Acoustic duct with peripherally segmented acoustic treatment

• US 3,937,590 A
• Filed: 09/03/1974
• Issued: 02/10/1976
• Est. Priority Date: 09/03/1974
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Mani, Ramani
• Primary Examiner(s): Gonzales, John F.
• Application Number:
  US05/503,031
• Time in Patent Office: 525 Days
• Field of Search: 181/33 H, 181/33 HA, 181/33 HB, 181/42, 181/50, 181/33 P, 181/33 E, 415/119, 137/15.1
• US Class Current: 415/119
• CPC Class Codes: F02C 7/045 having provisions for noise suppression
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 137/0536 Highspeed fluid intake means [e.g., jet engine intake]

Abstract

An acoustic duct such as a jet engine fan duct is lined with numerous peripherally spaced, longitudinally extending strips of sound-absorbing material which are effective to scatter spinning mode acoustic pressure fields to higher order, attenuating modes for improved noise suppression. These strips can be alternated with other strips having a different acoustical impedance, or combined with a longitudinally segmented treatment.

Claims

1. In a noise-suppressing duct having mounted therein rotating mechanical equipment with first stage rotor and stator blades which interact to generate spinning mode acoustic pressure fields with propagating and attenuating type modes, said duct being a rigid longitudinally extending duct with an acoustic lining attached to the inner surface thereof, the improvement in which said acoustic lining comprises

a first set of peripherally spaced, longitudinally extending strips of sound-absorbing material, said first set of strips being relatively narrow in the peripheral direction and in total number at least exceeding the number of first stage rotor blades,

a second set of peripherally spaced, longitudinally extending strips of sound-absorbing material mounted flush with said first set of strips and located between and alternating with said first set of strips,

said first and second set of strips being made of sound-absorbing materials having different acoustical impedances and in combination forming a continuous acoustic lining,

said first and second set of strips being effective to achieve scattering of said spinning mode acoustic pressure fields to increase the attenuating mode type content for improved noise suppression.

2. The combination according to claim 1 wherein individual strips of said first and second set of strips having approximately the same width.

3. In a noise-suppressing duct having mounted therein rotating mechanical equipment with first stage rotor and stator blades which interact to generate spinning mode acoustic pressure fields with propagating and attenuating type modes, said duct being a rigid longitudinally extending duct, the improvement which comprises

a first set of peripherally spaced, longitudinally extending strips of a first sound-absorbing material attached to the inner surface of said duct, said first set of strips being relatively narrow in the peripheral direction and equally spaced and in total number at least exceeding the number of first stage rotor blades,

a second set of at least several longitudinally spaced, peripherally extending strips of said first sound-absorbing material also attached to the inner surface of said duct and intersecting said first set of strips, said second set of strips being equally spaced in the longitudinal direction with a spacing less than one wavelength of sound at a selected frequency and further being mounted flush with said first set of strips,

said first set of peripherally spaced strips being effective to achieve scattering of the spinning mode acoustic pressure fields for improved noise suppression.

4. The combination according to claim 3 further including a third set of lining members of a second sound-absorbing material attached to the inner surface of said duct between said first and second set of strips and flush therewith,

said first and second sound-absorbing materials having different acoustical impedances.

5. In a noise-suppressing fan duct having an inlet duct and having mounted in said duct a compressor with first stage rotor and stator blades which interact to generate spinning mode acoustic pressure fields with propagating and attenuating type modes, said fan duct being a generally cylindrical rigid duct, wherein the improvement comprises

a circumferentially segmented acoustical treatment attached to the inner surface of said inlet duct and including a first set of circumferentially spaced, axially extending strips of a first sound-absorbing material, said first set of strips being relatively narrow in the circumferential direction and in total number at least exceeding the number of first stage rotor blades,

a second set of circumferentially spaced, axially extending strips of a second sound-absorbing material also attached to the inner surface of said inlet duct located between and alternating with said first set of strips so as to form a circumferentially continuous acoustic lining,

said first and second sound-absorbing materials having different acoustical impedances and said first and second set of strips further being mounted flush with one another,

said circumferentially segmented acoustical treatment being effective to achieve scattering of said spinning mode acoustic pressure fields to increase the attenuating type mode content for improved noise suppression.

6. The combination according to claim 5 wherein said circumferentially segmented acoustical treatment substantially covers the inner surface of said inlet duct.

7. The combination according to claim 5 wherein individual strips of said first and second set of strips have approximately the same width.

8. In a noise-suppressing fan duct having an inlet duct and having mounted in said duct a compressor with first stage rotor and stator blades which interact to generate spinning mode acoustic pressure fields with propagating and attenuating type modes, said fan duct being a generally cylindrical rigid duct, wherein the improvement comprises

a circumferentially segmented acoustical treatment attached to the inner surface of said inlet duct and including a first set of circumferentially spaced, axially extending strips of a first sound-absorbing material, said first set of strips being relatively narrow in the circumferential direction and in total number at least exceeding the number of first stage rotor blades,

an axially segmented acoustical treatment comprising a second set of at least several longitudinally spaced, peripherally extending strips of said first sound-absorbing material also attached to the inner surface of said inlet duct and intersecting said first set of strips, said second set of strips being equally spaced in the longitudinal direction with a spacing less than one wavelength of sound at a selected frequency and further being mounted flush with said first set of strips,

said circumferentially segmented acoustical treatment being effective to achieve scattering of the spinning mode acoustic pressure fields for improved noise suppression.

9. The combination according to claim 8 further including a third set of lining members of a second sound-absorbing material attached to the inner surface of said inlet duct between said first and second set of strips and flush therewith,

said first and second sound-absorbing materials having different acoustical impedances.