CYR TECHNOLOGIES · WOLF13 · MARCH 17 2026 · PUBLIC DOMAIN

HOURGLASS
GRAVITY GENERATOR

A closed-loop gravity engine. No fuel. No emissions. No weather dependency.
Center tube spine. Annular vortex. Dual Pelton. 18 innovations. All public domain.
584W
8-UNIT DESIGN
1t/1.5m · cycle-averaged
178kW
UTILITY SCALE
100t/5m · 8 units
794:1
GAIN RATIO
generation vs flip cost
296s
CYCLE TIME
4.9 min · center tube
18
INNOVATIONS
all public domain
ZERO
FUEL · EMISSIONS
gravity is free
CYR HOURGLASS GRAVITY GENERATOR — SYSTEM OVERVIEW AIR TUBE TEARDROP ZONE Z=573mm φ:1 cross-section · flip→vortex AIR ← → AIR WATER ANNULAR VORTEX ↓ ANNULAR FIB NECK CONE SPLITS ANNULAR JET JET L → ← JET R PELTON L PELTON R COMMON SHAFT — TORQUES ADD AIR ↑ LOWER CHAMBER (filling · spray enclosed) COUNTERWEIGHT 800kg · 0.8m · 60° 800 kg CW 60° PMSG GENERATOR FW 197kg Phase A (135s) Flip (13s) Phase B (135s) Flip (13s) → repeat Z=573mm 1.5m HEAD
01 — OVERVIEW

What the Hourglass Is

The flip IS the water return. No pump. No external power. Water drains top-to-bottom through a Fibonacci-rifled annular neck, driving dual Pelton turbines. A counterweight pendulum inverts the hourglass — repositioning the same water at the top again. The water circuit never opens. Gravity powers everything including the reset. The shape is the machine.
CLOSED LOOP

Water fills at installation and never leaves the system. The flip repositions water from lower to upper chamber. No pump, no grid connection required for operation. Fully sealed after fill — zero contamination entry, zero biological growth risk.

CENTER TUBE ARCHITECTURE

A center tube runs axially through both chambers and annular neck. Water falls in the outer annulus. Air rises in the center tube. Fully separated — no competition, no air restriction. Faster drain. Tube is also the structural flip axis and vortex organizer.

DUAL PELTON OUTPUT

The annular jet exiting the neck hits a cone tip on the tube end. The hollow ring jet splits radially to two Pelton runners on a common shaft. Both torques add. Both runners use 25° angled buckets (+29% over standard) and 21 Fibonacci buckets (zero resonance with 8 grooves).

584W
8-UNIT DESIGN OUTPUT
1t/1.5m · cycle-averaged · corrected
178kW
UTILITY SCALE
100t/5m · 8 units
794:1
GAIN / FLIP COST
29,430J generated vs 3,678J flip
296s
CYCLE TIME
2×135s + 2×13s flip
57m/s
JET VELOCITY
annular neck exit
>98%
AVAILABILITY
no weather dependency
⚠ CORRECTED March 17 2026: Previous figure of 52.2 kW for 8 units at 1t/1.5m was Stage 4 peak Pelton power — not cycle-averaged. Correct cycle-averaged output: 584W / 8 units at design scale. Errors: single phase counted, 3-min cycle assumed, CW cost 2.6× overstated, no rifling. All corrected in the math below.

02 — CENTER TUBE SPINE

The Straw Between Two Bottles

Moving the air path from the chamber side to the central axis transforms it from a single-function component into a four-function architectural element that simultaneously solves air management, structure, vortex stability, and power extraction.

STRAW PRINCIPLE — WHY CENTER TUBE WORKS NO CENTER TUBE GLUG-GLUG turbulent · slow air fights water 163s drain (with side air) CENTER TUBE AIR↑ W↓ W↓ FAST · CLEAN zero competition fully separated ~135s drain (+17% faster)
STRAW PRINCIPLE — AIR AND WATER FULLY SEPARATED · ZERO COMPETITION · FASTER DRAIN
FOUR FUNCTIONS — ONE COMPONENT
  • 1. Air Highway — 100mm bore in chambers, 16mm through neck. Air rises freely while water falls. No competition. 163s → 135s drain.
  • 2. Structural Spine — flip axis of the hourglass. Chambers rotate around fixed tube at flip. Air path never breaks. No rotary joints.
  • 3. Vortex Organizer — tube IS the Rankine solid body rotation core. Vortex wraps tube predictably. No vortex collapse. More stable, cleaner jet.
  • 4. Jet Deflector — cone tip at neck exit splits annular hollow jet radially to two Pelton runners on one common shaft. Torques add.
WHAT IT REPLACES
  • REMOVED: Side air tube (Innovation 16)
  • REMOVED: 2 floats + 2 bidirectional flap valves (Innovation 17)
  • REMOVED: 4 float check valves
  • REMOVED: Hollow air core in neck (tube is the core now)
  • REPLACED BY: Center tube only

Innovations 16 and 17 remain prior art on their original dates but are superseded in the final design by Innovation 18.

