LOCK SYSTEM FOR TURBINE ENGINE NACELLE AND NACELLE INCLUDING SAME

HIGH VISIBILITY HOOK LATCH

LOCKOUT HANGER SYSTEM

ELECTRICAL LOCKOUT SYSTEM FOR AIRCRAFT PROPULSION SYSTEM

PROPULSION ASSEMBLY COMPRISING AT LEAST ONE PROTECTIVE HOUSING CONFIGURED TO ACCOMMODATE AT LEAST A PORTION OF AN ELONGATED ELEMENT SUCH AS AN ELECTRIC CABLE

Mount with Plastically Straining Load Absorption Device

Frangible Fitting with Fail Safe Straps

AIRCRAFT PROPULSION ASSEMBLY COMPRISING A LOAD-BEARING STRUCTURE INTERPOSED BETWEEN AN ENGINE UNIT AND A PRIMARY STRUCTURE OF A PYLON

SOLENOID RATCHET MECHANISM

REMOTELY OPERATED LATCH FOR AIRCRAFT

LATCHES FOR NACELLE INNER STRUCTURE SECTIONS

Device to Secure an Engine Cowling to an Aircraft Engine

COWL ASSEMBLY FOR A GAS TURBINE ENGINE

JOINING FLANGE FOR AIRCRAFT NACELLE WITH ZONE OF FLEXIBILITY

MULTI-SYSTEM THRUST REVERSER FOR AIRCRAFT PROPULSION SYSTEM

PROPULSIVE ASSEMBLY WITH ENHANCED ENGINE COWL, AND AIRCRAFT COMPRISING SUCH AN ASSEMBLY

AIRCRAFT PROPULSION SYSTEM AND THRUST REVERSER MECHANISM

ACTUATOR WITH BACK-TO-BACK CLUTCH AND A NO-BACK UNIT

LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

THRUST REVERSER MANUAL DRIVE SYSTEM

ASSEMBLY COMPRISING A STATIONARY SURFACE AND A MOVABLE SURFACE OF AN AIRCRAFT

BOLTED CONNECTION BETWEEN MOUNTING BRACKET AND AIRCRAFT ENGINE CASE(S)

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN INTERMEDIATE COWL OF THE STATIONARY, REMOVABLE TYPE, MOUNTED ON A HINGE SYSTEM

MECHANISM FOR CONNECTING HIGH TEMPERATURE AIR DUCTING FOR AIRCRAFT ENGINE

PROPULSION SYSTEM FOR AN AIRCRAFT COMPRISING A TURBOJET, A PYLON AND ENGINE ATTACHMENT

NACELLE PIN LATCH ASSEMBLY

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

LOCK MECHANISM OF TELESCOPIC HOLD OPEN ROD

EXTERNAL POWER CONTROL MODULE FOR AND METHOD TO OPEN COWLING OF AN AIRCRAFT ENGINE NACELLE

ALIGNMENT SYSTEMS AND METHODS

Outer barrel support structure for nacelle inlet structure

AIRCRAFT COMPRISING AT LEAST ONE COWL HAVING TWO PARTS MOVABLE RELATIVE TO EACH OTHER

AIRCRAFT NACELLE COMPRISING A SEALED BOX STRUCTURE AND A DOOR WHICH OPENS THE BOX STRUCTURE TO THE OUTSIDE

Aircraft latch Assembly with Lock Sensor(s)

NACELLE FOR AN AIRCRAFT PROPULSION UNIT COMPRISING AN ACCESS SPACE CLOSED BY A TANGENTIALLY CLAMPED COWL

LOCK MECHANISM FOR TELESCOPIC HOLD OPEN ROD

HOOK LATCH FOR AIRCRAFT NACELLE COWLS

Aircraft propulsion assembly comprising at least one aerodynamic panel which is supported by at least one intermediate radial support, aircraft comprising at least one such propulsion assembly

