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Supplier: Messier-Bugatti-Dowty
Description: emergency extension system and the steering system. Messier-Bugatti-Dowty supplies: The landing gear retraction actuators The landing gear up-locks mechanisms The landing gear doors actuators, The landing gear and steering
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Supplier: SAE International
Description: This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft including all aircraft with vertical landing and crash attenuation requirements. All
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Supplier: SAE International
Description: This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft applications. All axles, wheel forks, axle beams, links, arms, mechanical and air-oil energy
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Supplier: SAE International
Description: This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft. All axles, wheel forks, links, arms, mechanical
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Supplier: Greene, Tweed & Co.
Description: APPLICATIONS Dynamic, unidirectional landing gear applications Accumulators and reservoirs Unidirectional utility actuators
- Shaft O.D. or Seal I.D.: 0.748 to 15.497 inch
- Material (ASTM Abbreviation): EPDM, Fluoroelastomer (FKM - Viton®, Fluorel®, etc.), Nitrile (NBR - Buna-N), Polyurethane / Urethane
- Features: Hydraulic / Pneumatic Seal
- Orientation / Direction: Internal / Rod Seal
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Supplier: Greene, Tweed & Co.
Description: Metric series available for metric-sized designs APPLICATIONS Accumulators and reservoirs Actuators (e.g., door actuators) Flight controls (e.g., spoilers, rudders, aileron, etc.) Landing gear actuator subsystems (e.g., end caps and static seals, etc.)
- Shaft O.D. or Seal I.D.: 0.1574804 to 15.74804 inch
- Maximum Operating Pressure: 4,000 psi
- Seal Type: Composite Seals
- Material (ASTM Abbreviation): EPDM, Flourosilicone (FVMQ, FMQ, FPM, FSI), Fluoroelastomer (FKM - Viton®, Fluorel®, etc.), Nitrile (NBR - Buna-N)
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Supplier: Strainsert
Description: Load Pins are typically designed to measure from 50 to well over 1 million pounds. A few typical applications include: Structural Tests Rocket Reaction Forces Mooring Lines Winch/Crane/Lifting Systems Aircraft Wing Joints Testing Machines Landing Gear Clevis Joints Sheave Axles
- Package: Load Pin
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Supplier: SAE International
Description: Scope of the DRESS project is to research, develop and validate a distributed and redundant electrical steering system technology for an aircraft nose landing gear. The new system aims to: • reduce system weight at aircraft level, replacing the current hydraulic actuation system
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Supplier: National Precision Bearing, Inc.
Description: hydraulic actuators, many aircraft landing gear door applications, vibration dampening devices, hinge and actuation link bearings for control surfaces, sliding guide bearings for flaps and leading edge slats, and power control system drive link bearings. Many others not
- Design Units: Inch
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Supplier: National Precision Bearing, Inc.
Description: impossible. Suited for hydraulic actuators, many aircraft landing gear door applications, vibration dampening devices, hinge and actuation link bearings for control surfaces, sliding guide bearings for flaps and leading edge slats, and power control system drive link
- Design Units: Inch
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Supplier: Greene, Tweed & Co.
Description: designs are unnecessary, keeping costs low Heavy section cap creates more stability in the gland Cost-effective design for valve applications APPLICATIONS Control modules in utility actuators Linear actuators in landing gear systems Valves in engine systems
- Shaft O.D. or Seal I.D.: 0.259 to 16.247 inch
- Seal Type: Composite Seals
- Material (ASTM Abbreviation): EPDM, Flourosilicone (FVMQ, FMQ, FPM, FSI), Fluoroelastomer (FKM - Viton®, Fluorel®, etc.), Nitrile (NBR - Buna-N)
- Orientation / Direction: External / Piston Seal, Internal / Rod Seal
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Supplier: Greene, Tweed & Co.
