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Supplier: Messier-Bugatti-Dowty
Description: The Messier-Bugatti-Dowty landing gear on the Rafale M (Navy version) are considered the most advanced system for carrier-compatible aircraft. Compared to the Rafale B and C (Air force Version) the nose and main landing gears on the navy version have been reinforced to
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Supplier: Accuris
Description: Aircraft Landing Gear
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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: Accuris
Description: INDICATOR, POSITION, LANDING GEAR
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Supplier: Accuris
Description: Aerospace Landing Gear Systems Terminology
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Supplier: SAE International
Description: This SAE Aerospace Recommended Practice (ARP) is intended to document the process of landing gear system development. This document includes landing gear system development plans for commercial, military, fixed wing and rotary wing air vehicles.
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Supplier: Accuris
Description: (R) Landing Gear System Development Plan
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Supplier: SAE International
Description: basic functional area or major component are as follows: a Landing Gear Systems 1 Landing Gear (General) (L/G) 2 Tire (Tire) 3 Wheel (Whl) 4 Brake (Brk) 5 Nose Wheel Steering (NWS) 6 Shock Absorber (S/A) 7 Skid Control (S/C) b Related Systems 1 Air Vehicle/Aircraft (A/V)
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Standards and Technical Documents - Environmentally Compliant Processes for Landing Gear -- AIR5479BSupplier: SAE International
Description: chromated primers, and high VOC (volatile organic compounds) topcoats. The AIR applies to landing gear structures and mechanisms for all types of civil and military aircraft. The potential replacements apply to both Original Equipment Manufacturer (OEM) hardware and overhaul of
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Supplier: Cequent Performance Products
Description: JACK-SWQ FL LX-B/O-2 SPD
- Actuation: Hand
- Features: Other
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Supplier: National Bronze & Metals Inc.
Description: Valve Seats, Pump Fluid Ends, Glands, Worms, Worms Wheels, Hot Mill Guides, Hand Gun Recoil Mechanisms, Landing Gear Parts, Air Craft Components, Wear Plates, Welding Jaws, Landing Gear Parts, Glass Molds, Machine Parts, Sewage Treatment Applications, Valve Components,
- UNS Number: 95,500
- AISI / AA / CDA Grade: 955
- Overall Width / OD: 1 to 9 inch
- Overall Thickness: 1 to 9 inch
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Supplier: Boeing Company (The)
Description: engineers designed special landing gear that could align with the runway allowing special takeoffs and landings. The original design of the B-52 placed a gunner in the tail of the aircraft. Later designs moved the gunner forward with the rest of the crew. After the Gulf War in
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Supplier: Enstrom Helicopter Corporation
Description: unparalleled stability and solid craftsmanship. With the fewest number of retirement items and no airframe life limit, our 480Bs have lower direct operating costs and spend less time on the ground. ENSTROM 480B features: Energy-absorbing landing gear Five-seat cabin configuration with
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Supplier: ASTM International
Description: requirements, (3) safety factors, (4) design airspeeds, (5) flight loads, (6) pilot control loads, (7) ground loads including landing gear shock absorption, and (8) emergency landing loads. Design and construction requirements are specified for: (1) materials, (2) fabrication
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Supplier: Shell Lubricants
Description: synthetic hydrocarbon hydraulic fluid AeroShell Fluid 71 – a preservative, mineral hydraulic fluid AeroShell Landing Gear Fluid - an extreme-pressure mineral hydraulic fluid AeroShell Shock Strut Fluid – a extreme-pressure, preservative mineral hydraulic fluid *only available in
- Type / Function: Hydraulic Oil / Fluid
- Composition / Chemistry: Petroleum / Mineral Oil, Synthetic
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Supplier: Cessna Aircraft Company
Description: Installed on Center Panel: Multifunction Display (MFD) Dual Touch-screen LCD Control Panels Electronic Standby Flight Display (ESFD) Installed Beneath Glareshield: Flight Guidance Panel (FGP) Installed on LH Tilt Panel: Electrical Power Panel Installed on RH Tilt Panel: Anti-Ice/De-Ice Panel
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Supplier: Greene, Tweed & Co.
