Resources Contact Us Home
Inverted airfoil pylon for an aircraft

Image Number 7 for United States Patent #7770841.

An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET.RTM. is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.

  Recently Added Patents
Thwarting keyloggers using proxies
Bus controller for handling split transactions
Multilayer films having reduced curling
Measurement of an analyte on the skin using a hue angle
Telecommunications system and method
Synthesizing VHDL multiple wait FSMS into RT level FSMS by preprocessing
Piezoelectric speaker and method of manufacturing the same
  Randomly Featured Patents
Thermosetting resinous binder compositions, their preparation and use as coating materials
Turret-type rotary rod-feeder machine
Pallet distance ranging device for forklift
Toy shotgun
Process for the preparation of 9-hydrazono-6,7,8,9-tetrahydro-4H-pyro[1,2-a]pyrimidine-4-one compounds, the salts and hydrates thereof
Weapon and weapon station system and method for loading, testing, targeting, and launching a weapon
Method for preparing exo-tricyclo[,5]non-7-ene-3-spiro-1'-(3'-ethyl-3'-alumina)cy- clopentane
Magnetic tunnel junction sensor with nickel-oxide longitudinal bias layer abutting opposite sides of active region
Fuel nozzle assembly
Bicycle suspension fork assembly