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Colin Vande Vijvere SLCEVO40

A PERSONAL SUPERLITE BUILD

SLCEVO40

Built around
the obsession.

POWERTRAIN

01 / POWERPLANT

The heart.
Uncovered.

Supercharged V8 power.
Engineered as a complete system.

Gen V LT4 dry-sump crate engine

Factory power
650 hp
Factory torque
650 lb-ft
Displacement
6.2 liters
Supercharger
1.7 liters
Engine weight Dry-sump LT4
~330 lb
Transmission weight Graziano six-speed manual
120–140 lb

Factory LT4 ratings; this build's measured output is not documented here. Chevrolet specifications

Loading engine model…
CONTROLLED TURNTABLE · 360° Original illustrative geometry. Reference accessories may differ from the build.

BEYOND THE ENGINE

Oil. Cooling.
Control.

Dry-sump lubrication
An AVIAID dry-sump tank complements the LT4's dry-sump configuration.
Thermal management
Dual Mishimoto intercoolers are part of the build's cooling system.
Engine management
The stock GM ECU, with HP Tuners for calibration and diagnostics.

02 / DRIVETRAIN

Every shift.
A connection.

A six-speed Graziano manual transaxle as seen in the Audi R8 and Lamborghini Gallardo.
Modified with an HCF drop gear to match the LT4’s characteristics.

SIX-SPEED / MANUAL PAIRED GEARS / SCHEMATIC 1 2 3 4 5 6 GRAZIANO + DROP GEAR
CONSTANT-MESH MOTION STUDY Illustrative geartrain, not the exact Graziano internals. One ratio engaged; the remaining output gears freewheel.
TRANSAXLEGraziano 6-speed
FLYWHEELHCF
CLUTCHTilton twin-disc

THE CONNECTION

Gearing with
a purpose.

The HCF drop gear adapts the Graziano to the lower-revving LT4. An HCF flywheel and Tilton twin-disc clutch complete the connection between engine and transaxle.

THE NEXT CHAPTER

A whole car.
A thousand decisions.

Suspension. Electronics. A planned active wing.
Return to the car to explore each system as the build takes shape.

Inside the workshop
About these visual studies

The workshop photograph shows Colin's actual car. The rotating engine and gearstack are original illustrations, not dimensioned CAD or a record of completed installations.

The LT4 photo reference shows a modified engine. Its output figures, internal modifications, and oil-pan configuration are not claims about this build. The Graziano reference depicts the OGeco hybrid concept, a different transmission. No reference photography is embedded in these illustrations.

02 / ELECTRONICS

Power. Data.
Driver.

A clear driver interface, managed electrical loads, and factory engine control. The next layer is a custom controller for active aero.

Explore the electronics

SUPPLIED D6 HARDWARE REFERENCE

The information
that matters.

An AiM 6-inch PDM display puts vehicle data and warnings in the driver's sightline. The supplied D6 CAD gives the dashboard packaging a real hardware envelope.

Role
Driver display & warnings
Reference
AiM PDM Dash 6-inch / D6
AiM technical reference
D6 / DISPLAYSUPPLIED CAD
Three-quarter render of the supplied AiM D6 display CAD, with its dark bezel, blank blue screen, buttons, and indicator strip.
Rendered from the supplied D6 geometry. The blue screen is the CAD material, not live telemetry.

PDM / EXACT MODEL TO CONFIRM

Distribute.
Protect. Diagnose.

Power distribution brings electrical loads, circuit protection, and fault feedback into a managed system. Output assignments and protection settings follow the actual module and loom design.

Role
Power switching & protection
Build record
Hardware model and circuit setup to document
POWER DISTRIBUTIONILLUSTRATIVE
Power distribution module, illustrative enclosure study An abstract black module with protected power paths. Its shape and connectors do not identify the installed PDM. PDM POWER / PROTECTION MANAGED POWER FAULT FEEDBACK SWITCH / PROTECT / DIAGNOSE
Original enclosure and functional study. Connector shapes and output count do not specify the build hardware.

CONFIRMED BUILD EQUIPMENT

Factory control.
Build-specific calibration.

The stock GM ECU anchors LT4 engine management. HP Tuners provides the calibration, scanning, and data-logging workflow for understanding and refining its operation.

Engine management
Stock GM ECU
Calibration & diagnostics
HP Tuners
HP Tuners GM reference
GM / LT4 ENGINE CONTROLILLUSTRATIVE
Illustrative GM engine control module An original silver finned controller illustration with three dark connector housings. The exact GM controller part number and enclosure are unconfirmed. GM ECU LT4 ENGINE CONTROL CALIBRATION / SCANNING / LOGGING
Original controller illustration. The exact GM ECU part number and enclosure are unconfirmed.

PLANNED / CUSTOM CONTROLLER

A separate
control problem.

The active wing needs its own sensing, actuation, and fail-state decisions. Custom aero control is planned; the operating strategy and physical integration remain engineering work to complete.

Scope
Active-aero control & DRS
Next decisions
Actuation, limits & failure behaviour
ACTIVE AERO / CONTROL STUDYPLANNED
Planned active-aero control concept A wing and an abstract controller linked by dashed functional paths. State sensing, actuation, travel limits, and failure behaviour remain to be designed. CUSTOM CONTROL PLANNED STATE / SENSING LIMITS / ACTUATION STRATEGY / LIMITS / FAIL STATE
Functional concept, not an installed wiring diagram or validated control law.

