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Degradation model

Let 0 denote the vector of component parameters i. 0, let y(f) be the vector of known measured outputs of the real system, (f) the vector of inputs into the system and into the nominal model of the system and wi (f) the vector of all switch states, i.e. m t) denotes the system mode. Assume that fault diagnosis has detected and isolated 1 as a single incipient fault starting at time instant to. Then [Pg.223]

9 Failure Prognosis for Hybrid Systems Based on ARR Residuals [Pg.224]

For instance, suppose that the degradation trend i (t) can be approximated by the simple nonlinear ODE [Pg.224]

With this solution replacing the nominal parameter 0i in (9.1) residual r (f) vanishes. [Pg.224]

In case multiple potential component faults may be the cause for the start of an abnormal behaviour of an ARR residual, then parameter estimation as part of fault isolation identifies the parameters that are going to deviate from their nominal values. For each of them, failure prognosis wUl have to identify a degradation model as a first step. This identification of degradation models can be performed in parallel. As a result, multiple faults may have different degradation profiles. [Pg.224]


Another problem occurs when some fire retardant formulations ate exposed to elevated temperatures (eg, when used as roof tmsses or as roof sheathing) thermal-induced strength reductions can occur in-service. The thermo-chemical factors were discussed by LeVan and Winandy (26), and a kinetic degrade model was developed (27). The treater should be consulted to obtain appropriate in-service modifications for specific fire retardant treatments. [Pg.327]

Implementation of advanced performance degradation models, necessitate the inclusion of advanced instrumentation and sensors such as pyrometers for monitoring hot section components, dynamic pressure transducers for detection of surge and other flow instabilities such as combustion especially in the new dry low NO combustors. To fully round out a condition monitoring system the use of expert systems in determining fault and life cycle of various components is a necessity. [Pg.647]

First-order kinetics is easier to apply to transport and degradation models because they do not require knowledge about particle geometry. [Pg.214]

EXAMPLE 6.10 Air-Stripping tower with first-order degradation, modeled as plugfiow, plug flow with dispersion, and mixed tanks-in-series reactors... [Pg.151]

Table 8.5. Examples of kinetic parameters for chlorophenol degradation modeled by Monod or Haldane (Kl involved) equations... [Pg.268]

Figure 1 Solid-state degradation models, a—fraction decomposed. A = Prout-Tompkins, kt = ln(-p ), B = 2 dimensional phase boundary kl = l-(l-a)1 2, C=Avrami-Erofeev, kt — [—ln(l — a)] , w=l, D = Avrami-Erofeev, = 0.5. Figure 1 Solid-state degradation models, a—fraction decomposed. A = Prout-Tompkins, kt = ln(-p ), B = 2 dimensional phase boundary kl = l-(l-a)1 2, C=Avrami-Erofeev, kt — [—ln(l — a)] , w=l, D = Avrami-Erofeev, = 0.5.
Degradation model of South Blackwater coal on three impact surfaces... [Pg.259]

The value of parameters for the degradation model for both types of coal at 5 m drop heights... [Pg.259]

Fig. 17. Comparison of raw data mid model data of South Blackwater at 5 m drop height. (D Model data = Degradation Model data). Fig. 17. Comparison of raw data mid model data of South Blackwater at 5 m drop height. (D Model data = Degradation Model data).
The degradation model of three samples (cushioned coal, initial 10% fines and initial 30% fines) of South Blackwater coal is determined on three impact surfaces (steel plate, conveyor belt and coal stockpile). Degradation model equation can be written as follows ... [Pg.259]

Non-cushioned coal sample of both types of coal dropped on different impact surfaces produced higher percentage of fines than the sample of cushioned coal, initial 10% fines, initial 30% fines and initial 50% fines. The cushioning effects of South Blackwater and Ensham coal with initial 10% fines dropped on steel surface produced more fines than conveyor surface and coal surface. The cushioning effect of fines on coal surface was least compare to other two impact surfaces. There was no significant difference of fines generation in between the three impact surfaces tested with a sample of initial 30% fines of both types of coal. The degradation model was used satisfactorily for South Blackwater coal on different impact surfaces. [Pg.260]

R.K. Sahoo, D. Roach, Degradation model of the dropped coal on different impact surfaces, BSH 23 (6) (2003) 6. [Pg.262]

Figure 9.19 Variations in the concentration ((Jig g 1) of five cell-associated 13C-labeled compounds oxic (I open) and anoxic (II open, and VI closed) incubations. Straight lines and curves were fit to a first-order degradation model of concentration data. (Modified from Sun et al., 2002.)... Figure 9.19 Variations in the concentration ((Jig g 1) of five cell-associated 13C-labeled compounds oxic (I open) and anoxic (II open, and VI closed) incubations. Straight lines and curves were fit to a first-order degradation model of concentration data. (Modified from Sun et al., 2002.)...
Biopolymer degradation model states that newly released bioploymers from organic matter will eventually be broken down into more labile smaller molecules. [Pg.515]

Substrates. The fabric substrates consisted of a standard 80 X 80 count (nominal) 3.5 oz/yd2 cotton print cloth, machine washed in a 0.1% solution of Triton X-100 this fabric exposed to 50-, 100-, or 150-Mrad doses of high energy electrons as described in Part I of this series (2) or this fabric degraded by hydrolysis in 5N HC1 at room temperature for 5.5 h. These degraded model fabrics were selected because their properties were sufficiently similar to those of archeological samples and because they could be prepared readily in large quantities. [Pg.311]

Figure 10 Catalyst Deactivation in Color Degradation Model for Deep HDS of Diesel Fuel... Figure 10 Catalyst Deactivation in Color Degradation Model for Deep HDS of Diesel Fuel...
Figure 11 Effect of Catalyst Aging on Apparent Activation Energy of K3 in Color Degradation Model... Figure 11 Effect of Catalyst Aging on Apparent Activation Energy of K3 in Color Degradation Model...
A major aliquot of a peak fraction (90%) was subjected to automated Edman degradation (model 477, Applied Biosystems). Typically, fractions of ca. 60 pi were applied to a polybrene-coated glass fibre filter and sequenced. [Pg.48]

A. The radiation exposure states have been changed to reflect new performance degradation modeling. The new states will appear in Joint Pub 3-12.2 and become doctrine. [Pg.35]


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