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Monthly Archives: diciembre 2012

KRIGING GEOSTATISTICAL DEFINITION




A geostatistical method of interpolating spatial data between locations at which values are known, using a linear combination of weights to the known data based on a model of spatial correlation. Usually involves estimating values based on measurements in boreholes. Kriging tends to produce average values. In simple kriging, the global mean is constant over the entire area; it is generally based on all the control points. In ordinary kriging, the local mean varies and is re-estimated based on the points in the moving neighborhood. Named for Daniel. G. Krige, South African mining engineer.



NODAL ANALYSIS – PETROLEUM ENGINEERING




INTRODUCTION TO NODAL ANALYSIS

POSSIBLE PRESSURE LOSSES IN COMPLETE SYSTEM

After a well is drilled and  completed, itrequires a great effort to transport or flow fluid through the reservoir until the piping system and ultimately flow into a separator for gas-liquid separation which are placed on the surface. the movement of these fluids requires energy to overcome friction losses and to lift the products. The pressure drop in the total system at any time will be the initial fluid pressure minus the final fluid pressure. This pressure drop is the sum of the pressure drops occurring in all of the components of the system. The selection and sizing of the individual component varies with producing rate.

The final desing of a production system cannot be separated into reservoir performance and piping system performance and handle independently. The amount of oil and gas flowing into well from the reservoir relies more on the pressure drop in the piping system, and the pressure of the piping system depends on the amount of fluid flowing through it. Therefore; the entire production system must be analyzed as a unit.

 SYSTEMS ANALYSIS APPROACH

The systems analysis approach, often called NODAL ANALYSIS has been applied for many years to analyse the performance of systems composed of interacting components (Electrical circuits, complex pipeline networks and centrifugal pumping systems are all analyzed using this method. The procedure consists of selecting a division point or node in the well and dividing the system at this point. All components upstream of the now comprise the inflow section, whereas the outflow section consists of all the components downstream of the node. A relationship among flow rate and pressure drop must be available for each component in the system. The flow rate through the system can be determined once the following requirements are satisfied:

  • Flow into the node equals flow out of the node,
  • Only one pressure can exist at a node.

The average pressure of the reservoir (Pavg) and the pressure of the system outlet called separator pressure ( Psep) are not functions of flow rate. Nevertheless, if the Psep is under control by a choke, it could be the Wellhead pressure (Pwh).

Once the node is selected, the node pressure is calculated from both directions starting at the fixed pressures.

Inflow to the node:

Pr – AP ( Upstream componets) = Pnode.

Ouflow from the node:

Psep + AP ( downstream components) = P node.

The pressure drop, AP, in any component varies with flow rate, Q. For that reason, a plot of node pressure versus flow rate will produce two curves, the intersection of which will give the conditions satisfying requirements (Flow into the node equals flow out of the node, and Only one pressure can exist at a node). That is illustrated as follows:

DETERMINATION OF FLOW CAPACITY

The effect of a change in any of the components can be analyzed by recalculating the node pressure versus flow rate using the features of the component that was changed. If a change was made in an upstream component, the outflow curve will remain unchanged.

SIMPLE PRODUCTION SYSTTEM

Nevertheless, if either curve is changed, the intersection will be shifted, and a new flow capacity and node pressure will exist. The curve will also be shifted if either of the fixed prcssures is changed. which may occur with depletion or a change in separatioll conditions.

The effect on the flow capacity of changing the tubing size is shown as follows , and so does the effect of a change in flowline size.

EFFECT OF TUBING SIZE

The effect of increasing the tubing size, as long as the tubing is not too large, is to give a higher node or well-head pressure for a given flow rate, because the pressure drop in the tubing will be decreased. This shifts the inflow curve upward and the intersection to the right. A large flowline will reduce the pressure drop in the flowline, shifting the outflow down and the intersection to the right. The effect of a change in any component in the system can be isolated in this manner. Also, the effect of declaning reservoir pressure or changing separator pressure can be determined.