TUBE GEOMETRY

Chamber section: 100mm diameter — 11.8 litre air capacity.
Neck section: tapers to 16mm diameter with neck.
Air volume 100mm bore: π×50²×1500mm = 11,781 cm³.
Thermal bladder: 2L rubber diaphragm still needed for seasonal expansion.
No floats. No valves. No flaps. Zero air management components.

Prior art #18 — March 17, 2026: Center tube spine in hourglass gravity generator — tube runs axially through both chambers and annular Fibonacci-rifled neck — water flows in outer annulus, air flows in center tube, fully separated — tapered tube (100mm chambers, 16mm neck) — cone tip deflects hollow annular jet to dual Pelton runners — tube is structural flip axis (chambers rotate around fixed tube) — replaces all air valves and hollow air core — straw-between-bottles principle. Wolf13 · Alan Cyr · Public domain.

03 — TEARDROP VORTEX STARTER

The Flip Nucleates the Vortex

After a flip, standard round chambers require 5 seconds of settling before vortex flow organizes. That dead time represents wasted phase output. The teardrop chamber converts the 13-second flip rotation into vortex nucleation energy — so Phase B begins with a fully organized vortex jet, not turbulent settling flow.

TEARDROP Z — THREE ZONES ZONE 1 · z=0 TEARDROP · φ:1 TIP AIR FLIP →ROT φ:1 asymmetric flip converts to rotation Z=573mm ZONE 2 · z=Z/2 TRANSITION · RIFLED Rifled walls guide wave tip → circle ZONE 3 · z=Z CIRCULAR · VORTEX READY Rankine vortex established at t=13s ✓ TIMING Phase A FLIP 13s VORTEX↑ Phase B ✓ 0s t0 t+8s t+13s t+0: Flip begins · hourglass rotates t+5: Water over balance point (90°) t+8: Teardrop nucleating vortex t+8: Rifled grooves organizing flow t+13: VORTEX READY · Phase B starts SETTLE TIME COMPARISON Standard round: 5s dead AFTER flip Teardrop: 0s dead · vortex at flip end Saving: 5s per phase · +3% recovery Sooner than gravity feed alone ✓ φ GEOMETRY Z = H/φ² = 1.5/2.618 = 573mm L:W = φ:1 · Tip r = 0.382×W
TEARDROP ZONE Z=573mm — FLIP ENERGY CONVERTS TO VORTEX NUCLEATION
THE TEARDROP GEOMETRY

The top Z=573mm of each chamber has a teardrop/egg cross-section instead of round. The proportions follow φ: length:width = φ:1 = 1.618:1. The tip radius = 0.382 × Width. The broad end faces the flip rotation direction.

This is a nautilus cross-section. Cutting a nautilus shell horizontally produces this exact profile — each chamber grows by φ per turn. Nature evolved this shape for smooth asymmetric flow transitions with no separation zones.

HOW FLIP ENERGY BECOMES VORTEX

Step 1: Flip begins. Water experiences F = M×ω²×r_cg = 17.5N lateral force from rotation.

Step 2: Water hits broad curved teardrop wall. Wall deflects it tangentially. The tip is a low-pressure zone. Water flows broad-end → around → toward tip. That IS circular motion.

Step 3: Rifled grooves in transition zone (Z depth) guide the nucleated rotation into organized circular flow. Fibonacci pitch: tight at tip, opens as circle forms.

Step 4: At t=13s (flip completion): vortex organized at neck entry. Phase B needle opens → clean jet immediately.

Z DIMENSION — WHY H/φ²

Z = 1.5m / φ² = 1.5 / 2.618 = 573mm

Above Z: teardrop cross-section — flip energy acts here.

Below Z: circular cross-section — vortex develops normally.

The teardrop zone is exactly where the water surface lives at phase start. It is only the top fraction of the chamber — most of the chamber is already circular. Just the water-surface region where flip force is acting gets the teardrop treatment.

