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Aircraft Engineering and Aerospace Technology, 1986
INCORPORATING many kinds of engineering in its design and construction, modern landing gear has advanced to the stage in which almost any aircraft can be supplied with a retractable configuration which can be stowed in a space which is often limited by aerodynamic and structural constraints.
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INCORPORATING many kinds of engineering in its design and construction, modern landing gear has advanced to the stage in which almost any aircraft can be supplied with a retractable configuration which can be stowed in a space which is often limited by aerodynamic and structural constraints.
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2021
This chapter describes the results obtained during the TILDA Project on the additional LAGOON landing gear test case.
F. Chalot +4 more
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This chapter describes the results obtained during the TILDA Project on the additional LAGOON landing gear test case.
F. Chalot +4 more
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A steerable landing gear for vehicles with main gear skids
Journal of Spacecraft and Rockets, 1969Steerable landing gear system consisting of freely castoring corotating wheel nose gear, tiltable axle and main gear skids for lifting body ...
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Aircraft Engineering and Aerospace Technology, 1971
A TRIPLEX HYDRAULIC SYSTEM provides maximum safety and reliability for the powered flying controls. In a triplex system, all three sub‐systems operate simultaneously so that if one fails, the two remaining sub‐systems continue to provide control without interruption, the failed sub‐system being isolated at leisure.
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A TRIPLEX HYDRAULIC SYSTEM provides maximum safety and reliability for the powered flying controls. In a triplex system, all three sub‐systems operate simultaneously so that if one fails, the two remaining sub‐systems continue to provide control without interruption, the failed sub‐system being isolated at leisure.
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Aircraft Engineering and Aerospace Technology, 1988
HAVING supplied components for early versions of the Airbus 300 as well as the A300–600 and A310, Dowty Rotol was in a strong position to offer its expertise on the A320. The company has design leadership on the main landing gear for this latest Airbus product and manufactures the units in a consortium with its partners, Messier‐Hispano‐Bugatti.
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HAVING supplied components for early versions of the Airbus 300 as well as the A300–600 and A310, Dowty Rotol was in a strong position to offer its expertise on the A320. The company has design leadership on the main landing gear for this latest Airbus product and manufactures the units in a consortium with its partners, Messier‐Hispano‐Bugatti.
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Aircraft Engineering and Aerospace Technology, 1973
THE BASIC MILITARY NEED for the C‐5 relates to the ‘Remote Presence’ concept involving rapid deployment of troops and all heavy equipment to any remote location thereby allowing for minimised standing army and equipment requirements. This ‘Remote Presence’ concept requires that a 300 ton airplane land and takeoff from an unsurfaced field.
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THE BASIC MILITARY NEED for the C‐5 relates to the ‘Remote Presence’ concept involving rapid deployment of troops and all heavy equipment to any remote location thereby allowing for minimised standing army and equipment requirements. This ‘Remote Presence’ concept requires that a 300 ton airplane land and takeoff from an unsurfaced field.
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Aircraft Engineering and Aerospace Technology, 1989
Aircraft undercarriage design involves the application and dissipation of energy within all the various mechanisms making up the complete gear. The functions of landing, taxying, retraction, lowering, steering and braking must be optimised such that each participating component plays its part in the processes.
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Aircraft undercarriage design involves the application and dissipation of energy within all the various mechanisms making up the complete gear. The functions of landing, taxying, retraction, lowering, steering and braking must be optimised such that each participating component plays its part in the processes.
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2017
<div class="section abstract"> <div class="htmlview paragraph">This ARP applies to all types and models of civil aircraft for landing gear structure and mechanism excepting wheels, tires and brakes. All axles, wheel forks, axle beams, links, arms, mechanical and air-oil energy absorbers, braces, lock assemblies, trunnion beams, etc., that
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<div class="section abstract"> <div class="htmlview paragraph">This ARP applies to all types and models of civil aircraft for landing gear structure and mechanism excepting wheels, tires and brakes. All axles, wheel forks, axle beams, links, arms, mechanical and air-oil energy absorbers, braces, lock assemblies, trunnion beams, etc., that
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2017
<div class="section abstract"> <div class="htmlview paragraph">The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber shock struts.</div></div>
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<div class="section abstract"> <div class="htmlview paragraph">The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber shock struts.</div></div>
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Aircraft Engineering and Aerospace Technology, 1968
WHILE an aircraft is in flight, the landing gear is a liability which, by virtue of its weight and size, and demands upon power supplies, reduces the efficiency of the aircraft. However, at two of the most critical and dangerous parts of the sortie, namely take‐off and landing, the safety of the aircraft depends to a very great extent upon the landing ...
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WHILE an aircraft is in flight, the landing gear is a liability which, by virtue of its weight and size, and demands upon power supplies, reduces the efficiency of the aircraft. However, at two of the most critical and dangerous parts of the sortie, namely take‐off and landing, the safety of the aircraft depends to a very great extent upon the landing ...
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