GB806385A - Improvements in or relating to the abatement of noise in gaseous currents - Google Patents
Improvements in or relating to the abatement of noise in gaseous currentsInfo
- Publication number
- GB806385A GB806385A GB3826/56D GB382656D GB806385A GB 806385 A GB806385 A GB 806385A GB 3826/56 D GB3826/56 D GB 3826/56D GB 382656 D GB382656 D GB 382656D GB 806385 A GB806385 A GB 806385A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stream
- series
- gaseous
- chambers
- silencers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/02—Energy absorbers; Noise absorbers
- F16L55/033—Noise absorbers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Exhaust Silencers (AREA)
Abstract
806,385. Silencing gaseous currents. HIRSCHORN, M. Feb. 7, 1956 April 13, 1955], No. 3826/56. Class 7(2) A method of abating the noise level of gaseous currents comprises the steps of introducing a gaseous stream into a conduit along the central longitudinal axis thereof, alternately inducing portions of the stream to flow in opposite directions substantially perpendicularly away from the axis of the conduit and inducing those portions to flow in opposite directions substantially perpendicularly toward the axis of the conduit, and concurrently expanding the volume of the gaseous stream at selected points along the direction of stream flow. As shown in Fig. 2, the sound attenuation apparatus comprises a casing 24 circular or rectangular in crosssection and inlet and exhaust tubes 26, 27, the casing defining a chamber 28 centrally and axially of which is suspended by members 30 a divider 29 of circular crosssection and provided with a partition 36 of sine-wave form, the latter forming chambers 37, 38; the walls of the divider are perforated with holes 39 which cover about one fourth of the surface area of the divider. Annular chambers 33, 34, subdivided by radial partitions, are located adjacent the tubes 26, 27, the walls 31, 32 of those chambers having openings 41, 42. The apparatus is mounted on wheels 16, Fig. 1, for manouverability at airports and has an intake portion 18 removably connected to the exhaust 19 of a jet aircraft 21, and a vertical exhaust portion 23; diffusers and watercooling are provided for afterburner operation of the aircraft engine. Two or more of the silencing devices may be disposed in series. In a modification, (a) the silencer has three stages 54, 55 and 56, Fig. 6, arranged in series, the chambers 68, 69 and 72, 73 extending across the casing 53 and being subdivided by partitions, and the intake tube 91 being conical in form, the gas exit comprises two openings 96, 97, and (b) a group of silencers are assembled in series and in parallel, Fig. 8, the gaseous stream being apportioned between the silencers 101 in parallel and each part of the stream flowing upwardly through a series of superposed silencers.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US806385XA | 1955-04-13 | 1955-04-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB806385A true GB806385A (en) | 1958-12-23 |
Family
ID=22158639
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3826/56D Expired GB806385A (en) | 1955-04-13 | 1956-02-07 | Improvements in or relating to the abatement of noise in gaseous currents |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB806385A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010020040A1 (en) * | 2008-08-18 | 2010-02-25 | Research In Motion Limited | Systems and methods for training sequence selection, transmission and reception |
CN111426045A (en) * | 2020-02-28 | 2020-07-17 | 青岛海尔空调电子有限公司 | Noise reduction air duct assembly for air duct machine and design method thereof |
-
1956
- 1956-02-07 GB GB3826/56D patent/GB806385A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010020040A1 (en) * | 2008-08-18 | 2010-02-25 | Research In Motion Limited | Systems and methods for training sequence selection, transmission and reception |
KR101237186B1 (en) * | 2008-08-18 | 2013-02-25 | 리서치 인 모션 리미티드 | Systems, devices, and methods for training sequence transmission and reception |
US8401101B2 (en) | 2008-08-18 | 2013-03-19 | Research In Motion Limited | Systems, devices, and methods for training sequence transmission and reception |
CN111426045A (en) * | 2020-02-28 | 2020-07-17 | 青岛海尔空调电子有限公司 | Noise reduction air duct assembly for air duct machine and design method thereof |
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