FRANGIBLE STRUT FOR GAS TURBINE ENGINE

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FRANGIBLE STRUT FOR GAS TURBINE ENGINE

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SUBBARAYACHAR MANJUNATH / THOKALA ANIL KUMAR / SHIVAPRAKASH JAYANTH HIREBELAGULY / KADAM PAVANKUMAR / KUMAR AVINASH

A frangible strut for a gas turbine engine includes a first end to couple to a first structure of the gas turbine engine, and a second end opposite the first end. The second end is to couple to a second structure of the gas turbine engine. The second end includes an outer portion coaxial with and spaced radially apart from an inner portion. The inner portion is to receive a fastening device to couple the second end to the second structure. The outer portion is coupled to a body of the frangible strut. The inner portion is interconnected to the outer portion by a plurality of frangible members that are spaced apart about a perimeter of the inner portion, and each of the frangible members are configured to release the inner portion from the outer portion. The frangible strut includes the body interconnecting the first end and the second end.

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Title :

FRANGIBLE STRUT FOR GAS TURBINE ENGINE

Additional title:

ZERBRECHLICHE STREBE FÜR EINEN GASTURBINENMOTOR
ENTRETOISE FRANGIBLE POUR MOTEUR À TURBINE À GAZ

Contributors:

SUBBARAYACHAR MANJUNATH (author) / THOKALA ANIL KUMAR (author) / SHIVAPRAKASH JAYANTH HIREBELAGULY (author) / KADAM PAVANKUMAR (author) / KUMAR AVINASH (author)

Publication date :

2022-08-17

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS