MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
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N/A
Issued Date -
Feb 13, 2025
app pub date -
Oct 21, 2024
filing date -
Oct 21, 2024
priority date (Note) -
Published
status (Latency Note)
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Abstract
A thrust reverser includes an outer articulating panel and an inner articulating panel. The outer articulating panel includes an outer thrust reverser door pivotally coupled to the outer articulating panel. The outer thrust reverser door is movable between an outer door stowed position and an outer door deployed position with respect to the outer articulating panel. The inner articulating panel includes an inner thrust reverser door pivotally coupled to the inner articulating panel. The inner thrust reverser door is movable between an inner door stowed position and an inner door deployed position with respect to the inner articulating panel. The inner thrust reverser door and the outer thrust reverser door are configured to redirect exhaust gasses to generate reverse thrust to an aircraft when the thrust reverser doors are in the deployed positions.
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International Classification(s)
- 2024 Application Filing Year
- F02K Class
- 131 Applications Filed
- 17 Patents Issued To-Date
- 12.98 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F02K Class
- 0 % this patent is cited more than
- < 1 Age