Loading in 5 sec....

TTA – Thermal Transient AnemometerPowerPoint Presentation

TTA – Thermal Transient Anemometer

- 227 Views
- Uploaded on
- Presentation posted in: General

TTA – Thermal Transient Anemometer

Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author.While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server.

- - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - -

Anemos: Greek for wind

Anemometer: to measure the wind

Thermal Transient: A heated sensor will lose energy to the passing wind. The higher the speed, the faster the loss and the shorter the “time constant ()” of the temperature decrease.

Ergo: utilize as the anemometer’s output.

Developed for underhood cooling circuit diagnostic evaluations:

- velocity and temperature distributions averaged over segments of the in-line heat exchanger
Developed under the sponsorship of

DiamlerChrysler Challenge Fund (originally with Mr. Clem Mesa, continued with Mr. Michael Zabat)

Patent Pending – MSU

Commercialized by DFTI – Digital Flow Technologies, Inc.

Underhood cooling circuit

HVAC ducts – flow rate distributions and thermal energy loss upstream of the register

Obvious objectives: transfer the thermal energy from the liquid media to the passing wind.

Obvious statement of success:

Obvious Problem: it is not feasible to construct a measurement scheme to obtain the infinite number of data points to evaluate the exit integral – assuming Tinlet=Tamb such that

TTA Strategy: obtain approximations to the spatial integral for area segments whose sum is the complete area of interest.

Diagnostic strategy: make the segments small enough that problem areas (e.g., downwind from crash members) are apparent.

Control electronics

- A frame with 8 cells to fit a heat exchanger

- A frame with 16 cells to fit the subject heat exchanger

(The control electronics schematic is provided in the TTA portion of www.dift-us.com.

See the MST article.)

A representative frame, mounted for calibration in the TSFL 22 (6161cm2) wind tunnel.

A 20-cell frame:

Frame Perimeter

Tungsten Wires

Pitot Probe

Typical Tungsten wire diameter = 5-8mil (0.127 to 0.203 mm)

Sensor wires are robust a la wind loads, dust, etc. impact.

- Hairs and grit will change the heat transfer coefficients but these can be cleaned off.
- Plastic deformation will nullify the basic calibration.

1) Obtain Tamb from R(Tamb)=R(T0)[1+(TambT0)]

2) Introduce heating current (I) such that:

I2RsensorTsensor≲Tmax

- where Tmax≲oxidation temperature
3) Cease heating current

- utilize measurement current (ca 10ma) to record R(t) during the temperature “decay” to Tamb

For h ≈ constant, T(t) for heat transfer dominated by the forced convection term is exponential since

(4)

(5)

Rn = Rn(T0)[1+(TnT0)]

(6)

(7)

(8)

Fit R(t) data to:

Utilize calibration data to determine spatially averaged velocity for the cell as:

(Note, this form of the TTA transfer function is motivated by that for a constant temperature anemometer. It is supported by the observed agreement with experimental data.)

Can be influenced by the alloys in the Tungsten, by the annealing processes, by witchcraft.

Hence, a hot-box has been constructed to determine for each cell of a completed frame.

Symbols show R(T) for different cells.

( = [slope]-1)

Conflicting information from basic heat transfer sources.

Fabrication and use of a test facility to directly evaluate the effect of Tamb(test)≠Tamb(cal).

Ford Haus HeaterFord Haus: A sub-atmospheric flow facility that allows the operator and test chamber to be on the upwind side of the external prime mover.

View from entry door into the 2.6m x 1.83m “Haus”.

Insulation is visible through the clear plastic side wall of the plenum chamber.

Solid State Temp. Sensors.

Pitot probe with adjacent Therms. Couple for velocity measure-ments.

5 lengths of 0.005” (0.127 mm) tungsten wire

5.66 m/s

1.49 m/s

← Location of Sensor Wire →

Tamb’ = 22°CV = 1.5 – 6.5 m/s

Tamb’’ = 72°CV = 1.5 – 6.0 m/s

Tamb’’’ = 103°CV = 1.5 – 6.0 m/s

Evaluate

It is inferred that the jump discontinuity for the 22°C=Tamb values represents the transition to vortex shedding. Future measurements for 72°C and 103°C=Tamb cases will test the hypothesis with higher velocity values.

The “A” terms, which represent free convection and heat loss by conduction, have been divided by their respective (Thot-Tamb) values. The averae of the three ratios was 0.0062. The three “low Re” data sets were brought to a common ordinate-intercept as A=0.0062 ΔT(°C). The three calibrations could then be made to agree by scaling the B’ terms with respect to ΔT.

1.) Step change in heat transfer, not previously seen with the TTA, is present with larger diameter sensor wires.

2.) Installed (in a frame) evaluation of is required for accurate Tambient measurements.

3.) Elevated (cf velocity calibration) temperature effects for a test condition must be addressed. (This presentation is advanced cf the associated SAE paper (#05VTMS-103). Further work is in progress.)