公开(公告)号：US09834315B2

公开(公告)日：2017-12-05

申请号：US14570152

申请日：2014-12-15

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Charles Lo ,  Eric Blumer ,  Dan Laboda ,  Alexander Bershitsky

IPC: B01D19/00 ,  B64D37/34 ,  B01D35/02 ,  B01D46/00

CPC classification number: B64D37/34 ,  B01D19/0005 ,  B01D19/0047 ,  B01D19/0057 ,  B01D19/0068 ,  B01D35/02 ,  B01D46/00

Abstract: An aircraft fuel deoxygenation system includes a boost pump, a contactor-separator, and a centrifuge-separator pump. The boost pump is adapted to receive fuel from a fuel source and inert gas from an inert gas source, and is configured to mix the fuel and inert gas and supply a fuel/gas mixture. The contactor-separator is coupled to receive the fuel/gas mixture and is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel with entrained purge gas and separated purge gas. The centrifuge-separator pump is coupled to receive the deoxygenated fuel with entrained purge gas and is configured to separate and remove the entrained purge gas from the deoxygenated fuel and supply the deoxygenated fuel and additional purge gas.

公开(公告)号：US20170267369A1

公开(公告)日：2017-09-21

申请号：US15076274

申请日：2016-03-21

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ming Xu ,  Cristian Anghel ,  Eric Blumer ,  Wayne Pearson

IPC: B64D41/00 ,  B64D13/06 ,  B64D27/10

CPC classification number: B64D41/00 ,  B64D13/06 ,  B64D2013/0611 ,  B64D2013/0644 ,  B64D2041/002 ,  Y02T50/56

Abstract: A system for driving an environmental control system (ECS) of a vehicle with ground-based electrical power may include a turbine engine on board the vehicle, coupled to the ECS to pneumatically drive the ECS, and an electric machine, on board the aircraft, mechanically coupled to the turbine engine, to drive the turbine engine. A control system such that the electric machine provides motoring assistance to the turbine engine, and that the motoring assistance is limited to match the available current from the ground-based electrical power.

公开(公告)号：US20160319666A1

公开(公告)日：2016-11-03

申请号：US14701262

申请日：2015-04-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Eric Blumer ,  David K. Jan ,  Jason Smoke ,  Robbie Joseph Adams ,  Harry Lester Kington

IPC: F01D5/06 ,  F04D29/60 ,  F04D29/32 ,  F01D5/04 ,  F04D29/28

CPC classification number: F01D5/066 ,  B22F3/1055 ,  B22F3/15 ,  B22F5/009 ,  B22F2998/10 ,  B22F2999/00 ,  B23P15/006 ,  F01D5/04 ,  F01D5/3061 ,  F01D5/34 ,  F04D29/284 ,  F04D29/321 ,  F04D29/322 ,  F04D29/329 ,  F04D29/601 ,  F04D29/644 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/23 ,  F05D2230/31 ,  Y02P10/295 ,  Y02T50/671 ,  B22F7/062 ,  B22F7/08 ,  B22F2207/01

Abstract: Bladed Gas Turbine Engine (GTE) rotors including deposited transition rings are provided, as are embodiments of methods for manufacturing bladed GTE rotors. In one embodiment, the method includes providing an outer blade ring having an inner circumferential surface defining a central opening, and depositing a deposited transition ring on the inner circumferential surface of the outer blade ring. The outer blade ring can be a full bladed ring or an annular grouping of individually-fabricated bladed pieces. After deposition of the transition ring, a hub disk is inserted into the central opening such that the transition ring extends around an outer circumferential surface of the hub disk. The transition ring is then bonded to the outer circumferential surface of the hub disk utilizing, for example, a hot isostatic pressing technique to join the transition ring and the outer blade ring thereto.

Abstract translation: 提供了包括沉积的过渡环的叶片燃气轮机发动机（GTE）转子，如用于制造叶片GTE转子的方法的实施例。 在一个实施例中，该方法包括提供具有限定中心开口的内周表面的外部叶片环，以及在外部叶片环的内圆周表面上沉积沉积的过渡环。 外刀片环可以是全刀片环或单独制造的刀片的环形组。 在沉积过渡环之后，毂盘插入中心开口中，使得过渡环围绕毂盘的外周表面延伸。 然后使用例如热等静压技术将过渡环接合到轮毂盘的外周面，以将过渡环和外刀环连接到其上。

公开(公告)号：US20160061451A1

公开(公告)日：2016-03-03

申请号：US14475106

申请日：2014-09-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rodolphe Dudebout ,  Eric Blumer

IPC: F23R3/08 ,  F23R3/00

CPC classification number: F23R3/06 ,  F01D5/186 ,  F01D9/023 ,  F05D2260/202 ,  F23R3/002 ,  F23R3/04 ,  F23R2900/03041 ,  F23R2900/03042 ,  Y02T50/675

Abstract: A combustor for a turbine engine is provided. A first liner has a first surface and a second surface. A second liner forms a combustion chamber with the second side of the first liner, and the combustion chamber configured to receive an air-fuel mixture for combustion therein. The first liner defines a plurality of effusion cooling holes configured to form a film of cooling air on the second surface of the first liner. The plurality of effusion cooling holes includes a first effusion cooling hole extending from the first surface to the second surface and including an inlet portion extending from the first surface, a metering portion fluidly coupled to the inlet portion, and an outlet portion fluidly coupled to the metering portion and extending to the second surface. The inlet portion is larger than the metering portion.

