FIELD: process engineering, aircraft engineering.
SUBSTANCE: invention relates to sealing compounds, particularly to sealing lower-density compound intended for sealing various assembly units and parts of aircraft structures (airframe, fuel tanks, etc.) operated in wide temperature range from -60°C to +130°C. Proposed compound comprises the following elements, weight parts, i.e. fluid thiokol - 100, adhesive additive - 6-14, carbon - 18 to 28, dibutyl phthalate - 3.2 to 6.5, melaniline - 0.9 to 1.05, manganese dioxide - 5.6 to 7.0, microspheres - 8 to 18, stearic acid - 0.028 to 0.38 and colophonium - 1 to 3.
EFFECT: higher tensile strength and heat resistance, longer life.
2 tbl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
ANTICORROSION SEALANT | 2023 |
|
RU2817353C1 |
METHOD OF PRODUCTION OF SEALING COMPOSITION | 2003 |
|
RU2263699C2 |
SEALING COMPOSITION | 2010 |
|
RU2436818C1 |
SEALING COMPOSITION | 1998 |
|
RU2153517C2 |
SEALING COMPOSITION (OPTIONS) | 2000 |
|
RU2205197C2 |
SEALING AND WATERPROOFING COMPOSITION | 2010 |
|
RU2434922C1 |
SEALANT COMPOSITION FOR BAND SEALER | 2014 |
|
RU2578157C1 |
COMPOSITION FOR PROTECTIVE COATING | 2006 |
|
RU2334158C1 |
SEALING AND WATERPROOFING COMPOSITION | 2010 |
|
RU2434921C1 |
SEALING AND WATERPROOFING COMPOSITION | 2010 |
|
RU2453573C1 |
Authors
Dates
2009-11-10—Published
2008-02-21—Filed