US3883264A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Quiet fan with non-radial elements
Assignee: Individual
•
Filing: 1971-04-08
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Granted: 1975-05-13
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Expires: 1991-04-08
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.
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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 |