IP Library › Granted Patent US 10,865,651
Granted Patent B2
US 10,865,651 · App. 16/183,357 · Granted Dec 15, 2020

Sealing assembly for a fluid kinetic machine, method for producing a sealing assembly as well as fluid kinetic machine

Inventors: Markus Schlemmer (Mainburg/Sandelzhausen, DE); Klaus Pirker (Klagenfurt, AT); Ralph Kropp (Wartenberg, DE); Lorenz Vinke (Arnsberg, DE); Waldemar Wiebe (Arnsberg, DE)
Assignees: MTU Aero Engines AG; Almecon Technologie GmbH
F01D11/001F01D11/003F16J15/444F05D2230/234F05D2230/54F05D2240/55F05D2240/56F05D2250/283F05D2250/75
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,865,651
App. No.
16/183,357
Granted
Dec 15, 2020
Kind
B2
Abstract

The invention relates to a sealing assembly for a fluid kinetic machine, in particular for an aircraft engine, for sealing a radial gap between a rotor and a stator, including at least one sealing support for retaining and/or fixing at least one sealing element, wherein the sealing support includes a first and a second radial web extending in a radial extension direction as well as an axial web extending in an axial extension direction, firmly bonded to the radial webs, and the radial webs form a receptacle for receiving an element of the stator. Therein, the radial webs are formed as sheet elements formed elongated in radial direction, wherein a radially interior end of the radial webs is respectively firmly bonded, in particular welded, to a radially exterior surface of the axial web.

Claims (15)

1. A sealing assembly for an aircraft engine, for sealing a radial gap between a rotor and a stator, including at least one sealing support for retaining and/or fixing at least one sealing element, wherein each sealing support includes a first and a second radial web extending in a radial extension direction as well as an axial web extending in an axial extension direction, firmly bonded to the radial webs, and the radial webs form a receptacle for receiving an element of the stator, wherein the radial webs are formed as flat sheet elements formed elongated in the radial direction, wherein a radially interior, non-bent end of the radial webs is respectively firmly bonded to a radially exterior surface of the axial web edge to edge.

2. The sealing assembly according to claim 1 , wherein the radial webs are welded to the radially exterior surface of the axial web.

3. The sealing assembly according to claim 2 , wherein the welding is effected by a laser.

4. The sealing assembly according to claim 2 , wherein the welding is performed in a direction, which is inclined to the radial and axial direction of a fluid kinetic machine and the sealing support, respectively, at an angle between 30° and 60°, preferably 115°.

5. The sealing assembly according to claim 1 , wherein the axial web is formed as a sheet element.

6. The sealing assembly according to claim 1 , wherein the sealing support is T-shaped such that the axial web extends beyond a connection area between the radial webs and the axial web on both sides in the axial direction.

7. The sealing assembly according to claim 1 , wherein an axially extending outer flange is formed at a radially outer end of at least one of the radially extending radial webs.

8. The sealing assembly according to claim 1 , wherein the sealing assembly includes a front ring or a front ring segment and/or a rear ring and/or a rear ring segment viewed in a flow direction, wherein the front ring or the front ring segment is connected to the first radial web and/or the rear ring or the rear ring segment is connected to the second radial web in a force-fit and/or firmly bonded manner.

9. The sealing assembly according to claim 8 , wherein the front ring or the front ring segment and/or the rear ring or the rear ring segment are formed as sheet elements.

10. The sealing assembly according to claim 1 , wherein the element of the stator is a blade foot or a blade foot segment of a guide blade ring, a guide blade ring segment or a guide blade of a fluid kinetic machine.

11. The sealing assembly according to claim 1 , wherein at least one slide stone is arranged between the radial webs and connected to them by at least one axial bolt.

12. The sealing assembly according to claim 1 , wherein the sealing element is formed as a honeycomb or brush seal.

13. The sealing assembly according to claim 1 , wherein the sealing assembly is a static inner air seal ring or a ring segment thereof.

14. The sealing assembly according to claim 1 , wherein the axial web is formed as a sheet element.

15. The sealing assembly according to claim 1 , wherein at least one sealing assembly is configured and arranged in a fluid kinetic machine.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 24, 2019
From: SCHLEMMER, MARKUS; PIRKER, KLAUS; KROPP, RALPH; VINKE, LORENZ; WIEBE, WALDEMAR
To: MTU AERO ENGINES AG; ALMECON TECHNOLOGIE GMBH
Reel/Frame 048120/0583 →
Priority Claims (1)
EP 17200845 · Nov 9, 2017 · regional
Continuity (1)
Related Publication 20190136705A1 · May 9, 2019
Cited By (2)
US 12,467,374 US 12,607,130