TY  - JOUR
AB  - The entrance 6 of a passage leading cooling air to the cylinders of an aircraft engine comprises an adjustable flap valve 10, which opens outwardly and is inwardly streamlined. The engine is surrounded by a streamlined cowling 4 and the entrance 6 is slightly offset to the bank of cylinders 3, the exit being on the opposite side of the cowling. In a radial‐cylinder engine a separate air passage is provided for each bank of cylinders.
VL  - 4
IS  - 11
SN  - 0002-2667
DO  - 10.1108/eb029622
UR  - https://doi.org/10.1108/eb029622
PY  - 1932
Y1  - 1932/01/01
TI  - Month in the Patent Office: A Selection of the More Important Aircraft and Engine Specifications Published Recently
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 294
EP  - 294
Y2  - 2024/09/20
ER  -