EFFECT OF FLOWLINE SIZE

A more frequently used analysis procedure is to select the node between the reservoir and the piping system. This node does divide   the well into a reservoir system component and a piping system component.

The effect of a change in tubing size on the total system producing capacity when Pwf is the node pressure is illustrated above. An increased in production rate achieved by increasing tubing size is illustrated às well. however, if tubing is too large, the velocity of the fluid moving up the tubing may be too low effectively lift the liquids to the surface. This could be caused by either large tubing or low production rates.

WELL RESTRICTED BY PIPING SYSTEM

A producing system may be optimized by selecting the combination of component characteristics that will give the maximum production rate for the lowest cost. Although the overall pressure drop available for a system, Psep, might be fixed at a particular time, the producing capacity of the system  relies more on where the pressure drop happens. If too much pressure drop occurs in one particular component or module, there may be insufficient pressure drop remaining for efficient performance of the other modules. Even though the reservoir may be capable of producing a large amount of fluid. If too much pressure drop occurs in the tubing , the well performance suffers.

For this type of well completion, it is obvious that improving the reservoir performance by stimulation would be a waste of effort unless larger tubing were installed.

A case in which the well performance is controlled by the inflow is shown. In this case, the exessive pressure drop could be caused by formation damage or inadequate perforations. It is obvious from the plot that improving the performance of the piping system or outflow or placing the well on artificial lift would be fruitless unless the inflow performance were also improved.

PRIMARY CEMENTING AND SQUEEZE CEMENTING




Oil well cementing is the proccess of mixing and displacing a cement slurry down the casing and up the annular space behind the pipe where it is allowed to set, thus bonding the pipe to the formation. No other operation in drilling or completion is as important in the producing life of the well as a successful primary cementing job.

PRIMARY CEMENTING

The first verified use of portland cement in an oil well, to shut off water that could not be held with a casing shoe, was in 1903. After placing the cement, the operator normally waited 28 days before drilling the cement and testing. Improvements in cements, understanding WOC times, and the use of admixes have reduced WOC time to a few hours under present-day practices.

Cementing procedures are clasified in to primary and secondary phases. Primary cementing is performed immediately after the casing is run into the hole. Its objective is to get effective zonal separation and to help protect the pipe itself. Cementing also helps to

  • Bond the Pipe to the formation.
  • Protect producing sttrata.
  • Minimize the danger of blowouts from high-pressure zones.
  • Seal off lost-circulation zones or other troublesome formations as a prelude to deeeper drilling.

Secondary Cementing, or squeeze cementing, is the process of forcing a cement slurry into holes in ther casing and cavities behind the casing. These operations are usually performed for repairing or altering a completed well at some later date, or they may be used during the initial drilling process. Squezze cementing is necessary for many reasons, but probably the most important one is to segregate hydrocarbon producing zones from those formations producing other fluids. The goal on a squeeze cementing job is to place the cement at the desired point or points necessary to accomplish the purpose.

  • Squezze cementing is also employed to:
  • Supplement or repair a faulty primary cementing job.CHANNEL BEHIND THE CASING AFTER PRIMARY CEMENTING
  • Reduce the gas-oil, water-oil, water-gas ratio.
  • Repair defective casing or improperly placed perforations.
  • Minimize the danger of lost circulation in an open hole while drilling deeper.
  • Abandon  permanently a nonproductive or depleted zone.
  • Isolate a zone prior to perforating for production or prior to fracturing.

ABANDONING A DEPLETED OIL OR GAS ZONE

COMBUSTIBLE DE AVIACION

 Uno de los mas usados en los combustibles de aviacion es la gasolina de aviación grado 100, conocida como  ”Avigas”, es un combustible de alto índice antidetonante (alto octanaje), producida a partir de gases de refinería (butilenos e isobutanos) que se hacen reaccionar con un catalAIRPLANEizador (ácido sulfúrico) en un proceso denominado alquilación para obtener un componente denominado “alquilato”. Al alquilato se le adicionan compuestos aromáticos (tienen mayor octanaje) de tal manera que se alcance un octanaje motor (MON) de 100 como mínimo. Para conseguir la capacidad antidetonante de 130 se le adiciona tetraetilo de plomo; por esta razón este producto también se denomina gasolina de aviación 100-130.