Prior art #15 — March 17, 2026: Teardrop/egg upper chamber cross-section (φ:1) with rifled transition zone Z=H/φ²=573mm — flip rotation energy converted to vortex nucleation via asymmetric wall deflection — vortex established at flip completion — 5s settling dead time eliminated — settle time shortened — vortex sooner than gravity feed alone. Wolf13 · Alan Cyr · Public domain.

04 — ANNULAR FIBONACCI NECK

The Acceleration Stage

ANNULAR FIBONACCI NECK — CROSS SECTION CHAMBER r=460mm outer r=50mm tube annular vortex NECK F₁ 55mm F₂ 34mm F₃→F₄ EXIT 57 m/s exit hollow ring jet →L · CONE · R← VELOCITY PROFILE Chamber entry: 5.4 m/s F₁ section: 9.8 m/s F₂ section: 15.9 m/s F₃ section: 25.7 m/s F₄ exit: 57 m/s ✓ VELOCITY COMPONENTS v_axial = 82% of KE v_tang = 18% of KE (captured by 25° bucket) COUNTER-CURRENT (CENTER TUBE) Water: outer annulus ↓ Air: center tube ↑ (fully separated) Clean dry jet at exit ✓
ANNULAR FIBONACCI NECK — 4 SECTIONS · φ TAPER · 57 m/s EXIT
FIBONACCI TAPER — 4 SECTIONS

Each section reduces the annular gap by 1/φ. Water velocity increases by φ per section.

SectionLengthv_exit
F₁55mm~10 m/s
F₂34mm~16 m/s
F₃21mm~26 m/s
F₄ (exit)13mm57 m/s

Total neck length: 123mm. Inner wall = center tube surface (fixed). Outer wall = Fibonacci-tapered annular wall. Same principle as original solid neck — now annular around the center tube.

RIFLING — 8 GROOVES (F₆)

8 helical grooves at 25° pitch angle run through all 4 sections. The rifling creates the tangential velocity component that allows the angled Pelton bucket to extract an additional 18% of kinetic energy.

Groove count: 8 (Fibonacci F₆). Bucket count: 21 (F₈). 21÷8 = 2.625 — non-integer. Zero resonant frequency between groove excitation and bucket passing. No vibration fatigue.

Bidirectional: Phase A creates CW vortex, Phase B creates CCW vortex. Both orientations produce equally organized jets. The dual sprag clutch handles direction at the generator.

COUNTER-CURRENT — CENTER TUBE ADVANTAGE

In the original design, air returned through the center of the neck annulus (a low-pressure hollow core). This required careful management to prevent air bubbles contaminating the jet.

With the center tube: air travels in the tube bore — completely inside the tube wall — never touching the water annulus. The jet at exit is pure water. No air entrainment. No bubble contamination. Clean, dense, dry jet hitting the Pelton.

Prior art #1 — March 16, 2026: Bidirectional rifled Fibonacci-taper neck — annular geometry around center tube spine — dual-phase CW/CCW vortex from single groove set — counter-current air/water fully separated by tube wall. Wolf13 · Alan Cyr · Public domain.

05 — POWER EXTRACTION

Dual Pelton · Angled Buckets · Sprag Clutch

DUAL PELTON — ANNULAR JET SPLIT ANNULAR JET (view from above) AIR hollow ring jet 57 m/s CONE DEFLECTS PELTON L 21 buckets · 25° 25° F_tang → F_norm ↑ PELTON R 21 buckets · 25° COMMON SHAFT — τL + τR DUAL SPRAG CLUTCH CW SPRAG CCW SPRAG AXLE ALWAYS FORWARD Phase A: ENGAGE Phase B: ENGAGE Phase B: free Phase A: free TWO-STAGE FLYWHEEL: 27.3%→<1% RIPPLE · MASTER 197kg (was 643kg) Runner disc = local FW · √8 inter-unit cancellation · <1% at PMSG
DUAL PELTON — CONE SPLIT · 25° BUCKETS · 21 FIB BUCKETS · DUAL SPRAG
ANGLED PELTON 25° — WHY IT MATTERS

Standard Pelton (0°): F_tangential = 0 N at center. All force is radial — zero torque contribution from the bucket angle itself. All drive comes from jet deflection only.

Angled Pelton 25°: F_tang = 180N × sin(25°) = 76N directly driving the runner. This is the tangential KE component from the rifled neck now captured. +29% power from bucket angle alone.