Long throw latch for aircraft system

AIRCRAFT FAIRING HAVING A REMOVABLE PANEL AND A COMPRESSIBLE SEAL, AIRCRAFT HAVING AT LEAST ONE SUCH FAIRING

Cowling latch interlock mechanism

PRESSURE RELIEF LATCH

MISALIGNMENT LATCH FOR AN AIRCRAFT SYSTEM

Aircraft nacelle equipped with at least one thrust reversal device comprising a downstream deflector, aircraft comprising at least one propulsion unit having such a nacelle

LONG THROW LATCH FOR AIRCRAFT SYSTEM

PROPULSION UNIT COMPRISING PENDULAR BIFURCATION PANELS

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

LOCKING SYSTEM FOR AN AIRCRAFT NACELLE

Inlet outer barrel segmented attach flange

AIRCRAFT PROPULSION UNIT COMPRISING AT LEAST ONE PRESSURE RELIEF DEVICE AND AIRCRAFT HAVING AT LEAST ONE SUCH PROPULSION UNIT

Aircraft propulsion system comprising a nacelle equipped with an improved articulation system

AIRCRAFT HAVING A LOCKING DEVICE AND A SYSTEM FOR VISUAL INDICATION OF THE STATE OF SAID LOCKING DEVICE

Aircraft propulsion system having a nacelle equipped with an improved articulation system

LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL

AIRCRAFT HAVING AN ENGINE PYLON WITH A MOBILE COWL

GUIDE ASSEMBLY FOR AN AIRCRAFT PROPULSION UNIT

PROPULSION SYSTEM OF AN AIRCRAFT, HAVING AN ASYMMETRICAL NACELLE

AIRCRAFT LATCH ASSEMBLY WITH LOCK

INNER COWL ARRANGEMENT FOR GAS TURBINE ENGINE

Assembly Comprising a Nacelle Panel and a Member Forming a Ball

HOOK LATCH FOR AIRCRAFT PANEL

AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MOBILE EJECTION STRUCTURE

Bypass turbofan including a system for blocking the secondary flow including veils

Latch assembly

COWL HOOP LATCH ASSEMBLY

EXPANDABLE DRONE

One-way speed limiter for a power door opening system for an aircraft

Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system

DEVICE FOR CONTROLLING AN ELECTRICAL THRUST REVERSER CONTROL SYSTEM FOR AN AIRCRAFT

ADJUSTABLE HOOK LATCH WITH INDEXING BEARING BLOCK

Propulsion unit for an aircraft and method for mounting same

Nacelle inlet assembly with composite lipskin

Nacelle inlet assembly that promotes laminar flow

Cowl assembly for a gas turbine engine

Aircraft equipped with at least one pressure-relief device including a mobile wall retained in a closed position

Aircraft propulsion unit comprising a nacelle and a turbomachine independently supported by a wing, fuselage or tail element

Balk device for door lock

Aircraft with a fuselage accommodating an unducted turbine engine

NACELLE FOR AN AIRCRAFT PROPULSION UNIT, COMPRISING A SAFETY ROD FORMING A STRUCTURAL REINFORCEMENT

Nacelle inlet structure fitting with locator clip and hoist bracket

Exhaust-gas treatment device for an aircraft engine

Aircraft safety keeper for latch utilization

Thrust reverser comprising pivoting half-assemblies and a connecting beam for the half-assemblies at the six o'clock position

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A LOAD BEARER

Aircraft

LOCKING MECHANISM FOR AT LEAST ONE MOVABLE ELEMENT SITUATED IN A FIRST ZONE AND COMPRISING A COMPONENT THAT CAN BE ADJUSTED FROM A SECOND ZONE, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH LOCKING MECHANISM

Hook Latch With Adjustable Throw

INLET ARRANGEMENT, A PROPULSION SYSTEM, AND AN AIRCRAFT

Aircraft comprising an engine pylon with a movable cover assembly and a specific locking system

Nacelle for an aircraft propulsion assembly comprising a flap for closing a recess for the passage of an actuator

