GAS TURBINE ENGINE PYLON ASSEMBLY AND GAS TURBINE ENGINE SYSTEM Russian patent published in 2014 - IPC B64D27/10

Abstract RU 2522208 C1

FIELD: engines and pumps.

SUBSTANCE: gas turbine pylon structure comprises inner engine nacelle arranged in engine central axis, outer nacelle arranged around inner nacelle to make fan stage to external airflow forced by blower. Besides it comprises pylon carrying inner and outer nacelles and extra gearbox arranged therein, axially and behind outer nacelle.

EFFECT: decreased weight, better engine cooling.

Similar patents RU2522208C1

Title	Year	Author	Number
GAS TURBINE ENGINE (VERSIONS)	2012	Marshall, Richard M.	RU2527815C2
GAS TURBINE ENGINE	2012	Susyu Gariel L. Merri Brajan D. Daj Kristofer M. Dzhonson Stiven B. Shvarts Frederik M.	RU2687861C2
GAS TURBINE ENGINE AND DISASSEMBLY OF ITS FRONT PART	2012	Otto Dzhon R. Sigal Brajan P. Sharma Sunil Dehvis Todd A.	RU2522344C2
GAS TURBINE ENGINE (VARIANTS)	2012	Suciu, Gabriel L. Merry, Brian D. Dye, Christopher, M. Johnson, Steven B. Schwarz, Frederick M.	RU2747543C1
GAS TURBINE ENGINE AND METHOD OF DISASSEMBLY OF ITS FRONT PART	2012	Otto Dzhon R. Sigal Brajan P. Sharma Sunil Dehvis Todd A.	RU2567483C2
GAS TURBINE ENGINE WITH DRIVE UNIT BOX	2022	Khasanov Rafis Zafarovich	RU2793638C1
GAS TURBINE ENGINE (VARIANTS)	2012	Devis Todd A. Rejnkhardt Gregori E. Dibenedetto Entso	RU2688073C2
METHOD OF GAS TURBINE ENGINE SERVICING (VERSIONS) AND GAS TURBINE ENGINE	2012	Sigal Brajan P. Dehvis Todd A.	RU2525038C2
GAS TURBINE ENGINE (VARIANTS)	2017	Sheridan, William G. Hasel, Karl L.	RU2676150C1
GAS TURBINE ENGINE	2014	Sheridan Uilyam G. Makkun Majkl E. Shvarts Frederik M. Kupratis Daniel Bernard Susyu Gabriel L. Akermann Uilyam K. Khazbend Dzhejson	RU2638709C2

RU 2 522 208 C1

Authors

Uinter Majkl

Dates

2014-07-10—Published

2013-01-14—Filed