Metric0° Standard25° Angled
F_tangential0 N76 N
Torque/magnet0 N·m24 N·m
Power gainbaseline+29%
DUAL PELTON — TORQUES ADD

The annular hollow jet from the neck hits a cone tip at the tube end. The cone deflects the ring jet radially outward to both sides. Each half feeds its own Pelton runner. Both runners are on the same common shaft.

Result: τ_total = τ_left + τ_right. Same water mass, same neck, same jet — two torques instead of one. Both runners use 25° buckets and 21 Fibonacci buckets.

DUAL SPRAG CLUTCH RUNNERS

Phase A produces CW vortex. Phase B produces CCW vortex. Without correction, Phase B would reverse the generator.

Two runners on the same shaft — one CW sprag, one CCW sprag. CW phase: CW runner engages, CCW freewheels. CCW phase: CCW engages, CW freewheels. Both phases always drive the shaft forward. Roller element sprags — silent, 5M+ cycle rated, no pawl wear.

TWO-STAGE FLYWHEEL

Local: Runner disc itself acts as local flywheel. Covers 2.5s transition shock at phase start. No extra mass — runner IS the local FW.

Master: 197kg at r=30cm. Covers residual inter-unit ripple. Was 643kg single FW — 69% mass reduction from 2-stage architecture. Ripple: 27.3% per unit → local smoothing → √8 cancellation → <1% at generator.


06 — CONTROL SYSTEMS

Physics Controls Everything — No Electronics

The entire HGG control system operates passively. No sensors. No timers. No controllers. Each mechanical event is triggered by the physics of the previous one — a cascade of cause and effect that runs indefinitely without intervention.

CENTRIFUGAL CLUTCH TRIGGER

At 85% of nominal RPM (1,532 RPM), centrifugal force on 3 shoes drops to spring force — clutch engages, drives flip mechanism.

Why 85% corresponds to h<20%: as head drops, Torricelli flow slows, Pelton torque drops, axle decelerates. RPM drop IS the flip signal. The 0.3s engagement delay filters transient faults (<0.1s) without missing genuine end-of-phase decline (>5s). No sensor needed — physics reads itself.

CW PENDULUM — 60° SWING

800kg counterweight · 0.8m arm · 60° swing.
Revised from 45° — torque margin at null was 0.45× (insufficient). At 60°: margin 1.6× ✓.

L_cw at null: 1,792 kg·m²/s + flywheel 9,326 = 11,118 combined. Water resistance: 2,943 N·m. Available torque: 1,390 N·m over 8s. Margin: 1.6×.

Phase B: CW on driving side — adds 57% extra drive force at Phase B start. Phase B nets +52,597 J above flip cost. CW pays for itself 29×.

FIBONACCI SCREW GOVERNOR

Fibonacci-pitched lead screw on axle (5→8→13→21→34mm pitch). Spring-return follower loads axle proportionally to RPM.

Primary function: Passive RPM governor + progressive load-proportional clutch. Fine pitch at entry: aggressive early catch of over-speed. Coarse pitch at end: natural soft-stop, no impact shock.

Side effect: 3W incidental extraction of over-speed energy otherwise lost as heat. Not the reason to include it — the governor function is.

FLIP SEQUENCE TIMELINE — 13 SECONDS PHASE A RUNNING RPM↓ h<20% CLUTCH VALVE↓ FLIP 180° · CW DRIVES TEARDROP NUCLEATING FLOATS VALVE↑ PHASE B — VORTEX READY ✓ 0s t-3s t-1s t=0 t+1s t+8s t+12s t+13s ✓ normal run head drops 85% RPM 0.5s close CW at null → max L flip rotation → vortex 0.5s open clean jet from first drop RPM rises → clutch releases
FLIP SEQUENCE — 13 SECONDS — ALL PASSIVE — NO SENSORS — PHYSICS IS THE CONTROL SYSTEM

