Thermal and fire protection for aircraft engine reversers.

According to FAA fireproofing regulations, commercial engine cowlings must be capable of withstanding a fuel-fed flame of 2000oF for fifteen minutes without flame penetration. To meet this requirement, there are two approved spray-on coatings, MA-25 S and 64-C1-2. For some time, many in the industry have been aware of reverser core failures resulting in heat induced degradation going unnoticed under spray-on coatings.

Hi-Temp Insulation provides removable reverser insulation blankets for CF6-6, CF6-50 and CF6-80 engine series. Each insulation blanket performs as a fireproof barrier in accordance with FAR 25.1191. The blanket tests were conducted in compliance with the criteria and requirements set forth in Federal Aviation Administration Advisory Circular AC 20-135. The insulation blankets prevent a burn through and/or backside ignition for a minimum of fifteen minutes.

Following is a list of the advantages removable insulation blankets offer over spray-on coatings. Many of these advantages where detailed in an article written for Aerospace Engineering by Paul Romnes, Engine Technical Services Maintenance Operations, United Airlines, San Francisco, CA.

Environmental:

  • Elimination of toxic emissions during the surface preparation and spray-on application of ablative insulation coatings.
  • Elimination of disposal problems associated with the coatings when removed for inspection and with the chemicals used during removal of the coatings.
  • Elimination of special training and handling.
  • Elimination of special purpose spray containment facilities.

Fit:

  • Blankets are manufactured to tool controlled tolerances.
  • Blankets are configured to pan down in specific areas to improve fit and avoid interference problems.
  • Blankets are designed around areas where insulation is not required, rather than applying a coating to the entire area, reducing overall weight.
  • Mechanical fasteners are used to precisely position and positively retain the blankets in place.

Consistency:

  • Blankets are not affected by high vibration levels of an in-flight environment that can cause fragile coatings to disintegrate.
  • Blankets are fabricated to tool-controlled dimensions.
  • Blanket thickness is controlled by both quilting the insulation core and heat curing the final lay-up under vacuum.
  • Blanket thermal efficiency is superior to coatings, and remains consistent due to controlled thickness and improved durability.

Durability:

  • Blankets are not as easily damaged as coatings during maintenance.
  • Blankets are more resistant to typical aircraft contaminants than coatings.
  • Blankets do not require top coats like those used as a binder for coatings.

Maintainability:

  • Blankets are easily repaired.
  • Blanket repair can be done "on-wing".
  • Blankets are easily removed and reinstalled for fan reverser inspections.

Inspections:

  • Reverser bond lines, between the hot-side surface and the honeycomb core, can be inspected more frequently due to improved accessibility.
  • With improved accessibility, a more reliable "tap test" and visual inspection can be performed.
  • Reversers require less repair time since coatings are not being removed and re-applied.

Cost:

  • Blankets last the life of the reverser under normal conditions.
  • Maintenance costs are reduced compared to removing and re-applying coatings.
  • Costly special handling, needed to use the highly toxic components of the coatings, is eliminated.
  • Products related to the coatings, that have a limited shelf life and must be stored, are eliminated.
  • Maintenance downtime for reverser removal and reinstallation, is reduced from ten days for coatings, to less than twelve hours for blankets.

Drawing Number

Application

Engine Model

Service Bulletin

Repair Specification

46M1015-301

MDC Left Hand

CF6-6

S/B 78-2011

33DOC0009

46M1016-301

MDC Right Hand

CF6-6

S/B 78-2011

33DOC0009

46M1019-301

MDC Left Hand

CF6-50

S/B 78-3012

33DOC0009

46M1020-301

MDC Right Hand

CF6-50

S/B 78-3012

33DOC0009

46M1035-301

BAC Left Hand

CF6-80C2

S/B 78-1045

33DOC0051

46M1036-301

BAC Right Hand

CF6-80C2

S/B 78-1045

33DOC0051

46M1035-303

ABI Left Hand

CF6-80C2

S/B TBD

33DOC0051

46M1036-303

ABI Right Hand

CF6-80C2

S/B TBD

33DOC0051

46M1035-303

MDC Left Hand

CF6-80C2

S/B TBD

33DOC0051

46M1036-303

MDC Right Hand

CF6-80C2

S/B TBD

33DOC0051

46M1039-301

ABI Left Hand

CF6-80E

S/B TBD

33DOC0051

46M1040-301

ABI Right Hand

CF6-80E

S/B TBD

33DOC0051

46M1043-301

ABI Left Hand

CF6-80A

S/B TBD

33DOC0051

46M1044-301

ABI Right Hand

CF6-80A

S/B TBD

33DOC0051

 

 

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