Pressure relief door assembly with temperature-actuated lock

AIRCRAFT SAFETY LATCH

Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure

Hinge for articulating two panels of an aircraft propulsion assembly

Propulsion assembly for an aircraft

Pylon system for coupling engine to vehicle

Assembly for an aircraft nacelle and comprising a support panel, a thermal protection element and a fastening system

Aircraft propulsion system with variable area inlet

Drive-through friction clutch as a tensile load disconnect

Assembly for a nacelle of an aircraft engine, said assembly comprising a fixed cowl and a cowl mounted so as to be able to move on the fixed cowl

PROPULSION ASSEMBLY FOR AN AIRCRAFT

Thrust reverser system latch assembly and method of operating same

OUTSIDE FIT FLANGE FOR AIRCRAFT ENGINE

Propeller deicing systems and methods

Attachment concept for a fairing on an airfoil body such as a flap or a wing of an aircraft

Adjustable motor fairings for aerial vehicles

AIRCRAFT FAIRING COMPRISING AT LEAST ONE FLEXIBLE JOINT CONNECTING A FIXED PANEL TO A MOVABLE PANEL

Guide systems for installing aircraft structures

Aircraft engine pylon having a movable assembly of cowls

Opening system for a door

High visibility hook latch

System with locking indicator for a nacelle element, comprising a removable key for locking and controlling the indicator

Thrust reverser cascade including acoustic treatment

Forward secondary structure for a mounting pylon of an aircraft

Encapsulated bearing block design for adjustable hook latch

ADJUSTABLE HOOK LATCH HAVING EFFICIENT LOAD PATH

Nacelle for a bypass turbomachine comprising a thrust reverser, bypass turbomachine comprising such a nacelle, and aircraft comprising at least one such turbomachine

Air inlet duct for a nacelle of an aircraft propulsion assembly

Aircraft engine nacelle cowling mechanism

Assembly for an aircraft having a pylon and a nacelle comprising a visor fitted with tensioning systems and centering systems

Gas turbine engine mounted above wing and with camber

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

Clevis-sensing adjustable hook latch

PROPULSION ENGINE AND COWL

Propulsion system for an aircraft

Turbojet engine fan casing

Actuation system for a thrust reverser of an aircraft propulsion system

Propulsion system arrangement for turbofan gas turbine engine

Nacelle air intake and nacelle comprising such an air intake

Nacelle air intake and nacelle comprising such an air intake

Propulsive assembly for aircraft

Amphibious aircraft taxiing systems

Expandable cellular system for a sandwich panel

Aircraft propulsion system nozzle with internal flow passage

Systems and methods for high visibility latch handle

Systems and methods for latch hook length adjustment

Aircraft electrically powered thrust reverser systems

Rotatable nacelle for centrifugal fan on aircraft

Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system

Tiltrotor aircraft rotating proprotor assembly

Support structure for inner cowls of an aircraft propulsion system

Nacelle with independent opening thrust reverser section

Bypass turbofan engine comprising mobile deflectors

Latching system with movable anti-shear mechanism

Aircraft nacelle comprising a cowl and an automatically-operated locking device that limits the deformation of the cowl

Pressure relief assembly

LATCH ASSEMBLY

Structural panel with integrated coupler

Self-aligning door bogie

Aircraft and propulsion engine mount system

Propulsion assembly for an aircraft, having a maneuverable thrust reverser

Turbofan comprising a system comprising a screen for closing off the bypass duct

Hinged assembly with fail-safe hinge pin

Dual axis hinge radial displacement limiter

Nacelle auxiliary landing gear

Assembly and method for handling an aircraft propulsion unit

Drain mast seal assembly with seal wedge(s)

