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:
Aug. 10, 2021

Filed:

May. 17, 2016
Applicant:

Mitsubishi Heavy Industries Aero Engines, Ltd., Aichi, JP;

Inventors:

Ryutaro Fujisawa, Tokyo, JP;

Tomoyuki Onishi, Tokyo, JP;

Yasuyuki Uetsuki, Tokyo, JP;

Tadayuki Hanada, Aichi, JP;

Yohei Fujimoto, Aichi, JP;

Takafumi Ota, Aichi, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/82 (2006.01); F02C 7/20 (2006.01); F01D 25/24 (2006.01); F23R 3/60 (2006.01); F02K 3/06 (2006.01); F02C 7/00 (2006.01);
U.S. Cl.
CPC ...
F02K 1/82 (2013.01); F01D 25/24 (2013.01); F02C 7/00 (2013.01); F02C 7/20 (2013.01); F02K 3/06 (2013.01); F23R 3/60 (2013.01); F05D 2220/323 (2013.01); F05D 2240/14 (2013.01); F05D 2260/30 (2013.01); F05D 2260/31 (2013.01); F05D 2260/941 (2013.01);
Abstract

An aircraft component is used in a gas turbine engine for an aircraft. The aircraft component includes an annular part having an outer peripheral surface, and a boss part protruding from the outer peripheral surface of the annular part in a radial direction. In the boss part, at least two through-holes are formed to penetrate the boss part in the radial direction at predetermined intervals. In the boss part around the two through-holes, a cut-out part where a part of the boss part is cut out is formed.


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