System for reducing aircraft noise and hush kit

• US 4,836,469 A
• Filed: 05/29/1987
• Issued: 06/06/1989
• Est. Priority Date: 05/29/1987
• Status: Expired due to Term

• Current Assignee: ROHR Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Valsan Partners Limited Partnership
• Inventors: Wagenfeld, Robert E.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Corl, Rodney
• Application Number:
  US07/055,635
• Time in Patent Office: 739 Days
• Field of Search: 244/1 N, 244/55, 181/213, 181/220, 181/222, 181/296
• US Class Current: 244/1.00N
• CPC Class Codes: B64D 2033/0206 comprising noise reduction means, e.g. acoustic liners
• CPC Class Codes: B64D 33/04 of exhaust outlets or jet pipes exhaust outlets for combustion engines in general F01N; jet pipes or nozzles for jet-propulsion plants per se F02K; plants characterised by the form or arrangement of the jet pipe or nozzle F02K ; attitude, flight direction, or altitude control by jet reaction B64C
• CPC Class Codes: F02K 1/46 Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing F02K1/28, F02K1/36, F02K1/38 take precedence
• CPC Class Codes: F02K 1/827 Sound absorbing structures or liners

Abstract

A system is provided for existing three-engine jet aircraft to reduce the noise levels at take-off and landing in order to meet governmental noise regulations. The system is particularly suitable for 727-200 aircraft having three JT8D engines. A hush kit is formed of the modified components for installation in existing airplanes.

Claims

1. A method for quieting jet engine noise produced by an airplane having three jet engines upon take-off and landing, comprising:

(a) replacing two outboard-mounted jet engines at the rear of the fuselage with jet engines which produce lower noise and greater thrust;

(b) retaining a center fuselage-mounted jet engine, and removing a thrust reverser from the aft position thereof;

(c) mounting a forced-air mixer on the center engine at the position from which the thrust reverser was removed, the mixer being adapted to combine cold air passing around the engine with hot air passing through the engine, to reduce engine noise emitted by the center engine; and

(d) mounting an acoustic nozzle comprised of sound-attenuating material aft of the forced-air mixer on the center engine,

whereby the noise level produced the airplane is reduced to a sufficiently quiet level to meet governmental noise regulations while remaining airworthy and permitting operation without reduced payloads or thrust.

2. A method as in claim 1 further comprising replacing two outboard-mounted nacelles with larger nacelles to accommodate the two replaced outboard-mounted jet engines at the rear of the fuselage.

3. A method as in claim 2 further comprising fitting heavier struts for the two replacement outboard-mounted nacelles for the two outboard-mounted jet engines at the rear of the fuselage.

4. A hush kit for adapting a jet airplane having two jet engines mounted on the rear of the fuselage and one jet engine mounted on the empennage, so as to meet governmental noise level regulations, comprising:

(a) two nacelles adapted to be mounted to the rear sides of the fuselage, each containing a jet engine having lower noise and greater thrust then the outboard mounted jet engines on the airplane;

(b) means adapted for mounted the nacelles to the fuselage;

(c) a forced-air mixer adapted to be fitted to the empennage-mounted jet engine; and

(d) a nozzle lined with sound-attenuating material on the airflow surfaces thereof and adapted to be mounted aft of the forced-air mixer,

whereby the components of the kit are adapted to be substituted for existing components of the airplane to facilitate reduction of engine noise during take-off and landing of the airplane.