公开(公告)号：CA2865896A1

公开(公告)日：2013-09-12

申请号：CA2865896

申请日：2013-02-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OSORIO OMAR I

IPC: F02C7/224 ,  F02C3/04 ,  F02K3/06 ,  F02M31/08 ,  F02M31/125

Abstract: A fuel heating system for a gas turbine engine comprises a first heat exchanger, a second heat exchanger, a fuel pump and a valve. The first heat exchanger produces a heated air flow. The second heat exchanger receives the heated air flow from the first heat exchanger. The fuel pump provides a fuel flow. The valve is coupled to the fuel pump to intermittently include the second heat exchanger in the fuel flow based on a temperature of the fuel flow. A method of heating fuel in a gas turbine engine comprises providing fuel to a gas turbine engine with a fuel pump to sustain a combustion process, heating a flow of air with exhaust gas from the combustion process, and heating fuel from the fuel pump en route to the gas turbine engine with the flow of air based on a temperature of the fuel.

公开(公告)号：CA2865896C

公开(公告)日：2020-01-28

申请号：CA2865896

申请日：2013-02-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OSORIO OMAR I

IPC: F02C7/224 ,  F02C3/04 ,  F02K3/06 ,  F02M31/08 ,  F02M31/125

Abstract: A fuel heating system for a gas turbine engine comprises a first heat exchanger, a second heat exchanger, a fuel pump and a valve. The first heat exchanger produces a heated air flow. The second heat exchanger receives the heated air flow from the first heat exchanger. The fuel pump provides a fuel flow. The valve is coupled to the fuel pump to intermittently include the second heat exchanger in the fuel flow based on a temperature of the fuel flow. A method of heating fuel in a gas turbine engine comprises providing fuel to a gas turbine engine with a fuel pump to sustain a combustion process, heating a flow of air with exhaust gas from the combustion process, and heating fuel from the fuel pump en route to the gas turbine engine with the flow of air based on a temperature of the fuel.

公开(公告)号：EP2946088A4

公开(公告)日：2016-01-20

申请号：EP13871803

申请日：2013-01-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WONG CHUNG ,  VITALE JACK V ,  OSORIO OMAR I ,  CHEN DAIH-YEOU

IPC: F02C1/00 ,  F01D25/14 ,  F02C6/00 ,  F02C7/228 ,  F02C7/25

CPC classification number: F02C7/25 ,  F01D25/145 ,  F02C7/22 ,  F05D2220/50 ,  F05D2230/54 ,  F05D2240/15 ,  F05D2250/231 ,  F05D2250/37 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/675 ,  Y10T29/49828

Abstract: A gas turbine engine according to one disclosed non-limiting embodiment of the present disclosure includes an engine case, a multiple of fuel injectors mounted to the engine case, and a fire shield mounted to the engine case to surround at least one, but less than all, of the multiple of fuel injectors. In a further embodiment of the foregoing embodiment, the fire shield includes a sheet metal alloy layer. In the alternative or additionally thereto, in the foregoing embodiment the fire shield includes a composite cloth on an interior of the sheet metal alloy layer with respect to the engine case.

Abstract translation: 根据本公开的一个公开的非限制性实施例的燃气涡轮发动机包括发动机壳体，安装到发动机壳体上的多个燃料喷射器，以及安装到发动机壳体上的防火罩，以围绕至少一个但小于 全部是燃油喷射器的数量。 在上述实施例的另一实施例中，防火罩包括金属板合金层。 在替代或附加地，在前述实施例中，防火罩包括相对于发动机壳体在金属板合金层内部的复合布。