El número 100 significa la capacidad antidetonante requerida por los motores de los aviones una vez alcanzada la velocidad de crucero y el número 130 identifica la capacidad antidetonante requerida para el despegue que es cuando los motores desarrollan la máxima potencia.

Usos:


Esta gasolina se encuentra diseñada para utilizarse en aviones con motor de pistón. No es recomendable usar esta gasolina en motores de automóviles porque contiene plomo, el cual daña los convertidores catalíticos, además del impacto ambiental que generan estas emisiones.

Los aviones propulsados por  turbina (turborreactor, turbopropulsor o turbohélice) utilizan queroseno, de propiedades similares a la gasolina, obtenido también en el proceso de refino del petróleo. Con independencia de su graduación, es incoloro o amarillo pálido. Este combustible, específico para motores de turbina, no puede emplearse de ninguna manera en motores de pistón.

Precauciones para el manejo 

El AVIGAS se clasifica como un líquido inflamable clase 1A de acuerdo con la Norma 321 de la NFPA, por lo cual debe tenerse especial cuidado y es indispensable cumplir con los estándares establecidos para el diseño de los tanques de almacenamiento, tuberías, llenaderos y equipo de las estaciones de servicio al público.

Este producto es volátil, genera vapores desde una temperatura de -43°C, SUPPLYlos cuales al mezclarse con aire en proporciones de 1.1 a 7.6% en volumen producen mezclas inflamables y explosivas. Cuando se diseñen plantas de almacenamiento, estaciones de servicio, o cualquier otra instalación para el manejo de esta gasolina, deben aplicarse las normas NFPA en para lo relacionado con la protección contra incendios, las Normas API y las reglamentaciones expedidas por las autoridades gubernamentales de control tanto nacional como regional y local.

No es recomendable dar a este producto usos diferentes del mencionado antes debido a que los vapores que genera son más pesados que el aire, por lo tanto tienden a depositarse en lugares bajos donde están localizadas normalmente las fuentes de ignición tales como pilotos de estufas, interruptores de corriente eléctrica, tomas de corriente y puntos calientes tales como lámparas incandescentes, los cuales pueden producir incendios y explosiones.

Debe evitarse la inhalación de vapores debido a que estos son tóxicos y en concentraciones altas pueden causar mareos, pérdida del conocimiento y, en casos extremos, hasta la muerte.

Nunca se debe almacenar gasolina de aviación en una casa, apartamento o en cualquier recinto cerrado. El combustible se evapora continuamente y, además de generar una atmósfera de vapores tóxicos, puede causar un incendio o una explosión. Para un manejo seguro debe utilizarse ropa impermeable adecuada, gafas y guantes de seguridad. 

En el Peru la comercializacion de Combustible de Aviacion es bien restringido asi como tambien esta prohibido por el uso del kerosene ya que el combustible de aviacion es un kerosene ya tratado cumpliendo ciertas especificaciones internacionales.

Los consumidores de este tipo de combustible deben estar debidamente acreditados y certificado por la Direccion General de hidrocarburos ( DGH). Las ventas que se realiza son nacionales o exportaciones.

UBICACION DEL COMBUSTIBLE EN EL AVION

SEISMIC 4D FOUR-DIMENSIONAL

Three-dimensional seismic data represent static reservoir properties, because the data are collected during one instant in time. Four-dimensional, or “timelapse” seismic data, offer the opportunity to monitor the movement of reservoir fluids while they are being produced. Thus, 4D seismic measures dynamic reservoir properties. The underlying principle of 4D seismic is that acoustic properties of reservoir strata will change as a function of change in fluid content and type within the rock’s pore spaces. Thus, 3D seismic surveys that are shot in the same (or similar) manner, at the same location, and at successive times during the life of a field, record rock-fluid changes that result from fluid movement.