PIVOT FAIRING THRUST REVERSER
First Claim
Patent Images
1. An aircraft engine thrust reverser comprising:
- an exhaust duct having an inlet at one of end for receiving exhaust from said engine, an outlet nozzle at an opposite end for discharging said exhaust, a pair of opposite side beams extending between said inlet and nozzle, and a pair of opposite portals disposed circumferentially between said beams forward of said nozzle;
a pair of thrust reverser doors disposed in respective ones of said portals, and rotatably mounted to said beams at corresponding pivots;
a pair of actuators mounted on respective ones of said beams and operatively joined to said doors for selective rotation thereof about said pivots; and
two pairs of blister fairings disposed inside said duct and sealingly joining said doors to said beams around respective ones of said pivots.
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Accused Products
Abstract
A thrust reverser includes a pair of doors covering corresponding portals in an exhaust duct between an inlet and outlet nozzle at opposite ends thereof. The duct also includes a pair of side beams having actuators mounted thereon, and operatively joined to the doors for selective rotation thereof about corresponding pivots. Blister fairings are disposed inside the duct and sealingly join the doors to the beams around respective ones of the pivots.
15 Citations
27 Claims
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1. An aircraft engine thrust reverser comprising:
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an exhaust duct having an inlet at one of end for receiving exhaust from said engine, an outlet nozzle at an opposite end for discharging said exhaust, a pair of opposite side beams extending between said inlet and nozzle, and a pair of opposite portals disposed circumferentially between said beams forward of said nozzle;
a pair of thrust reverser doors disposed in respective ones of said portals, and rotatably mounted to said beams at corresponding pivots;
a pair of actuators mounted on respective ones of said beams and operatively joined to said doors for selective rotation thereof about said pivots; and
two pairs of blister fairings disposed inside said duct and sealingly joining said doors to said beams around respective ones of said pivots. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 16, 17, 18, 19, 20)
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15. An aircraft engine thrust reverser comprising:
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an exhaust duct having an inlet and outlet nozzle at opposite ends, a pair of side beams extending therebetween, and a pair of diametrically opposite portals disposed forward of said nozzle;
a pair of thrust reverser doors disposed in said portals and rotatably mounted to said side beams at corresponding pivots;
means for selectively deploying open and retracting closed said doors around said pivots; and
means including a plurality of blister fairings covering said pivots for sealing closed each of said doors around said portals.
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21. An aircraft engine thrust reverser comprising:
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an exhaust duct having an inlet and outlet nozzle at opposite ends, a pair of side beams extending therebetween, and a pair of diametrically opposite portals disposed forward of said nozzle;
a pair of thrust reverser doors disposed in said portals and rotatably mounted to said side beams at corresponding pivots;
means mounted on said side beams for selectively deploying open and stowing closed said doors around said pivots;
means for sealing closed each of said doors around said portals; and
means for selectively latching closed said doors, and unlatching said doors only after said doors are overstowed. - View Dependent Claims (22, 23, 24, 25, 26, 27)
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Specification