The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 20, 2022

Filed:

May. 22, 2020
Applicant:

Lufthansa Technik Ag, Hamburg, DE;

Inventors:

Jan Sassmannshausen, Hamburg, DE;

Eugen Roppelt, Hamburg, DE;

Assignee:

LUFTHANSA TECHNIK AG, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B25B 1/00 (2006.01); F01D 25/28 (2006.01); B25B 27/14 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); B25B 27/14 (2013.01); F05D 2230/72 (2013.01); F05D 2260/02 (2013.01); F05D 2260/38 (2013.01); F05D 2300/432 (2013.01);
Abstract

A tool holds and axially fixes a high-pressure shaft of an aircraft engine in a state where a high-pressure turbine stage is demounted. The tool includes: a shaft end cap having an inner radius, which is adapted to a predetermined shaft diameter, the shaft end cap plugs onto a turbine-side end of the high-pressure shaft; a shaft end cap receptacle receives the shaft end cap in a radially movable manner and in an axially limited manner in a first direction; a connector is fastenable to the shaft end cap receptacle and has a shank, which is insertable into the high-pressure shaft, the connector being configured to axially secure the shaft end cap receptacle; and a spring element, which is positionally fixed with respect to the shaft end cap receptacle, the spring element being configured to apply a predetermined spring force to the shaft end cap in the radial direction.


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