|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F16H-037/06 F16H-035/08 F16H-057/00|
|미국특허분류(USC)||74/661 ; 74/402 ; 74/410 ; 74/665L|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 43 인용 특허 : 1|
A drive system for a multiple gas turbine engine system includes power output shafts from first and second gas turbine engines, each power shaft connected to drive a load and each engine including a load sharing cross-over shaft for power transfer from one of the engines to the other engine; a right angle gear box assembly connects each of the power output shafts to the cross-over shaft and each of the right angle gear box assemblies includes first and second load sharing gear paths including tooth geometry in an input bevel gear configured to produce a ...
In a multiple engine drive system having first and second engines with an output shaft connected to drive a load and including a load sharing cross-over drive between each of the engine output shafts to maintain power transfer to each of the loads when one of the engines is disconnected from the system, the improvement comprising: a right angle gear box assembly connecting each of the output shafts to the cross-over drive, each gear box assembly having an input gear connected to one of the output shafts and an output gear connected to the cross-over driv...