Description: resistance APPLICATIONS Landing gear (e.g., end caps and static seals for actuators) Accumulators and reservoirs Actuators (e.g., door actuators) Flight controls (e.g., spoilers, rudders, aileron, etc)
- Maximum Operating Pressure: 4,000 psi
- Seal Type: Composite Seals
- Action: Double Acting
- Material (ASTM Abbreviation): EPDM, Flourosilicone (FVMQ, FMQ, FPM, FSI), Fluoroelastomer (FKM - Viton®, Fluorel®, etc.), Nitrile (NBR - Buna-N)
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Supplier: Trelleborg Sealing Solutions Americas
Description: PEEK composite HiMod® Advanced Composite Bearing Plus – enhanced dual-layer bearing with a low friction modified PEEK liner, bonded to continuous carbon fiber PEEK composite backing Applications Petrochemical pump wear rings Oil & Gas swivel joint back-up rings Aerospace landing gear
- Design Units: Metric
- Bushing Type: Sleeve
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Supplier: Cessna Aircraft Company
Description: Glareshield: Flight Guidance Panel (FGP) Installed on Left-Hand Tilt Panel: Electrical Power Panel Installed on Right-Hand Tilt Panel: Anti-Ice/De-Ice Panel Landing Gear Control Panel Installed on Pedestal: Engine Power Levers Flaps Control Pressurization Panel Engine Control/Start
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Supplier: CEF Industries LLC
Description: Gear, Nose Wheel Steering, Canopy Aircraft Scavenger Pumps Variable Bleed Valves Capabilities/Benefits/Advantages High Degree of Design freedom: Flexible shafts allow for limitless possibilities in the location of drive sources, whether electric/hydraulic motors or manual. This design
- Rotation: Bidirectional
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Landing Gear: Struts, Actuators, Pivots Cockpit Controls Wing, Trailing Edge: Flaps, Spoilers Wing, Leading Edge: Slats Hydraulic Fuel Pumps Flight Control Systems: Aileron, Rudder, Elevator Electric Actuators Engine (read more)
Browse Aerospace Bearings Datasheets for GGB -
weight. These innovations improve aircraft efficiency and passenger confidence while extending service life. Landing Gear Applications: Struts Actuation Pivot Points (read more)
Browse Aerospace Bearings Datasheets for GGB -
The easyE® line of electric linear actuators features four models— easyE-25, easyE-35, easyE-50, and easyE-60—with outer diameters of 25, 35, 50, and 60mm, respectively. This slim, in-line design, achieved through a linear layout of motor, gear, and spindle, ensures seamless (read more)
Browse Linear Actuators Datasheets for Bansbach Easylift® -
in site) to energized a set of gears, operating any type of valve. Pneumatic or hydraulic actuators: using either a rack & pinion or a scotch yoke device for moving a rotary valve. They are other types of valve and damper actuators that use a combination of (read more)
Browse Electric Rotary Actuators Datasheets for Indelac Controls, Inc. -
availability in site) to energized a set of gears, operating any type of valve. Pneumatic or hydraulic actuators: using either a rack & pinion or a scotch yoke device for moving a rotary valve. They are other types of valve and damper actuators that use a combination of (read more)
Browse Electric Rotary Actuators Datasheets for Indelac Controls, Inc. -
any type of valve. Pneumatic or hydraulic actuators: using either a rack & pinion or a scotch yoke device for moving a rotary valve. They are other types of valve and damper actuators that use a combination of existing motors and gears, but most applications are (read more)
Browse Electric Rotary Actuators Datasheets for Indelac Controls, Inc. -
gear, flight controls and engines, to passenger seating and a wide variety of made-to-measure applications for the Aerospace industry: Landing Gear Struts Wing Flap Actuators Hydraulic Fuel Pumps Flight Control Systems Electric Actuators (read more)
Browse Aerospace Bearings Datasheets for GGB -
Lee Shuttle Valves are miniature, 3 port, hydraulic valves that allow fluid to flow from one of two inlet sources to a common outlet. They are small enough to fit right into the head of an actuator, saving both space and weight. As with all Lee Inserts, they require no (read more)
Browse Hydraulic Valves Datasheets for Lee Co. (The) -
like: A Health Monitoring Management System (HMMS) for landing gear, incorporating a network of real-time event monitoring sensors Force and position sensors that replace hydraulic systems, facilitating electrification Our experienced technical experts will (read more)
Browse Voice Coil Actuators and Motors Datasheets for Sensata Technologies -
Winch/Crane/Lifting Systems Landing Gear Clevis Joints Mooring Lines/Lanyards Sprocket/Pulley Axles Bombay/Cargo Doors Railroad/Towbar Connections Armanent Suspension Systems Rocket Reaction Forces Aircraft Wing Joints (read more)
Browse Force and Load Sensors Datasheets for Strainsert
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Federal Register > Friday, October 16, 1998 > [63 FR 55560] Airworthiness Directives; Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes
The proposed AD would require inspecting the main landing gear hydraulic actuators to determine whether a certain Frisby Aerospace actuator is installed, and reworking or replacing any of these Frisby Aerospace actuators.
