Fluid flow interruption device for fuel supply system for gas turbine, particularly aircraft gas turbine, comprises fluid passage which is formed in housing, where moving interruption element is locked in fluid passage in housing

摘要

The fluid flow interruption device comprises a fluid passage (2) which is formed in housing (1), where a moving interruption element (3) is locked in the fluid passage in the housing from a releasing position. The interruption element is arranged between a fluid inlet (5) and a fluid outlet (6).