Air conduction system
AssigneeMTU Aero Engines AG
InventorNils Busch
Life of this patent
Estimating the term…
Abstract
The invention relates to an air conduction system for an aircraft engine with a primary flow channel and a branch channel, in which, in particular, the branch channel can be a secondary flow channel and/or a bleed air channel, wherein the branch channel branches off the primary flow channel at a connecting region, comprising a closing device arranged at or in the connecting region for separating the branch channel from the primary flow channel, wherein the closing device has at least one closing ring for closing the connecting region.
Claims13
An air conduction system for an aircraft engine with a primary flow channel and a branch channel, wherein the branch channel is a secondary flow channel and/or a bleed air channel and wherein the branch channel branches off the primary flow channel at a connecting region, comprising:
- a closing device arranged at or in the connecting region for separating the channel from the primary flow channel;
- wherein the closing device has at least one closing ring for closing the connecting region.
Dependencies are inferred from the claim text.