Device and Method for Treating a Gas Flow
20170189849 ยท 2017-07-06
Inventors
Cpc classification
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/14
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01D2257/708
PERFORMING OPERATIONS; TRANSPORTING
B01D53/1425
PERFORMING OPERATIONS; TRANSPORTING
B01D2258/0258
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A device and a method treats a gas flow. Combustible components are separated from a first gas flow by means of an absorption process using a liquid medium in an absorption device; the components dissolved in the liquid medium are deposited into a second gas flow by means of a desorption process in a desorption device; and the concentration of combustible components in the second gas flow is set to a specified value. The second gas flow with the combustible components is additionally supplied to a gas turbine as fuel in order to generate electric energy and heat. A virtually energy-neutral exhaust air purification process is possible using the proposed device and method.
Claims
1. A device for treating a gas stream, having at least an absorption device which is suitable for removing flammable constituents from a first gas stream by absorption using a liquid medium; a desorption device which is suitable for separating flammable constituents dissolved in the liquid medium into a second gas stream; and a gas turbine, wherein the flammable constituents in the second gas stream have a concentration which can be set to a predetermined value; and wherein the gas turbine is supplied with the second gas stream, containing the flammable constituents, as fuel.
2. The device as claimed in claim 1, wherein the gas turbine is supplied with no other fuel in addition to the second gas stream containing the flammable constituents.
3. The device as claimed in claim 1, wherein the absorption device comprises the following: a carrier arrangement having an inlet and an outlet for the liquid medium, the carrier arrangement being configured such that, between the inlet and the outlet, the liquid medium is guided past a number of carriers having a surface and forms a flowing liquid film on the surface of the carriers; and a gas stream guide which is configured such that the first gas stream comes into contact with the flowing liquid film on the surface of the number of carriers.
4. A method for treating a gas stream, having the steps of: removing flammable constituents from a first gas stream by absorption using a liquid medium; separating the flammable constituents dissolved in the liquid medium into a second gas stream by desorption wherein the flammable constituents in the second gas stream have a concentration; setting the concentration of flammable constituents in the second gas stream to a predetermined value; and supplying the second gas stream, containing the flammable constituents, as fuel to a gas turbine.
5. The method as claimed in claim 4, wherein the gas turbine is supplied with no other fuel in addition to the second gas stream containing the flammable constituents.
6. The device as claimed in claim 2, wherein the absorption device comprises the following: a carrier arrangement having an inlet and an outlet for the liquid medium, the carrier arrangement being configured such that, between the inlet and the outlet, the liquid medium is guided past a number of carriers having a surface and forms a flowing liquid film on the surface of the carriers; and a gas stream guide which is configured such that the first gas stream comes into contact with the flowing liquid film on the surface of the number of carriers.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The invention will be explained in greater detail below, with reference to the appended drawings, in which identical reference signs denote identical or functionally equivalent elements, and in which:
[0017]
[0018]
[0019]
[0020]
DETAILED DESCRIPTION
[0021]
[0022] As shown in greater detail in
[0023] The desorption device 20 has a column 21 supplied with the liquid medium A, which is heated and charged with flammable constituents. The liquid medium A is added to the head of the column 21 and, in counter-flow to the liquid medium A, air is supplied as a second gas stream G so as to be enriched with the flammable constituents from the liquid medium A. Thus, the liquid medium A can be regenerated, collected in the sump of the column 21 and subsequently returned, clean, to the absorption device 10. Also, the second gas stream G can be enriched with the flammable constituents, such that it is possible to create a gas stream G which is suitable for combustion in a micro-gas turbine. In particular, the desorption device 20 is configured such that the concentration of flammable constituents in the second gas stream G which is suitable for combustion can be set to a predetermined value. This can be achieved for example by regulating the volumetric flow of the gas stream G.
[0024] A suitable flammable constituent in the second gas stream is for example butanol, combustion in a micro-gas turbine being possible for a concentration of at least 1.8 g of butanol per cubic meter of air. Especially suitable for combustion is a concentration in the range of 3.3-3.8 g of butanol per cubic meter of air.
[0025] Combustion of the second gas stream G takes place in a micro-gas turbine 30 which is illustrated schematically and by way of example in
[0026] After natural gas E has been supplied, possibly for starting the turbine, the supply of natural gas is switched off and combustion in the combustion chamber is sustained only by the gas stream G, which contains both the combustion air and the flammable constituent as fuel. Conventional flashback prevention means may be provided between the combustion chamber 33 and the compressor 37 in order to restrict combustion to the combustion chamber 33. For starting the turbine, the combustion chamber 33 contains an ignition device. The hot combustion gases are then expanded in the turbine 34, in order to thus drive the air compressor 37 and a generator 35 for electricity generation. A suitable generator 35 is for example a permanent magnet generator, which can be operated without interconnection of a mechanical gearing.
[0027] The generator generates electrical energy S which can subsequently be used for example for operating the absorption device 10, the desorption device 20, or for feeding into the electrical grid. Furthermore, the exhaust gas heat exchanger 38 provides hot gas H which can be further used in processes such as heating the liquid medium A in the desorption device 20.
[0028] The proposed device makes it possible to clean an exhaust air stream and simultaneously permits the generation of electrical energy and heat, in order to thus permit almost energy-neutral exhaust air cleaning.