Abstract translation: 提供了一种用于涡轮发动机的燃烧器。 第一衬垫具有第一表面和第二表面。 第二衬套形成具有第一衬里的第二侧的燃烧室，并且燃烧室被配置为容纳用于在其中燃烧的空气 - 燃料混合物。 第一衬套限定了多个排出冷却孔，其构造成在第一衬里的第二表面上形成冷却空气的膜。 多个排出冷却孔包括从第一表面延伸到第二表面的第一渗出冷却孔，并且包括从第一表面延伸的入口部分，流体连接到入口部分的计量部分，以及流体连接到 计量部分并延伸到第二表面。 入口部分大于计量部分。

公开(公告)号：US20150314229A1

公开(公告)日：2015-11-05

申请号：US14310531

申请日：2014-06-20

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Russell W. Johnson ,  Peter M. Michalakos ,  Eric Blumer ,  Alexander Bershitsky ,  Charles Lo

IPC: B01D53/047 ,  B01J19/24 ,  B01D53/22

CPC classification number: B01D53/047 ,  B01D19/0005 ,  B01D19/0026 ,  B01D53/225 ,  B01D53/229 ,  B01D53/864 ,  B01D2053/221 ,  B01D2256/10 ,  B01D2257/104 ,  B01D2257/702 ,  B01D2258/06

Abstract: An aircraft fuel deoxygenation and tank inerting system includes an inert gas source, a fuel deoxygenation system, and an air/fuel heat exchanger. The inert gas source is configured to supply inert gas having an oxygen concentration of less than 3%. The fuel deoxygenation system is adapted to receive fuel from a fuel source and the inert gas from the inert gas source. The fuel deoxygenation system is configured to remove oxygen from the fuel and thereby generate and supply deoxygenated fuel and oxygen-rich purge gas. The air/fuel heat exchanger is adapted to receive compressed air from a compressed air source and the deoxygenated fuel from the fuel deoxygenation system. The air/fuel heat exchanger is configured to transfer heat from the compressed air to the deoxygenated fuel, to thereby supply cooled compressed air and heated deoxygenated fuel.

Abstract translation: 飞机燃料脱氧和罐惰化系统包括惰性气体源，燃料脱氧系统和空气/燃料热交换器。 惰性气体源被配置为提供氧浓度小于3％的惰性气体。 燃料脱氧系统适于从燃料源接收燃料和来自惰性气体源的惰性气体。 燃料脱氧系统被配置为从燃料中除去氧气，从而产生和供应脱氧燃料和富氧吹扫气体。 空气/燃料热交换器适于接收来自压缩空气源的压缩空气和来自燃料脱氧系统的脱氧燃料。 空气/燃料热交换器被配置为将热量从压缩空气传递到脱氧燃料，从而供应冷却的压缩空气和加热的脱氧燃料。

公开(公告)号：US20140190347A1

公开(公告)日：2014-07-10

申请号：US13734875

申请日：2013-01-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Yates Wong ,  Eric Blumer ,  Eduardo Guerra ,  Yogendra Yogi Sheoran ,  Zedic Daniel Judd

IPC: F02C7/052

CPC classification number: F02C7/052 ,  F01D25/002 ,  F05D2260/607 ,  Y02T50/671 ,  Y02T50/675

Abstract: An inlet particle separator system for a vehicle engine includes a separator assembly and a liquid injection system. The separator assembly defines an inlet flow path for receiving inlet air and includes a scavenge flow path and an engine flow path downstream of the inlet flow path. The separator assembly is configured to separate the inlet air into scavenge air and engine air such that the scavenge air is directed from the inlet flow path into the scavenge flow path and the engine air is directed from the inlet flow path into the engine flow path. The liquid injection system is coupled to the separator assembly and configured to introduce a diffused liquid into the inlet air flowing through the separator assembly.

Abstract translation: 用于车辆发动机的入口颗粒分离器系统包括分离器组件和液体喷射系统。 分离器组件限定用于接收入口空气的入口流动路径，并且包括清除流动路径和在入口流动路径下游的发动机流动路径。 分离器组件构造成将入口空气分离成清空空气和发动机空气，使得清扫空气从入口流动路径引导到清除流动路径中，并且发动机空气从入口流动路径引导到发动机流动路径中。 液体注射系统联接到分离器组件并且构造成将扩散的液体引入流过分离器组件的入口空气中。