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US3883264A Expired / Lapsed US ⏱️ 0.0 years remaining

Quiet fan with non-radial elements

Assignee: Individual
•
Filing: 1971-04-08
•
Granted: 1975-05-13
•
Expires: 1991-04-08
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Abstract

Abstract In an air blower or axial compressor, such as employed in airplane power plants, ventilating systems, etc., a series of rotating vanes, stationary vanes, or supporting structure of streamline struts is oriented in circumferentially leaning relation to another series of blades in the machine so as to effect a reduction in noise.

Inventors

  • 👤 Gadicherla V R Rao

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 21:04
CPC Classifications
F; F01; F01D; F01D1/00; F01D1/02; F01D1/04; F01D5/00; F01D5/12; F01D5/14; F01D5/141; F01D5/142; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F04D29/542; F04D29/544; F04D29/56; F04D29/563; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 196 words
In an axial flow apparatus of the type described, in combination: a rotor unit and a stator unit each comprising a circumferential array of vanes; said rotor unit being rotatable in axial adjacency to said stator unit for imparting energy to an axial flow through the apparatus; one of said units having a frame comprising inner and outer supports; said vanes of one unit including a plurality of non-radial vanes of airfoil cross-section which are similarly oriented in nonradial positions leaning circumferentially away from the radial in a common direction throughout their radial extent; said vanes being secured between said supports; the vanes of the other unit being oriented in positions angularly related to the positions of said non-radial vanes; said non-radial vanes comprising a first circumferential array of vanes all similarly oriented in positions leaning circumferentially away from the radial in one direction and a second circumferential array of vanes leaning away from the radial in an opposite direction; whereby the pulsations created by the vanes of said rotor unit passing the vanes of said stator unit will be attenuated by the radial progressions of the crossings of the relatively moving vanes, thereby reducing noise.
Claim 2
Dependent Claim 196 words
In an axial flow apparatus of the type described, in combination: a rotor unit and a stator unit each comprising a circumferential array of vanes; said rotor unit being rotatable in axial adjacency to said stator unit for imparting energy to an axial flow through the apparatus; one of said units having a frame comprising inner and outer supports; said vanes of one unit including a plurality of non-radial vanes of airfoil cross-section which are similarly oriented in nonradial positions leaning circumferentially away from the radial in a common direction throughout their radial extent; said vanes being secured between said supports; the vanes of the other unit being oriented in positions angularly related to the positions of said non-radial vanes; said non-radial vanes comprising a first circumferential array of vanes all similarly oriented in positions leaning circumferentially away from the radial in one direction and a second circumferential array of vanes leaning away from the radial in an opposite direction; whereby the pulsations created by the vanes of said rotor unit passing the vanes of said stator unit will be attenuated by the radial progressions of the crossings of the relatively moving vanes, thereby reducing noise.
Claim 3
Dependent Claim 33 words
An axial flow apparatus as defined in claim 1; said first and second circumferential arrays being disposed in respective axially adjacent planes and all secured between the same inner and outer support members.
Claim 4
Dependent Claim 34 words
An axial flow apparatus as defined in claim 1; said first and second circumferential arrays being disposed in respective planes which are separated by an axial space in which the other unit is received.

References Cited (Backward Citations)

US1062258A Cited
US2029813A Cited
US2570155A Cited
US2650752A Cited
US2962260A Cited
US3237849A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-05-12 1978-11-11 1979-05-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-05-12 1982-11-11 1983-05-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-05-12 1986-11-11 1987-05-13 $7700.00 Window Closed / Lapsed

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