Automatically igniting gas flares
12474049 ยท 2025-11-18
Assignee
Inventors
- Anas H. Safar (Dhahran, SA)
- Abdulaziz H. Altijani (Al Khobar, SA)
- Mohammed A. Almubayedh (Dhahran, SA)
- Rashid O. Al-Rashidi (Dhahran, SA)
Cpc classification
F23G7/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23Q2/285
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23Q1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D15/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2207/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23Q1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Systems and devices for igniting a gas to be flared include: a body having an inlet and an outlet, the body defining a channel extending between the inlet and the outlet; an igniter operable to generate a spark at the outlet of the body; an actuator disposed in the channel, the actuator configured to harvest energy when the gas to be flared flows from the inlet to the outlet through the channel and transfer the energy to the igniter.
Claims
1. A system for igniting a gas to be flared, the system comprising: a body having an inlet and an outlet, the body defining a channel extending between the inlet and the outlet; an igniter operable to generate a spark at the outlet of the body; an actuator disposed in the channel, the actuator configured to harvest energy when the gas to be flared flows from the inlet to the outlet through the channel and transfer the energy to the igniter, and a flare tip, the flare tip incorporating the body.
2. The system of claim 1, further comprising a source of the gas to be flared, the source in fluid communication with the inlet of the body.
3. The system of claim 2, further comprising a conduit having a flare tip, the inlet of the body in fluid communication with the conduit and positioned to receive a portion of the gas to be flared.
4. The system of claim 3, wherein the outlet of the body is positioned to provide a spark or flame in the conduit.
5. The system of claim 2, wherein the channel of the body is a primary route through which the gas to be flared travels from the source to an outside environment.
6. The system of claim 2, wherein only a portion of the gas to be flared travels through the body.
7. The system of claim 1, further comprising a pilot ignition system.
8. The system of claim 1, wherein the actuator comprises a turbine.
9. The system of claim 8, wherein the actuator comprises a first member and a second member positioned in contact with the first member such that relative motion between the first member and the second member generates sparks.
10. The system of claim 9, wherein the turbine is operably coupled to the first member such that rotation of the turbine causes relative motion between the first member and the second member.
11. The system of claim 9, wherein the first member comprises a ferrocerium alloy and the second member comprises a material harder than the first member.
12. The system of claim 9, wherein the actuator further comprises a shaft of the turbine connected to a first pulley, a second pulley in communication with the first pulley such that the rotation of the first pulley causes rotation of the second pulley, the second pulley connected to the first member.
13. A device for igniting in a flare tip, the device comprising: a body having an inlet and an outlet, the body defining a channel extending between the inlet and the outlet; an igniter operable to generate a spark at the outlet of the body; an actuator disposed in the channel, the actuator configured to harvest energy when the gas to be flared flows from the inlet to the outlet through the channel and transfer the energy to the igniter, wherein the actuator comprises a turbine.
14. The device of claim 13, wherein the actuator comprises a first member and a second member positioned in contact with the first member such that relative motion between the first member and the second member generates sparks.
15. The device of claim 14, wherein the turbine is operably coupled to the first member such that rotation of the turbine causes relative motion between the first member and the second member.
Description
DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
DETAILED DESCRIPTION
(4) This specification describes an approach to automatically igniting gas flares. This approach includes mechanical devices that can be installed in a flare tip to ignite gas as the gas flows through the flare tip. These devices can be an integral part of flare tips or can be added on to existing flare tips to retrofit them. With the added devices, the flare tips can be self-ignited, for example, without additional utilities or power. These devices can be the primary source of ignition on the flare tip or can be a secondary source of ignition that can provide redundancy in igniting the flare tip.
(5)
(6) Ignition is the process through which combustion is initiated and occurs when a flammable mixture of fuel and oxidizer come in contact with a suitable ignition source. The energy for ignition can be obtained from a variety of sources such as direct contact with a spark or flame, static electricity, autoignition, autooxidation, and adiabatic compression.
(7) When the energy for ignition is supplied to the fuel-oxidizer mixture, the reactant bonds of the mixture rupture, producing intermediate species such as CH.sub.3, H, O, etc. Such species are extremely reactive and recombine to form the final combustion products CO.sub.2 and H.sub.2O. This reaction, once started, can continue until the reactants are consumed.
(8) The ignition energy of the gases to be flared is dependent on the composition of the gases, for example, sweet gas which mainly includes methane can have an ignition energy of 0.3 MJ while acid gas that contains hydrogen sulfide can decrease the ignition energy to 0.22 MJ. In some cases, the ignition energy of the gases to be flared can be between 0.2 to 0.35 MJ.
(9) In some cases, during relief scenarios the velocity profile of the gases being flared at the flare tip can range from Mach 0.3 (326 ft/s) to Mach 1 (1087 ft/s). In other cases, such as routine flaring activities, the velocity profile of the gases being flared can range from 0.5 to 1 ft/s.
(10) Flare tips can use a continuous flare pilot burner that is ignited by a flame front generator (FFG). An FFG is a device that sends a small burst of flame to the top of a flare stack, allowing the operator to ignite the pilot burner from ground level. FFG devices have been used to ignite flare pilot burners from a great distance such as 1 mile. Ignition devices should be designed for the particular equipment and the specific set of process conditions for which they will be used.
(11)
(12) In some implementations, the actuator 136 is operable to harvest energy from gases being flared with velocities of the gases at the flare tip up to 1087 ft/s to generate a spark to ignite the gases being flared. In some implementations, the actuator 136 can harvest energy from gases being flared with velocities at the flare tip in the range of 0.5 ft/s to 1 ft/s.
(13) The igniter 134 is operable to generate a spark at the outlet 140 of the body 132. The igniter 134 can be such that higher flaring events will generate larger and/or more sparks to increase the likelihood that the gases to be flared will ignite. The actuator 136 may comprise a first member and a second member in contact with the first member such that relative motion between the first member and the second member generates a spark or a plurality of sparks. If the actuator 136 is a turbine, the turbine may be operably connected to the first member such that the rotation of the turbine causes the relative motion between the first member and the second member.
(14) In some implementations, the first member of the igniter can comprise a pyrophoric alloy such as a ferrocerium alloy. The second member of the igniter can comprised of a harder material such as steel. The relative motion between the first member that is in contact with the second member can generate sparks with temperatures up to 6000 F. This can meet the ignition energy of the gases being flared.
(15) The body 132 may be incorporated into a flare tip. The flare tip may also comprise additional flare tip ignition devices such as a pilot burner with a flame front generator. The igniter 134 can be disposed near the top of the flare tip.
(16) The size and material of the device 130 can be dependent on the size of the flare tip, the capacity of the flare tip, and/or the type of flare tip (e.g., low temperature or high temperature). For example, a cold flare tip can use a device 130 including a stainless steel material.
(17)
(18) The flare tip of the conduit 154 may comprise additional ignition devices such as a pilot ignition system or a pilot burner with a flame front generator. The igniter 134 may be a secondary or redundant device for igniting the gas to be flared.
(19) The size and material of the system 150 can be dependent on the size of the flare tip, the capacity of the flare tip, and/or the type of flare tip (e.g., low temperature or high temperature). For example, a cold flare tip can use a device 130 including a stainless steel material.
(20) A number of embodiments of the invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the invention. For example, a device for igniting gases to be flared can include various elements based on the expected gas composition and velocity of the gases to be flared. Accordingly, other embodiments are within the scope of the following claims.