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PDF, 1.06 MB - Woodrow Wilson International Center for Scholars

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- 2 - S/NBF/T158<br />

compressed air passes through the apertures into the interior of the<br />

cylinder. This design was chosen owing to the difficulty of selecting<br />

suitable heat-resisting steel <strong>for</strong> the chamber. At present the<br />

interior per<strong>for</strong>ated cylinder is changed every 14 hours.<br />

6. Instead of an axial flow gas turbine there is fitted<br />

[1 group unrecovered] tangential flow turbine [1 group unrecovered]<br />

the latter [1 group unrecovered] checking.<br />

No. 639. MAY [MAJ][iii]<br />

T.N.: [a] Inserted by the translator.<br />

Comments: [i] ARSENIJ: Andrej Ivanovich ShEVChENKO.<br />

S/NBF/T158<br />

[ii] The following details relate to a jet aircraft engine.<br />

[iii] MAJ: Pavel Ivanovich FEDOSIMOV.<br />

.W.S. No. XY-50.2<br />

- 409 -

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