|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-001/04 F01N-001/02 F01N-001/08 F01N-001/12 F02K-001/00 F01N-001/00|
|미국특허분류(USC)||181/213; 181/250; 181/273; 181/274; 181/276; 181/279; 415/119; 060/770|
|우선권정보||DE-10 2010 026 834 (2010-07-12)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 28|
A gas-turbine exhaust cone includes a cone shaped outside cone 1 closed in a flow direction, an inside cone 2 arranged in the outside cone 1 over at least part of the length of the exhaust cone, with the inside cone 2 being connected to the outside cone 1 via at least one helical partition wall 3, thereby forming an interspace 4 between the outside cone 1 and the inside cone 2. The interspace 4 is connected to inlet openings 5 at its inflow side and opens at an exit side 6 towards an interior 7 of the outside cone 1. A dampening element 8 is arranged in ...
1. A gas-turbine exhaust cone, comprising: a cone shaped outside cone closed in a flow direction;an inside cone positioned within the outside cone over at least part of a length of the exhaust cone;at least one partition wall spirally arranged between the outside cone and the inside cone and connecting the inside cone to the outside cone in a spaced apart manner to form an interspace between the outside cone and the inside cone;at least one inlet opening connected to the interspace at an inflow side thereof, the interspace opening at an exit side towards...