公开(公告)号：JP2013079645A

公开(公告)日：2013-05-02

申请号：JP2012211687

申请日：2012-09-26

Applicant: United Technologies Corp ,  ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation

Inventor： MAALOUF FADI S ,  DITOMASSO JOHN C

IPC: F02C7/00 ,  F02K3/06

CPC classification number: F01D25/28 ,  F01D25/246 ,  F02C7/20 ,  F02K3/06 ,  Y02T50/672

Abstract: PROBLEM TO BE SOLVED: To provide a strut rod which achieves a structural guide vane capable of withstanding normal load conditions and sudden load conditions on an engine while minimizing noise.SOLUTION: A fan exit case includes structural guide vanes 28 and strut rods 30. The vane 28 is connected to a center body 34 in an inner circumferential end part 36, and connected to an outer circumferential side case 32 in an outer circumferential end part 38. Moreover, the rod 30 is connected to the center body 34 in an inner circumferential side end part 40, and is connected to the outer circumferential side case 32 in an outer circumferential side end part 42. The vane 28 recedes so that connection of the vane 28 to the center body 34 in the inner circumferential side end 36 is made at a location closer to a fan 12 than connection of the vane 28 to the outer circumferential side case 32 in the outer circumferential side part 36. The rod 30 is connected with an A-type frame configuration so that the outer circumferential side end part 42 of the two rods 30 are connected to the outer circumferential side case 32 at the section closer to each other.

Abstract translation: 要解决的问题：提供一种支柱，其实现能够在发动机上承受正常负载条件和突然负载条件的结构导叶，同时使噪声最小化。 解决方案：风扇出口外壳包括结构导向叶片28和支柱30.叶片28连接到内周端部36中的中心体34，并且在外周侧连接到外周侧壳体32 此外，杆30在内周侧端部40连接到中心体34，并且在外周侧端部42连接到外周侧壳体32.叶片28后退，使得 在外周侧部36中，将叶片28与中心体34的连接形成在比叶片28与外周侧壳体32的连接更靠近风扇12的位置。杆 30与A型框架结构连接，使得两个杆30的外周侧端部42在彼此更靠近的部分处连接到外周侧壳体32。 版权所有（C）2013，JPO＆INPIT

公开(公告)号：JPH11229897A

公开(公告)日：1999-08-24

申请号：JP34089098

申请日：1998-12-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NIKKANEN JOHN P ,  SANDAHL STEVEN D ,  ZYSMAN STEVEN H ,  DITOMASSO JOHN C

IPC: F02C7/18 ,  F02C7/04 ,  F02C7/12 ,  F02K1/48

Abstract: PROBLEM TO BE SOLVED: To enable the prevention of damage by foreign matter such as ice without installing complicated valve means. SOLUTION: An outlet/inlet module is disclosed which has both an inlet 58 and an outlet 62 for a heat exchanger system. The heat exchanger system 54 is placed in a cavity portion within a nacelle core chamber and communicates to a fan bypass duct through an inlet duct 76 which slopes down suddenly in a radially inward direction, and an exhaust duct 86. Weight ratio and aerodynamic performance of the system have been improved. A module is comprised of an integrated cast with a lobe shaped mixer 94 at the outlet thereof.

公开(公告)号：DE69816013D1

公开(公告)日：2003-08-07

申请号：DE69816013

申请日：1998-12-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NIKKANEN JOHN P ,  SANDAHL STEVEN D ,  ZYSMAN STEVEN H ,  DITOMASSO JOHN C

IPC: F02C7/18 ,  F02C7/04 ,  F02C7/12 ,  F02K1/48

Abstract: An inlet and outlet module (108) having both an inlet (58) and an outlet (62) for a heat exchanger system (52) is disclosed. Various construction details which improve the stiffness to weight ratio and the aerodynamic smoothness are developed. In one embodiment, the module (108) is formed of a one piece casting having a lobed mixer (94) at the outlet.

公开(公告)号：DE69816013T2

公开(公告)日：2004-04-01

申请号：DE69816013

申请日：1998-12-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NIKKANEN JOHN P ,  SANDAHL STEVEN D ,  ZYSMAN STEVEN H ,  DITOMASSO JOHN C

IPC: F02C7/18 ,  F02C7/04 ,  F02C7/12 ,  F02K1/48

Abstract: An inlet and outlet module (108) having both an inlet (58) and an outlet (62) for a heat exchanger system (52) is disclosed. Various construction details which improve the stiffness to weight ratio and the aerodynamic smoothness are developed. In one embodiment, the module (108) is formed of a one piece casting having a lobed mixer (94) at the outlet.

公开(公告)号：EP2904252A4

公开(公告)日：2015-12-09

申请号：EP13843942

申请日：2013-03-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： POPE ANDREW ,  YUDICHAK DAVID J ,  LUCASHU JOHN P ,  REINHARDT GREGORY E ,  DITOMASSO JOHN C ,  CONNER STEVEN L ,  KLINETOB CARL BRIAN ,  LEROUX JASON

IPC: F01D5/14 ,  F02C3/00 ,  F02C7/00 ,  F02K3/00 ,  F02K99/00

CPC classification number: F01D9/02 ,  F01D1/02 ,  F01D5/147 ,  F01D9/041 ,  F05D2230/23 ,  F05D2240/12 ,  Y02T50/671

Abstract: A static guide vane for use in a fan section of a gas turbine engine includes an outer platform and an inner platform. The inner and outer platforms are connected by an airfoil. The airfoil have channels extending into a main body of the airfoil to reduce the weight of the vane. A cover closes off the channels with the cover providing a portion of the airfoil.

Abstract translation: 用于燃气涡轮发动机的风扇部分的静态导向叶片包括外平台和内平台。 内外平台通过翼型连接。 翼型件具有延伸到翼型件的主体中的通道，以减小叶片的重量。 盖子封闭通道，盖子提供翼型的一部分。

公开(公告)号：EP2973869A4

公开(公告)日：2016-03-30

申请号：EP14769073

申请日：2014-03-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ANDERSON CARNEY R ,  DITOMASSO JOHN C

IPC: H01R4/66 ,  B64D45/02 ,  F16B1/00 ,  F16B19/02 ,  H01R4/30 ,  H01R4/64 ,  H02G13/00

CPC classification number: B64D45/02 ,  F16B19/02 ,  F16B2001/0064 ,  H01R4/308 ,  H01R4/64 ,  H01R2201/26 ,  H02G13/40

Abstract: A grounding sleeve for grounding an electrically insulated element disposed between two metal components includes an annular body extending between a first end and a second end. At least one window is formed in the annular body between the first end and the second end.