Description: actuators, valves, and the most rugged landing gear shock strut applications. The 11,000 Series seals are designed to fit industrial O-ring glands incorporating nominal rod and bore diameters for zero, one and two backup widths per MIL-P-5514B. The G-T design resists extrusion by
- Maximum Operating Pressure: 0 to 10,000 psi
- Operating Temperature: -70 to 450 F
- Seal Type: Composite Seals
- Action: Double Acting
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Supplier: Shenzhen INVT Electric Co., Ltd.
Description: gear installation and motor installation. For gear installation, the regular 50~200-PPR 24V incremental encoder can satisfy the requirements with ±5 mm leveling precision, reducing system cost while satisfying special application requirements and exhibition purposes of customers;
- Maximum Output Voltage: 440 volts
- Supply Voltage (AC): 380 to 440 volts
- Operating Temperature: -10 to 50 C
- Frequency: 50 Hz, 60 Hz
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Description: Construction of Towers, Masts and Hoistway Enclosures 21 5.1 Tower or Mast Construction 21 5.2 Protection of Spaces Below Hoistways Not Extending to the Lowest Floor of the Building 22 5.3 Hoistway Enclosures 22 5.4 Hoist Structure 22 5.5 Erection and Dismantling 23 5.6 Landings 24 6.
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(per MIL-V-19068) which means the normal port (N) closes before the emergency port (E) opens. At no time, are all three ports open simultaneously. This requirement is commonly found in aircraft landing gear systems. Lee Spring Biased Shuttle Valves can be used to reduce the flow required to (read more)
Browse Hydraulic Valves Datasheets for Lee Co. (The)
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Evaluation of accelerated deterioration in NAPTF flexible test pavements
Using the pavement response test results from the NAPTF and ILLI-PAVE structural models, Gomez-Ramirez and Thompson (2002) further verified the principle of superposition for six-wheel B777 and four-wheel B747 landing gear configurations.
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Effect of Dynamic Aircraft Gear Loads on Asphalt Concrete Strain Responses
Using the pavement response test results from the NAPTF and ILLI-PAVE structural models, Gomez-Ramirez and Thompson ͓17͔ verified the principle of superposition for six-wheel B777 and four-wheel B747 landing gear configurations.
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Pavement Deformation Characteristics under Repeated Aircraft Loading with Fixed Wander Sequence
The south side ͑LANE 5͒ was loaded with a four-wheel dual-tandem B747 landing gear having 1118-mm ͑44-in.͒ dual spacing and 1473-mm ͑58-in.͒ tandem spacing.
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Forensic investigation of failed airfield test pavements
All test sections, except the high-strength test sections, were simultaneously trafficked using simulated Boeing 777 (B777) and Boeing 747 ( B747 ) landing gears until the test sections were deemed to be failed.
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Towbarless leads the way
The company's ARTS 1 and 2 is a recovery system for failure of some or all landing gear on a B747 .
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Noise reduction assessments and preliminary design implications for a functionally-silent aircraft
62 Assumed landing gear and flap parameters of a B747 -400. . . . . . . . . . . . . . . .
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On the use of a steerable main landing gear for crosswind landing assistance
Airbus A380 Like the B747 the A380 is equipped with two pairs of main landing gears [6].
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Aeroacoustics Conferences > Investigating landing gear noise using fly-over data: the case of a Boeing 747-400 (AIAA 2013-2115)
In the present work, measurements of a Boeing B747 -400 were used to determine the contribution of the landing gear to the overall noise emitted during a fly-over and how the broadband noise from the landing gear scales with the flight…
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ICAO Journal 2005 No. 6
Factors contributing to brake fires after a B747 landing at Sydney included presence of incorrect and excessive grease on the landing gear axles, inadvertent deselection of reverse thrust, and heat generated by the brakes on the landing roll and subsequent taxiing.
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Journal of Aircraft > Unsteady Surface Pressure Characteristics on Aircraft Components and Far-Field Radiated Airframe Noise
For the second test series, two main landing gear models (synthesized from those of large commercial aircraft such as DC-10, L-1011, or B747 ) of scale 1:4 were attached to the wings of the SB-10 (Fig. 3).
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