerted downwards on the seat, against the action of a shock absorber.
Owner:ZODIAC SEATS FRANCE

System and method for facilitating target aiming and aircraft control using aircraft displays

An improved system and method are disclosed for facilitating target aiming and aircraft control by flight crews using electronic displays. For example, an aircraft display system is disclosed that includes a database for storing target location and boundary data, a processing unit, a position and direction determination unit for use in determining the position of an aiming symbol on a display, a graphics display generator, and a visual display. The processing unit determines whether or not a selected target to be displayed is obscured or covered by the aiming symbol to be displayed. If any portion of the target is obscured or covered by the aiming symbol, then the processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of the portions of the aiming symbol that obscure or cover the target. Notably, the transparency of any symbol (or portion of a symbol) can be increased if that symbol obscures or covers a target being displayed or viewed. Thus, the visibility of targets viewed using onboard visual displays is significantly enhanced, whereby the targets are obscured by the symbols used to aim and control the aircraft. Advantageously, target aiming and aircraft control are facilitated, which reduces pilot workload and navigation errors, and thus results in increased aircraft safety.
Owner:HONEYWELL INT INC

Apparatus, system and method for aircraft security and anti-hijacking intervention

A system and method for operating an aircraft such that any hostile persons taking over the cockpit, for instance, terrorists or a disgruntled pilot, cannot control the flight path of the aircraft to enter restricted airspace, such as ‘no fly’ zones, or any authorized pilots while operating an aircraft cannot unintentionally enter any no fly zone areas.
Owner:ARNOUSE DIGITAL DEVICES

Safe landing system and method for rescuing airplane out of action in flight

InactiveCN101274668AAvoiding casualtiesGround installationsAircraft safetyHuman life
The invention relates to a safe landing system and a method for rescuing airplanes, wherein, a carrying device (1) uses a landing-guiding device (2) to detect flight information, such as location, direction and speed, etc. of the airplane (4) and then based on the flight information, the airplane (4) is guided to be matched with the carrying device (1) till the carrying device (1) and the airplane (4) synchronously move to the same horizontal position and direction to cause the airplane (4) to downwards move gradually onto the carrying support (103) of the carrying device (1). Then the engine of the airplane (4) is turned off and the carrying device (1) is decelerated by a brake device (102) to be completely stopped. The safe landing system and the method for rescuing the airplanes can rescue the airplane (4) which breaks down for the duration of the flight and can not successfully open a belly to lower down a take-off and landing device and airplane wheels. By adopting the safe landing system and the method for rescuing the airplanes, the airplane (4) can land safely to not only ensure the safety of human life, but also avoid the economic loss of plane crash.
Owner:黄金富

Aircraft security system

It guarantees the immediate disablement of any violent action bringing the perpetrators under control without any possibility of escape, attack or aggression. It includes an image transmission system with night-time and daytime vision in an angle of 360°, wide angle and zoom, the image being transmitted continuously to the cockpit (2) and to a security cabin (4), as well as providing images for ground. The cabins (2, 4) are sterile, with hermetic sealing, furthermore having an independent communication system between them and an independent aeration and ventilation system. Selective switched triggers for paralysing gas are provided in both cabins (2, 4) with independent action by the captain of the aircraft in order to inundate the passenger cabin with complete paralysis of everyone therein.
Owner:GONZALEZ MANUEL ARDURA

Wind tunnel test gust generator

PendingCN107966263ARich flow fieldAerodynamic testingEngineeringControl system
The invention discloses a wind tunnel test gust generator, which relates to the field of aircraft wind tunnel test research and can realize gust load alleviation to actively control the gust flow field environment needed by the wind tunnel test research and provide an important theoretical basis for the aircraft structure design and the aircraft safety and comfort improvement. The wind tunnel testgust generator is a longitudinal gust generator which can generate a stable harmonic flow field in a vertical direction, is mainly composed of a drive mechanism, a cascade swinging mechanism, a control system and a rack, and is applicable to the test gust generation field.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Quick collector for borings

The invention belongs to the boring and processing technology, and relates to a device capable of collecting borings. A main body structure of a quick collector for borings is a hemispherical housing; a central hole for allowing a bore bit to get in and out is formed in the center of the hemispherical housing; one side of the bottom of the hemispherical housing is an open type, and is in contact with a component surface to form a sealed space; a borings collecting hole is formed in the hemispherical housing; and a negative-pressure absorbing device is connected outside the borings collecting hole, and is used for absorbing away borings. The quick collector for the borings disclosed by the invention can be used for limiting the borings within a limited area, so that a great deal of splash is avoided, the borings can be automatically cleaned, independent cleaning is not required after boring, the boring operation is greatly convenient and aircraft safety is improved.
Owner:HARBIN

