Ducted open rotor apparatus and method

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C244S065000, C244S05300R, C248S554000, C060S904000, C416S179000, C416S189000, C416S190000

Reexamination Certificate

active

07850116

ABSTRACT:
A propulsor apparatus for a mobile platform, for example an aircraft is provided. The propulsor apparatus includes an aerodynamically shaped propeller duct that houses at least a portion of a turboprop engine, and fully houses a propeller driven by the engine. Inside the propeller duct is a circumferential ring that closely surrounds the propeller such that only a small clearance is provided between the outermost tips of the propeller blades and an inner surface of the circumferential ring. The circumferential ring includes sound deadening material that attenuates noise generated by the tip vortices created at the outermost tips of the propeller blades. The propeller duct and circumferential ring are supported by a plurality of structural rods that couple to structure of the mobile platform, for example to the spars within a wing of an aircraft. The apparatus and method significantly reduces the noise associated with a turboprop engine.

REFERENCES:
patent: 3837602 (1974-09-01), Mullins
patent: 3952973 (1976-04-01), James
patent: 4043522 (1977-08-01), Vetter
patent: 4116405 (1978-09-01), Bacchi et al.
patent: 4358074 (1982-11-01), Schoen et al.
patent: 4437627 (1984-03-01), Moorehead
patent: 4544115 (1985-10-01), Edgley
patent: 4569199 (1986-02-01), Klees et al.
patent: 4657209 (1987-04-01), Edgley
patent: 4817382 (1989-04-01), Rudolph et al.
patent: 4917336 (1990-04-01), Jacobs et al.
patent: 5452575 (1995-09-01), Freid
patent: 5467941 (1995-11-01), Chee
patent: 5943856 (1999-08-01), Lillibridge et al.
patent: 2005/0239940 (2005-10-01), Shima et al.
patent: WO 90/09313 (1990-08-01), None
“Performance Study of a Ducted Fan” by Abrego and Bulaga dated Jan. 2002.
National Advisory Committee for Aeronautics Technical Note 3547 titled “Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack from 0°to 90°” by Lysle P. Parlett dated Nov. 1955.
Smithsonian/NASA ADS Physics Abstract Service “An estimate of the noise shielding on the fuselage resulting from installing a short duct around an advanced propeller” by James H. Dittmar dated Mar. 1988.
AIAA 89-2478 “Ducted Ultra High Bypass Engine Configuration Definition” by H. Geidel and D. Gray dated Jul. 1989.
Glenn Technical Reports Server “Ultra-High Bypass Ration Jet Noise” by John K.C. Low dated Oct. 1994.
Glenn Technical Reports Server “Flow Analysis for the Nacelle of an Advanced Ducted Propeller at High Angle-of-Attack and at Cruise with Boundary Layer Control” by D.P. Hwang, D.R. Boldman, and C.E. Hughes dated Jan. 1994.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Ducted open rotor apparatus and method does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ducted open rotor apparatus and method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ducted open rotor apparatus and method will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4217962

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.