Blade fragment barrier for aircraft engine inlet cowl

Turbomachine nacelle having acoustically porous walls

Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nesting

Cowl door latch assembly

Nacelle cowl deflection limiter

Aircraft engine exhaust systems enabling reduced length aft strut fairings

Linkage(s) between inner and outer cowl doors

Linkage supporting a door of an aircraft propulsion system

Load-bearing structure intended to be mounted on a gas generator

Grid-type thrust reverser for turbojet engine

One-way clutch for use in a no-back clutch design

Movement-limiting device for a turbine engine and associated method

Inlet bulkheads for large diameter aircraft engines

AIRSKI EVTOL PAV WITH INTEGRATED DUCTED-FAN FAIRING

Bypass propulsion unit, comprising a thrust reverser with movable cascades

Nacelle

Nacelle thrust reverser compression rod supporting system

MACHINABLE MOLDED FRETTING BUFFER

Latch and method for operating said latch

Nacelle with a translatable inlet for an aircraft propulsion system

Propulsion unit including lifting points disposed on thrust reverser cylinder supports

Drive unit for an aircraft having lifting points, and carriages for supporting such a unit

Opening cowl assembly and deployment mechanism

Defrosting and acoustic treatment device for an air intake lip of a turbojet engine nacelle

Inlet bulkhead with ventilation groove

Aircraft nacelles having adjustable chines

Arrangement for coupling fairing panel to engine casing

Rear assembly of an aircraft turbojet engine nacelle comprising a thrust reverser with sliding cascades

Membrane thrust inverter for an aircraft propulsion unit

Fan cowl securement retainers

Aircraft engine assembly with isolation valve outside uncontained rotor impact area

LOCKING DEVICE FOR FLAPS ON AIRCRAFT

Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle

Aircraft propulsion unit and method for ventilating an engine enclosure

Method of extracting mandrel for hollow-hat panel production

Propulsion unit for aircraft comprising an assembly box-type structure in the six o'clock position

Self-engaging fan cowl hook latch

Nacelle with tangential restraint

Metal insulating part

Thrust reverser assembly for an engine nacelle of an aircraft

Thrust reverser with movable cascades for an aircraft propulsion unit and related mounting and dismounting methods

Fastening device for a heat-shield panel

Fuel cell powered line-replaceable thrust module

Bulkhead shims for curvilinear components

TURBOJET COMPRISING A THRUST REVERSER DRIVE MECHANISM

System for warning an open state of a two-part fan cowl

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

Adjustable motor fairings for aerial vehicles

Jet engine nacelle comprising a mobile assembly and a reinforced fixed structure

Pivoting connection device providing a connection between at least two components, aircraft comprising a cowl equipped with said pivoting connection device

Motive fairing assembly for use in rotorcrafts

PRESSURE RELIEF LATCH

Propulsive assembly of an aircraft comprising a junction fairing between a nacelle and a pylon of the aircraft equipped with a removable cowl and aircraft equipped with said propulsive assembly

Latch having shear load carrying capability

Propulsion assembly for an aircraft, comprising a load support

Brake systems for aircraft and related methods

BRAKE SYSTEMS FOR AIRCRAFT AND RELATED METHODS

Aerodynamic nacelle strakes as axial locator

Propulsion engine thermal management system

GUIDED FAN COWL HINGE

Aircraft nacelle comprising a cowl with two articulated doors

High visibility panel latch

Slat-thrust reverser clearance

ENGINE MOUNTED AIRCRAFT GEARBOX DISPOSED IN PYLON

Pressure relief assembly

Nacelle cowl hinge

Fireproof pressure relief assembly

Forward part of an aircraft propulsion unit nacelle comprising a main propagation path for forces between an air intake lip and a back skin of an acoustic panel

Aircraft turbomachine assembly comprising an articulated cowl

Blocker door pressure relief systems and methods

Magnetic fire seal for aircraft nacelle

Thrust reverser compression rod engagement apparatus

Inner fixed structure leading edge latch

PRESSURE RELIEF DOOR ASSEMBLY

STRUCTURE, SUSPENSION SYSTEM, ENGINE ASSEMBLY AND AIRCRAFT

Electronic release system for a hold open rod mechanism

Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps

Aircraft cowl locking system

Aircraft turbine engine assembly comprising a hinged cover

Externally verifiable thermal compensation of cowl opening actuator

Roll load bearing aircraft propulsor moveable panel systems and methods

Geared turbofan gas turbine engine mounting arrangement

Nacelle for an aircraft turbojet engine provided with a device for detecting deformation of its movable structure