Large aircraft point cloud model self-supervision semantic segmentation method based on deep learning

PendingCN111860520AAccurate and Effective Shape Semantic SegmentationReasonable ideaImage enhancementImage analysisPoint cloudEngineering
The invention discloses a large aircraft point cloud model self-supervision semantic segmentation method based on deep learning, and the method comprises the steps: collecting large-size aircraft point clouds from a plurality of stations through a laser tracker, and generating a plurality of groups of 3D point cloud data; constructing a global measurement field, performing initial registration onthe plurality of groups of 3D point cloud data based on the global measurement field, and performing fine registration on the initially registered point cloud data based on graph optimization to obtain a complete aircraft point cloud model; and carrying out self-supervised semantic segmentation on the complete aircraft point cloud model. According to the invention, an optical three-dimensional detection system measurement technology is utilized to process and analyze acquired 3D data, so that shape semantic segmentation on a large aircraft can be accurately and effectively carried out, the conception is reasonable, and automatic application can be realized in scenes such as aircraft safety inspection and the like in practice.
Owner:南京耘瞳科技有限公司

Aircraft safety take-off control method and device

The invention discloses an aircraft safety take-off control method. The method comprises the steps of 10, obtaining information of an angle between an aircraft body and the horizontal plane through an angle sensor; 20, judging whether the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value or not; 30, controlling the aircraft to take off if the obtained information of the angle is smaller than or equal to the maximum safety angle threshold value. The invention further discloses an aircraft safety take-off control device. By the adoption of the technical scheme, whether the aircraft is horizontally placed or not can be accurately judged, and the aircraft can safely take off.
Owner:SHENZHEN AEE AVIATION TECH

Aircraft safe landing method and landing device

InactiveCN106394922ASolve the problem of safe landingEliminate or minimize harmArresting gearVehicle frameStops device
The invention discloses an aircraft safe landing method and a landing device. A landing car is adopted to reduce the speed and the kinetic energy of an aircraft to reach zero within short time to solve such safe landing problems of the aircraft due to undercarriage failures; the landing car includes a frame, multiple sets of wheels, a stop plate A, buffer pads A, a platform, multiple rows of stop devices and a control room; multiple buffer pads A stacked and connected in sequence are mounted on the stop plate A; an airport control center controls the landing speed, angle and direction of the landing car and the aircraft forcedly landed by the failures, gradually lowers the speed of the landing car; meanwhile, an ejector rod is hoisted; a platform rotates around a rotating shaft; an angle alpha of the platform is gradually changed from zero degree to a certain degrees, and meanwhile, the aircraft is decelerated; an aircraft head or an aircraft body or other part and the buffer pads A are deformed; and the buffer pads A coat the surface of the aircraft, so that the resistance is further increased, the speed of the aircraft is reduced to zero, the landing is safe, and the harm to the aircraft and persons therein is eliminated or reduced.
Owner:DALIAN HUAGONG INNOVATION TECH

Aircraft safety detection management device and safety control system

The present invention discloses an aircraft safety detection management device. The aircraft safety detection management device comprises N battery packs, N BMS modules corresponding to the battery packs and a BMS host; the N battery packs are arranged in parallel; each of the battery packs comprises a plurality of batteries; the BMS modules acquire the monitoring data of the battery packs, wherein the monitoring data contain the temperature and electric quantity of the battery packs and the individual voltage of each battery; and after an aircraft takes off, the BMS host compares the monitoring data with a first preset value, a second preset value and a third preset value and judges whether the monitoring data exceeds the first preset value, the second preset value and the third preset value so as to output alarm signals of corresponding levels. According to the aircraft safety detection management device of the invention, the battery packs are arranged independently, each battery pack is provided with an independent module, and therefore, each battery pack can be monitored independently, the service lives of the battery packs can be prolonged, and the safety use degrees of the battery packs can be improved; and grading detection is performed according to the electric quantity and temperature of the battery packs and the individual voltage of each battery, so that the corresponding alarm signals can be outputted, and therefore, the use safety of the aircraft can be improved. The invention also discloses a corresponding safety control system.
Owner:深圳市哈威创新技术有限公司

Apparatus, system and method for aircraft security and anti-hijacking intervention

