公开(公告)号：US20190063367A1

公开(公告)日：2019-02-28

申请号：US15689218

申请日：2017-08-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Danis Burton Smith ,  Alexandre Guerinot ,  Remo Neri ,  James Thomas Ayers, III

IPC: F02K1/76 ,  F02K1/60

Abstract: A system and method for an improved thrust reverser is provided. The provided thrust reverser employs hidden linkage assemblies to decrease drag in the engine exhaust flow and increase turbine engine performance. The hidden linkage assemblies are placed in a space between the blocker door and the transcowl, thereby not affecting the engine exhaust flow.

公开(公告)号：US20210023927A1

公开(公告)日：2021-01-28

申请号：US16521068

申请日：2019-07-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Andrew Appleby ,  Laurence Liston ,  Remo Neri ,  Justin Mickelsen

IPC: B60K5/12 ,  B64D27/26

Abstract: A mount for coupling an engine to a vehicle includes an engine bracket to couple to the engine. The engine bracket includes a body that has a first end opposite a second end, and the body defines an offset coupling portion between the first end and the second end. The offset coupling portion protrudes from the body between the first end and the second end to define a receptacle. The mount includes a vehicle bracket to couple to the vehicle. The vehicle bracket includes a first bracket end opposite a second bracket end. The first bracket end is offset from the second bracket end and the first bracket end is received within the receptacle to couple the engine bracket to the vehicle bracket.

公开(公告)号：US20170204808A1

公开(公告)日：2017-07-20

申请号：US14997611

申请日：2016-01-18

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Danis Burton Smith ,  Robert Romano ,  John Taylor Pearson ,  Morris Anderson ,  Remo Neri

IPC: F02K1/62 ,  F02K1/76 ,  F01D25/24

CPC classification number: F02K1/62 ,  F02K1/72 ,  F02K1/763 ,  F05D2240/91 ,  F05D2250/34 ,  F05D2250/411 ,  F05D2260/50 ,  Y02T50/671

Abstract: A thrust reverser system for a turbine engine includes a support structure, a transcowl, and a door. The transcowl is mounted on the support structure and is axially translatable, relative to the support structure, between first and second positions. The door is pivotally coupled to the support structure and is rotatable, about a pivot axis, between stowed and deployed positions when the transcowl translates between the first and second positions, respectively. The door has an internal surface and a balance plane, and pressure forces acting along the balance plane effectively creates no moment about the pivot axis. The internal surface of the door has a first surface area forward of the balance plane and a second surface area aft of the balance plane, and the second surface area substantially exceeds the first surface area.