FIELD: aerospace engineering.
SUBSTANCE: invention relates to aerospace engineering, in particular, to compensating elements incorporated with pneumohydraulic system lines. Proposed compensator comprises compensating elements, flanges and pipes. It also comprises, at least, two sections of thin-wall pipes with flutes arranged at an angle to each other approximating to slant angle. Note that the pipeline is furnished with tie-rod that have spherical joints on its ends, one end being jointed to the pipeline centre, the other one being linked up with the fixed rigidly fastened element. Note here that the said tie-rod goes as close as possible to the position perpendicular to the plane wherein aforesaid sections of thin-walled pipes with flutes are located.
EFFECT: higher reliability of compensator operation.
2 dwg
Title | Year | Author | Number |
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COMPENSATOR (VERSIONS) | 2007 |
|
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TUYERE APPARATUS OF BLAST FURNACE | 0 |
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SU1748651A3 |
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Authors
Dates
2009-08-10—Published
2007-07-02—Filed