A security mechanism identifies users, so as to restrict access and operation to authorized users, such as to persons authorized to access and fly a particular aircraft. The security mechanism comprises one or more security devices to identify the user attempting to gain access or operate the controller; and one or more monitoring devices to determine whether or not the user identified is authorized to have access or operate the controller. Methods of safely operating aircraft are also described. The methods include protocols for limiting access to the aircraft and assuming remote control of the aircraft if a possibly hostile situation is detected.
Owner:ARNOUSE DIGITAL DEVICES

Aircraft safety device systems

An aircraft system comprising a deflector assembly including, a base having mounting apertures; an inner ring concentrically positioned within an outer ring, the inner ring and the outer ring have an annulus defined therebetween via a base plate, a plurality of rods attached within the annulus and culminating at an apex creating a conical profile; and a forward-mounted cone-shaped deflecting member. The base plate comprises a through hole allowing airflow through the deflector assembly to supply an airplane engine. The aircraft safety device system further comprises at least one locking latch for removably securing the deflector assembly to a housing of the airplane engine. The aircraft safety device is mountable inside a lip of the housing of the airplane engine. Further, the aircraft safety device provides protection for airplane engines from air born animate and inanimate objects.
Owner:JONES RICHARD +1

Non-centralized safety interval autonomous keeping system for pilot

The invention discloses a non-centralized safety interval autonomous keeping system for a pilot, which is characterized by comprising a conflict probability module, a graded warming module and a dynamic release module. The input part is composed of four kinds of data of aircraft performance, a flight status, an airspace situation and a flight intention, and the output part is aircraft operation parameters. The system uses the aircraft safety interval autonomous keeping as a research object, problems of conflict detection and conflict release between aircrafts, the aircraft and a ground obstacle and the aircraft and the special restricted airspace existing in intensive flights under different performance, different missions and different priorities of heterogeneous aircrafts in a civil aviation operation condition can be solved. Key technologies such as conflict detection among multiple aircrafts, conflict release strategy optimization and flight conflict autonomous graded evaluation in the civil aviation operation condition are broken through, and a set of complete non-centralized safety interval autonomous keeping system for the pilot is brought forward.
Owner:CIVIL AVIATION FLIGHT UNIV OF CHINA

Apparatus, system and method for aircraft security

A security mechanism identifies users, so as to restrict operation to authorized users, such as to persons authorized to fly a given aircraft. The security mechanism comprises a controller operable by a user; one or more security devices to identify the user attempting to operate the controller; and one or more monitoring devices to determine whether or not the user identified is authorized to operate the controller.
Owner:ARNOUSE DIGITAL DEVICES

Patrol aircraft safety control system

The invention relates to a patrol aircraft safety control system, which comprises a ground control device, an emergency air bag device, an aircraft and a main control chip and a slave control chip for controlling the aircraft, wherein the aircraft is provided with an image acquisition unit, a flight control unit, a wireless transmitting and receiving device and a memory electrically connected with the main control chip respectively; the ground control device comprises a wireless transmitting and receiving module, an aircraft remote control module and a flight path module; the aircraft is also provided with a speed sensor, a GPS positioning device, a six-axis inertial sensor and an ultrasonic sensor electrically connected with the input end of the slave control chip, and the output end of the slave control chip is electrically connected with a rotor control device, a speed reducing protection device, and a gas generating device. The aircraft can perform patrol automatically according to the made flight path, the aircraft reduces the speed once fault happens, the air bag can be ejected in time, and the process is safe and reliable.
Owner:天津津宇凯创航空科技发展有限公司

Aircraft double-redundancy anti-skid control system

The present invention relates to an aircraft double-redundancy anti-skid control system, which comprises an anti-skid controller, an electromagnetic hydraulic lock, a brake control valve and a wheel speed sensor. According to the present invention, during a normal anti-skid control process, the main anti-skid control plate card of the anti-skid controller, the brake control valve, and the main electrical coil of the wheel speed sensor are in a working state, the standby anti-skid control plate card and the standby electrical coil are in a warm standby state, the anti-skid control system automatically switches to a standby working state when any one of the main anti-skid control plate card, the brake control valve and the main electrical coil of the wheel speed sensor produces failure, and no influence is generated to the main anti-skid control when any one of the standby anti-skid control plate card of the anti-skid controller, the brake control valve and the standby electrical coil of the wheel speed sensor produces failure, such that the operation reliability of the anti-skid control system is improved, and the aircraft safety is effectively improved.
Owner:XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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