公开(公告)号：JP2000186575A

公开(公告)日：2000-07-04

申请号：JP32057699

申请日：1999-11-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER RYAN K ,  GIRGENTI ALEXANDER P ,  KEVIN G VAN DUNN ,  TIZIANI PETER C ,  AVIS THOMAS B ,  PORTELINHA ANTONIO J

IPC: F02C7/32

Abstract: PROBLEM TO BE SOLVED: To minimize the damage of a gear box housing and an auxiliary machine in a rotor unbalance state like the fan blade loss state. SOLUTION: A mounting part 60 to mount an auxiliary machine 50 on a gear box comprises a mounting plate 62 connected to the auxiliary machine 50; links 64 and 66 to connect a first end part to the mounting plate 62 through a grommet 74 having elasticity, and a bush; brackets 68 and 70 to interconnect the links 64 and 66 and an engine case. In a normal engine working state, the auxiliary machine 50 is insulated in vibration from the engine case. In a high rotor unbalance state like during a loss of a fan blade, the grommet 74 being an elastic member is squeezed, the auxiliary machine 50 is coupled to an engine case, a load on a connection part between the gear box and the auxiliary machine is minimized, and damage due to a rotor unbalance load is minimized.

公开(公告)号：JP2003161167A

公开(公告)日：2003-06-06

申请号：JP2002290990

申请日：2002-10-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NIKKANEN JOHN P ,  MIGLIARO EDWARD F ,  ZYSMAN STEVEN H ,  AVIS THOMAS B

IPC: F01D25/00 ,  F01D9/06 ,  F02C9/18 ,  F02K3/04 ,  F02K3/075

Abstract: PROBLEM TO BE SOLVED: To provide an upgraded bleed deflector to be used within a gas turbine. SOLUTION: A bleed deflector comprises an inlet portion 22 which receives bleed air from an engine, a perforated top plate 44 through which bleed air is discharged into a fan duct 30, and an aerodynamically shaped strut which enables positioning of the perforated top plate 44 above the inner wall of the fan duct 30, and allows air for mixing to flow in the bottom of the perforated top plate 44. COPYRIGHT: (C)2003,JPO

公开(公告)号：DE69930360T2

公开(公告)日：2006-08-03

申请号：DE69930360

申请日：1999-12-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER RYAN K ,  GIRGENTI ALEXANDER P ,  AVIS THOMAS B ,  VAN DUYN KEVEN G ,  TIZIANI PETER C ,  PORTELINHA ANTONIO J

IPC: F02C7/32 ,  F01D21/04

Abstract: A mount (9) for a gearbox accessory (50) for a gas turbine engine substantially isolates the accessory (50) from direct mechanical loading from the engine case (22) during normal engine operating conditions and couples the accessory (50) to the engine case (22) during high rotor imbalance conditions to minimize interface loads between the gearbox (40) and the accessory (50). By coupling the gearbox (40) to the accessory (50), the two are displaced substantially in unison, thereby minimizing interface stresses therebetween. Various construction details of the mount for the gearbox accessories (50) are disclosed.

公开(公告)号：DE69930360D1

公开(公告)日：2006-05-11

申请号：DE69930360

申请日：1999-12-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER RYAN K ,  GIRGENTI ALEXANDER P ,  AVIS THOMAS B ,  VAN DUYN KEVEN G ,  TIZIANI PETER C ,  PORTELINHA ANTONIO J

IPC: F02C7/32 ,  F01D21/04

Abstract: A mount (9) for a gearbox accessory (50) for a gas turbine engine substantially isolates the accessory (50) from direct mechanical loading from the engine case (22) during normal engine operating conditions and couples the accessory (50) to the engine case (22) during high rotor imbalance conditions to minimize interface loads between the gearbox (40) and the accessory (50). By coupling the gearbox (40) to the accessory (50), the two are displaced substantially in unison, thereby minimizing interface stresses therebetween. Various construction details of the mount for the gearbox accessories (50) are disclosed.