公开(公告)号：WO2013154649A3

公开(公告)日：2014-03-20

申请号：PCT/US2013022388

申请日：2013-01-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: F02K3/02

CPC classification number: F02K3/06 ,  F02C3/107 ,  F02C7/36 ,  F05D2220/323 ,  F05D2250/44

Abstract: A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.

Abstract translation: 燃气涡轮发动机包括非常高速的低压涡轮机，使得由低压涡轮机的出口面积所规定的数量乘以低压涡轮转速的平方，与高压涡轮机的相同参数相比是在 在约0.5和约1.5之间。

公开(公告)号：WO2014007886A3

公开(公告)日：2014-03-13

申请号：PCT/US2013034045

申请日：2013-03-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  PICKFORD SIMON ,  ACKERMANN WILLIAM K ,  SNAPE NATHAN

IPC: F02C7/18 ,  F02C7/12

CPC classification number: F01D9/065 ,  F01D1/02 ,  F01D5/02 ,  F01D9/02 ,  F01D25/12 ,  F02C7/04 ,  F02C7/047 ,  F02C7/18 ,  F02C7/32 ,  F05D2220/30 ,  F05D2260/20 ,  F05D2260/213 ,  Y02T50/675

Abstract: An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.

Abstract translation: 示例性涡轮机组件包括涡轮机的鼻锥以及至少部分位于鼻锥内部的泵。 泵通过电机有选择地旋转以将空气传送至内部。

公开(公告)号：WO2014007884A2

公开(公告)日：2014-01-09

申请号：PCT/US2013034024

申请日：2013-03-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  PICKFORD SIMON ,  ACKERMANN WILLIAM K ,  SNAPE NATHAN ,  HIPSKY HAROLD W

CPC classification number: F01D25/12 ,  F01D25/02 ,  F01D25/14 ,  F02C7/04 ,  F02C7/047 ,  F02C7/055 ,  F02C7/14 ,  F02C7/18 ,  F02C7/185 ,  F05D2250/141 ,  F05D2250/232 ,  F05D2250/51 ,  F05D2260/213 ,  F05D2260/98 ,  Y02T50/675

Abstract: An example turbomachine assembly includes, among other things, a nose cone of a turbomachine. The nose cone provides an aperture that communicates air to an interior of the nose cone.

Abstract translation: 涡轮机组件的示例尤其包括涡轮机的鼻锥体。 鼻锥提供将空气连通到鼻锥内部的孔。

公开(公告)号：WO2014018142A2

公开(公告)日：2014-01-30

申请号：PCT/US2013037675

申请日：2013-04-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD ,  MERRY BRIAN D ,  ACKERMANN WILLIAM K

CPC classification number: F01D25/162 ,  F02C3/107 ,  F02C7/06 ,  F02K3/06

Abstract: A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5. The high pressure turbine is supported by a bearing positioned at a point where the first shaft connects to a hub carrying turbine rotors associated with the second turbine section.

Abstract translation: 燃气涡轮发动机包括超高速低压涡轮机，使得与低压涡轮机的相同参数相比，由低压涡轮机的出口面积乘以低压涡轮机转速的平方所确定的量处于 比率在约0.5和约1.5之间。 高压涡轮机由位于第一轴连接到承载与第二涡轮机部分相关联的涡轮机转子的轮毂的点处的轴承支撑。

公开(公告)号：WO2013154633A2

公开(公告)日：2013-10-17

申请号：PCT/US2013021641

申请日：2013-01-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GLAHN JORN A ,  ACKERMANN WILLIAM K ,  CRAWLEY CLIFTON J ,  STRIPINIS PHILIP S

IPC: F02C7/12 ,  F02C6/08

CPC classification number: F02C6/08 ,  F01D25/18 ,  F01D25/183 ,  F02C7/12 ,  F02C7/14 ,  F05D2260/601 ,  Y02T50/675

Abstract: A gas turbine engine includes a buffer system that includes a first circuit and a second circuit. The first circuit can communicate a first buffer supply air to a first portion of the gas turbine engine and the second circuit can communicate a second buffer supply air to a second portion of the gas turbine engine.

Abstract translation: 燃气涡轮发动机包括缓冲系统，该缓冲系统包括第一回路和第二回路。 第一回路可将第一缓冲器供应空气传送至燃气涡轮发动机的第一部分，并且第二回路可将第二缓冲器供应空气传送至燃气涡轮发动机的第二部分。

公开(公告)号：CA2856723A1

公开(公告)日：2013-10-17

申请号：CA2856723

申请日：2013-01-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: F02K3/02

Abstract: A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.

公开(公告)号：CA2854077A1

公开(公告)日：2013-08-08

申请号：CA2854077

申请日：2013-01-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  SUCIU GABRIEL ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD

IPC: F04D29/04

Abstract: A gas turbine engine includes a very high speed fan drive turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5. The high pressure turbine is mounted by bearings positioned at an outer periphery of a shaft driven by the high pressure turbine.

公开(公告)号：SG10201911799YA

公开(公告)日：2020-01-30

申请号：SG10201911799Y

申请日：2013-01-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

Abstract: A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.

公开(公告)号：CA2945265A1

公开(公告)日：2017-05-09

申请号：CA2945265

申请日：2016-10-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  SCHWARZ FREDERICK M ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD

IPC: F02C7/36 ,  F02C7/06

Abstract: A gas turbine engine according to an example of the present disclosure includes, among other things, a fan having one or more fan blades. A compressor section is in fluid communication with the fan. The compressor section includes a first compressor section and a second compressor section. A turbine section is in fluid communication with the compressor section. The turbine section includes a first turbine section and a second turbine section. The first turbine section has a first exit area at a first exit point and rotates at a first speed. The second turbine section has a second exit area at a second exit point and rotates at a second speed. A first performance quantity is defined as the product of the first speed squared and the first area. A second performance quantity is defined as the product of the second speed squared and the second area.

公开(公告)号：BR102014007285A2

公开(公告)日：2015-05-26

申请号：BR102014007285

申请日：2014-03-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCUNE MICHAEL E ,  HUSBAND JASON ,  SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD ,  SUCIU GABRIEL L ,  ACKERMANN WILLIAM K

IPC: F02C7/20

Abstract: Motor de turbina a gás um motor de turbina a gás inclui um suporte flexivel para um sistema de engrenagens de acionamento de ventoinha. Uma turbina de acionamento de ventoinha a alta velocidade aciona o sistema de engrenagens de acionamento da ventoinha.