Control concept for closed loop Brayton cycle

Patent metadata

Field	Value
Publication number	US-10001065-B2
Application number	US-201615139003-A
Country	US
Kind code	B2
Filing date	Apr 26, 2016
Priority date	Apr 29, 2015
Publication date	Jun 19, 2018
Grant date	Jun 19, 2018

Abstract

An improved closed loop Brayton cycle for a power plant is provided that includes a heater, at least one turbine, a recuperator, at least one cooler, at least one compressor, a bypass line and a flap valve arrangement in a closed circuit in which working fluid is circulated to produce electricity via a generator. Depending upon the requirement, such as, in case of gird load disconnection, speed of a shaft-line to which the turbine, the compressor and the generator are configured is also required to be reduced without any impact on the pressure drop in the cycle. For that the non-tight flap valve arrangement is configured on each conduit between the heater and the at least one turbine in a closest possible proximity to each turbine inlet.

First claim

What is claimed is:

1. An improved closed loop Brayton cycle for a power plant, the cycle having a working fluid flowing therein for operation, the cycle, comprising:
a heater having an inlet and an outlet, the heater adapted to supply heat to the working fluid flowing in the cycle;
at least one turbine operable on expansion of the heated working fluid, and drivingly connected to a variable load via a shaft-line, each of the at least one turbine having an inlet and an outlet, wherein each inlet of the at least one turbine is connected to the outlet of the heater via a conduit;
a recuperator connected to the at least one turbine via each turbine outlet to receive expanded working fluid to cool thereto, and connected to the heater via the inlet of the heater;
at least one cooler connected to the recuperator to further cool the working fluid;
at least one compressor on the shaft-line and driven by the at least one turbine, the at least one compressor connected to the at least one cooler to receive and compress the working fluid to transfer to the recuperator to be heated by the expanded working fluid from the at least one turbine and supply to the heater; and
a non-tight flap valve arrangement configured on each conduit between the heater and the at least one turbine in a closest possible proximity to each turbine inlet to manage the mass flow of working fluid through the non-tight flap valve arrangement to control the shaft-line speed when the variable load is disconnected from a power grid.

2. The cycle as claimed in claim 1 , wherein the conduit comprises a recess where the non-tight flap valve arrangement is housed in the recess to substantially minimize pressure drop in the cycle upon normal operation.

3. The cycle as claimed in claim 2 , wherein the non-tight flap valve arrangement comprises:
a flap member; and
an attaching segment having a flap axle to pivotally attach the flap member, the attaching segment enables the attachment of the non-tight flap valve arrangement on the conduit to be housed at the recess,
wherein the flap member at an open position completely covers the recess and allows the working fluid to fully flow from the conduit to the at least one turbine, and
wherein the flap member at closed position is non-tight, which allows the conduit to be partially closed to enable the adjustment of the mass flow of working fluid to admit from the conduit to the at least one turbine.

4. The cycle as claimed in claim 3 , wherein the flap member is shaped to correspond the shape of the conduit to substantially minimize pressure drop in the cycle upon normal operation.

5. The cycle as claimed in claim 3 , further comprising a covering arrangement adapted to cover the recess and the non-tight flap valve arrangement and block exiting of the working fluid from the cycle.

6. The cycle as claimed in claim 3 , wherein the non-tight flap valve arrangement in closed position is non-tight, in which the flap member is configured to pivotally swing along the flap axel that enables the flap member to be partially opened to allow the working fluid with adjusted mass flow to pass from the conduit.

7. The cycle as claimed in claim 3 , wherein the non-tight flap valve arrangement is a self-closing non-tight flap valve arrangement that is adapted to be partially closed in response to disconnection of the variable load from the power grid.

8. The cycle as claimed in claim 7 , wherein the self-closing non-tight flap valve arrangement is controlled via an electronic module.

Assignees

• Alstom Technology Ltd
• General Electric Technology Gmbh

Inventors

• Laffont Patrick

Classifications

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• F04D29/321

  for axial flow compressors · CPC title

• F01D17/148

  by means of rotatable members, e.g. butterfly valves · CPC title

• F01D17/105

  by passing part of the fluid · CPC title

• F05D2270/091

  in particular sudden load loss · CPC title