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Federal Register > Wednesday, February 10, 1999 > [64 FR 6512] Airworthiness Directives; Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes
This AD requires inspecting the main landing gear hydraulic actuators to determine whether a certain Frisby Aerospace actuator is installed, and reworking or replacing any of these Frisby Aerospace actuators.
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Federal Register > Friday, June 17, 2011 > [76 FR 35344] Airworthiness Directives; Costruzioni Aeronautiche Tecnam srl Model P2006T Airplanes
During Landing Gear retraction/extension ground checks performed on the P2006T, a loose Seeger ring was found on the nose landing gear hydraulic actuator cap.
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Landing Gear Free-Fall Simulation and Kinetic Energy Optimization
… gear kinetic energies (nominal and limit values) and limiting time The parameters selected to have their values changed during the optimization process were the piston areas (without modifying the chamber total volume) of main landing gear hydraulic actuators , the orifice diameter of …
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http://dspace.mit.edu/bitstream/handle/1721.1/17096/JP-WP-92-01-26847987.pdf?sequence=1
thrust reverser control valves valves, nose landing gear steering equipment valves: landing gear hydraulic actuators .
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Federal Register > Wednesday, June 6, 2001 > [66 FR 30302] Airworthiness Directives; Raytheon Aircraft Company Models 99, 99A, 99A (FACH), A99, A99A, B99, and ...
This AD requires you to inspect all main landing gear (MLG) hydraulic actuators to determine the end cap part number that is installed, and replace any actuator that has a part number 4A125C32 end cap.
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Federal Register > Thursday, November 2, 2000 > [65 FR 65805] Airworthiness Directives; Raytheon Aircraft Company Models 99, 99A, 99A (FACH), A99A, B99, and C9...
The proposed AD would require you to inspect all main landing gear (MLG) hydraulic actuators to determine the end cap part number that is installed, and replace any actuator that has a part number 4A125C32 end cap.
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Industrial implementation of nanostructured cobalt as an alternative to hard chrome
… 1920’s.4 As a result of their intrinsic high hardness and low coefficient of friction, hard chrome coatings have been specified for the protection of steel substrates for a variety of applications including: aircraft landing gear , hydraulic actuator rods and cylinders, gas …
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Properties of WC‐CoCr Based Coatings Deposited by Different HVOF Thermal Spray Processes
These include aircraft landing gear , hydraulic actuators or jet engine bearings.
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Using (Zn-Ni-Sio2) Electrocomposite Coating To Prevent Carbon Steel Against Acidic Environments
Zn-Ni-SiO2 coating has recently been used to replace cadmium plating which is widely used in the aerospace industries ( i.e. landing gear , hydraulic actuators , high performance fasteners, break and fuel lines) because of its excellent corrosion resistance and its electrochemical …