BUILD IN PROGRESS GM ECU and HP Tuners are confirmed. AiM display geometry is supplied; installation and final display setup are still to document. PDM identification is pending. Custom active-aero control is planned.

03 / SUSPENSION

DESIGN IN PROGRESS

Geometry first.
Adjustment second.

The rear cantilever needs a rethink. Then comes the tuning: QA1 MOD dampers, Hyperco springs, and front and rear sway bars designed around this chassis.

Technical illustration of a coilover with attached piggyback canister and two external QuickTune-style valve packs. Exact part dimensions are unconfirmed.
01 COILOVER CAD 02 ATTACHED CANISTER 03 QUICKTUNE PACKS
Illustrative technical component study. Attached canister and valve-pack details are a reference-based visual study.

01 / REAR CANTILEVER

Get the leverage right.

The rocker translates wheel movement into damper movement. Reworking its pivots and pickup points lets us shape motion ratio and progression, use the available damper stroke, and keep clearance through bump and droop.

Motion ratio = shock movement ÷ wheel movement.

Hardpoints, ratios and travel margins still need to be established on the car.

KINEMATIC STUDYSCHEMATIC / NOT TO SCALE
Wheel, pushrod, rocker and damper linkage Move the travel control to raise the wheel. A fixed-length pushrod rotates the rocker around its fixed pivot and moves the damper. These are illustrative hardpoints, not measured SLC geometry. 1 2 3
1 Wheel + pushrod2 Rocker pivot3 Damper stroke
Illustrative linkage only. The control demonstrates the relationship, without a measured ratio or travel claim.

02 / QA1 MOD SERIES

Room to tune.

Independent high- and low-speed compression and rebound adjustments give the MOD series four ways to shape damping. “Speed” means shock shaft speed, not road speed.

The piggyback nitrogen canister attaches directly to the shock base. QuickTune’s external compression and rebound valve packs can be swapped on the car. This study adds those visible features to the supplied coilover CAD; final dimensions and full-travel clearance remain design tasks.

COMPRESSIONREBOUND
LOW SHAFT SPEED
Body control
Extension control
HIGH SHAFT SPEED
Sharp inputs
Fast extension

Adjustment functions overlap. Final valving and settings need testing.

03 / FRONT + REAR SWAY BARS

Build the balance.

Designing both bars from scratch gives us control of packaging, lever arms and front-to-rear roll stiffness. The aim: tune roll resistance and handling balance without relying only on stiffer road springs.

Bar section, arm length, links and mounts will be developed together. Loads, clearance, fatigue and vehicle testing still need to validate the design.

ANTI-ROLL PRINCIPLEONE AXLE / SCHEMATIC
Sway bar response to wheel movement Opposite wheel movements twist the bar. Equal movements rotate the arms together with much less torsional resistance in an ideal symmetric system. 1 2 3
1 Chassis mounts2 Torsion section3 Arms + end links
Opposite wheel movement twists the bar, adding roll resistance. Front and rear bar choices set the balance together.

04 / ACTIVE AERO · PLANNED

One wing.
Two intentions.

Rear element raised.

The rear element sits at its higher illustrative angle. Select DRS to flatten its orientation.

Illustrative dual-element wing side section with a fixed main plane and a pivoting rear element FIXED MAIN PLANE REAR ELEMENT PIVOT STUDY DOWNFORCE POSITION

WING ONLY / ILLUSTRATIVE ESTIMATE

Speed. Squared.

Illustrative, unvalidated wing-only model. GT3 RS coefficients have not been verified; both coefficients below are arbitrary assumptions.

F↓ = ½ ρ v² S C↓

Downforce position

Assumed C↓ = 1.00

— lbf ↓

— N

F↓ = 0.5 × ρ × v² × S × C↓

DRS position

Assumed C↓ = 0.30

— lbf ↓

— N

F↓ = 0.5 × ρ × v² × S × C↓

JavaScript enables the speed control, editable assumptions and estimates. The force equation remains available as an educational model.

Assumptions, area & sources

ASSUMED OVERALL SPAN70 in / 1.778 m

SHARED REFERENCE AREA S0.5334 m²

Example area only until the local CAD footprint is available.

The 210 mph slider limit is a chosen illustration range, not a measured top speed. A separate, provisional gearing estimate is about 205.7 mph at 6,600 rpm with 325/25ZR20 rear tires, 0.70 sixth gear, an assumed 1.04 drop gear and 3.462 final drive. Tire rolling diameter and gearing assumptions are not verified as an operating speed.

Positive force means downforce. The same reference area is used for both positions; their assumed coefficients create the difference. Car speed assumes still air.

The 1.00 / 0.30 coefficients are arbitrary examples, not verified GT3 RS values or CFD / wind-tunnel results. This estimates wing-only vertical force, not whole-car aero, drag reduction or setup guidance. Real coefficients vary with angle and flow conditions. Porsche's published total-car downforce does not establish coefficients for this wing or these poses.

Conversions: v (m/s) = speed (mph) × 0.44704; 1 lbf = 4.448221615 N. Model: NASA lift equation, using a positive-downward coefficient convention.

The wing and custom control modules are planned. Integration, actuation, control logic, and validation remain future work.