Mechanism for indicating position of a latch mechanism for an aircraft nacelle

Propulsion unit for an aircraft, connected to the fuselage of said aircraft

Propulsion system arrangement for turbofan gas turbine engine

Rear assembly of a turbojet engine nacelle including a fireproof sealing device

AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA

Aircraft turbomachine assembly comprising an articulated cowl

GAS TURBINE ENGINE MOUNT ARRANGEMENT

Air intake, nacelle and propulsion unit for monobloc sector aircraft

Nacelle of an aircraft propulsion assembly comprising a plurality of damper elements between a front section and a main section, and associated aircraft propulsion assembly

Aerodynamic aircraft wall comprising at least one vortex generator, and aircraft comprising the said aerodynamic wall

Pivoting connection device between at least two components, aircraft comprising a cowl provided with said pivoting connection device

Aircraft comprising at least one cowling equipped with an improved hinge system

ADJUSTMENT FEATURES FOR ENGINE COWL DOOR

Passive particle separation system

Aircraft turbojet engine nacelle, propulsion unit and aircraft including such a nacelle

Turbojet including a nacelle equipped with a thrust reverser system including a hinged structure

Device providing pivoting connection between at least two components, aircraft comprising a cowl equipped with this pivoting-connection device

Door for a tiltrotor proprotor pylon

Diaphragm latch

Aircraft nacelle with rotary fan cowling incorporating an access hatch

TURBINE ENGINE

Fan cowl latch concept for fuselage mounted power plant

Nacelle equipped with a thrust-reversing system comprising doors and anti-vibration systems for the doors in stowed position

Front fairing of an aircraft pylon comprising a mobile shroud and aircraft equipped with said front fairing

Aircraft bypass turbojet engine with opening fitted with a hinge with gooseneck fitting

Moveable aircraft cowl and bypass section

Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure

NACELLE FOR AN AIRCRAFT POWER UNIT

TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST-REVERSING SYSTEM COMPRISING OUTER AND INNER DOORS

Nacelle of a turbojet engine comprising a thrust-reversing door

Nacelle of a turbojet engine comprising an outer thrust-reversing door

Locking hinge apparatus for aircraft doors

Pin latch with adjustable pre-load

Propulsion unit for an aircraft, with reduced aerodynamic drag

Nacelle for an aircraft turbojet engine with hybrid air inlet and fan cowl

Nacelle forward part of a propulsion assembly comprising an inclined stiffening frame

JET ENGINE COMPRISING A NACELLE EQUIPPED WITH A THRUST REVERSING SYSTEM COMPRISING DOORS

System for actuating a panel of a turbojet engine nacelle

SYSTEM FOR AND METHOD OF ACTUATING AN AIRCRAFT COWL

Turbine engine nacelle comprising a cooling device

Pylon of a propulsion unit

Hydraulic piston actuator for a door

Aircraft comprising at least one engine assembly linked to the fuselage of the aircraft by two connecting rods positioned at least partially in an air inlet of the engine assembly

System for monitoring the state of a hook-keeper unit

ELECTRO-MECHANICAL ACTUATOR SYSTEM FOR OPENING AND CLOSING OF AIRCRAFT ENGINE COWL DOORS

Mounting assembly

Load controlling bolted flange deformable spacers

Load controlling bolted flange deformable spacers

Latch indication system and method for a fan cowl of an air vehicle

Actuator with vibration attenuation using visco elastic materials

Fan cowl mounted to thrust reverser

Mounting device with pin actuator

Tiltrotor aircraft rotating proprotor assembly

Hold open j-track locking mechanism for cowling

Bi-folding engine cowl having a plurality of open positions to provide access

Safety maintenance panel for a thrust reverser

High-mounted aircraft nacelle

Baseless vortex generator

Modular aircraft

Fairing integrating with outer mold line and protective portions