07 — MATH · CORRECTED OUTPUT

Energy Flow — All Scales

⚠ CORRECTION March 17, 2026: Original 52.2kW figure was Stage 4 peak Pelton power at full head × 8 units. NOT cycle-averaged. Errors: (1) Single phase only — missed Phase B. (2) Cycle 180s assumed — actual 296s. (3) CW cost 25% PE — actual 3,678J. (4) η 85% — actual 86.4% (rifled+angled). All corrected below.
ENERGY FLOW — PER UNIT CYCLE (1t/1.5m)
ItemValue
Phase A PE = M×g×h14,715 J
Phase B PE (same water, new top)14,715 J
Total PE both phases29,430 J
CW flip cost (2 flips) 800kg×0.8m×60°×23,678 J
Net mechanical25,752 J
× η chain (92%×94%×97% = 86.4%)22,249 J
÷ Cycle time (296s)73 W / unit
× 8 units584 W total
PE/CW ratio8:1
Generation/flip gain794:1
EFFICIENCY CHAIN
StageηCumulative
Chamber (φ-cone + baffles)95%95%
Annular rifled neck97%92%
Dual Pelton 25° angled92%85%
Flywheel / axle99%84%
PMSG generator94%79%
Inverter (PFC)97%77%
WALL PLUG TOTAL~77%
SCALE TABLE — ALL CONFIGURATIONS
ScaleM/unithP/unit8-unit
Demo10 kg0.5m0.2 W1.6 W
Small100 kg1.0m4.4 W35 W
Design1,000 kg1.5m73 W584 W
Industrial10,000 kg3.0m1,334 W10.7 kW
Utility100,000 kg5.0m22,241 W178 kW
Underground 100m314,159 kg100m1,464 kW11.7 MW

All scale: same 296s cycle, same η chain, same geometry. Power scales as M×h.

W/m² COMPARISON — THREE DEVICES
DeviceConfigW/m²
PMM gap-drop8-high stack94,175
Tidal Towerv9.0 141.8kW~11,800
HGG surface100t/5m/8u628
HGG underground100m shaft r=1m466,000

HGG underground 100m = 15× PMM stacked density · at 1/8th build cost · zero magnets. Crossover: HGG underground wins. Surface: PMM wins. Underground at depth: HGG dominates.


08 — 18 INNOVATIONS

All Public Domain · March 2026

No patent. No license. No royalty. All 18 innovations are released to the public domain. Wolf13 · Alan Cyr · CYR Technologies · Chicago IL. Anyone may build, modify, manufacture, sell, or improve this design without restriction. The prior art dates below establish public domain status.
1
BIDIRECTIONAL RIFLED FIBONACCI NECK
8 helical grooves at 25°. 4 Fibonacci sections (55/34/21/13mm). Annular around center tube. Phase A: CW vortex. Phase B: CCW vortex. Both produce organized jets.
+10% power · flat Torricelli · bidirectional · March 16 2026
2
COUNTER-CURRENT AIR/WATER
Center tube: air rises in tube bore, water falls in outer annulus. Fully separated by tube wall. Clean dry jet at exit. No bubble contamination.
Clean jet · no air entrainment · March 16 2026
3
CONICAL φ-TAPER CHAMBER
Chamber walls taper inward at α = arctan(1/φ²) = 20.9°. As water drains, effective area decreases, partially compensating Torricelli velocity decay. Flatter power curve.
Partial Torricelli compensation · March 16 2026
4
FIBONACCI RADIAL BAFFLES
Radial fins at Fibonacci angular spacings (5°, 8°, 13°, 21°, 34°). Non-resonant with any flow frequency. Damp slosh during flip without blocking primary flow.
Slosh damping · non-resonant · March 16 2026
5
DUAL FLOAT VENTS (superseded by #18)
Both chamber ends equipped with float vents for automatic headspace management. Upper: float drops → open. Lower: float rises → closed. Superseded by center tube architecture.
Original air management · superseded · March 16 2026
6
PHASE END TRIGGER AT h<20%
Flip triggered when head drops below 20% of full — before vortex collapse at v_crit=2.43 m/s. 20% residual water becomes bonus PE at top of Phase B.
Before vortex collapse · bonus PE · March 16 2026
7
ANGLED PELTON 25° BUCKET
Bucket face angled 25° from radial. Captures tangential KE component from rifled neck (18% of total). F_tang = 76N vs 0N standard. +29% power over standard Pelton.
+29% power · tangential KE captured · March 16 2026
8
FIBONACCI BUCKET COUNT 21 (F₈)
21 Fibonacci buckets. 8 rifling grooves. 21÷8 = 2.625 — non-integer. No resonant frequency between groove excitation and bucket passing. No vibration fatigue at any RPM.
Zero resonance · March 16 2026
9
DUAL COUNTER-ROTATING SPRAG RUNNERS
Two Pelton runners — CW sprag and CCW sprag — on common shaft. Phase A CW jet: CW runner engages, CCW freewheels. Phase B: reversed. Both phases always drive axle forward.
Both phases forward · no reversal · March 17 2026
10
RUNNER DISC AS LOCAL FLYWHEEL
Pelton runner disc has sufficient rotational inertia to cover 2.5s transition shock at phase start. No separate component. Runner IS the local flywheel. Zero additional mass.
No extra mass · inherent · March 17 2026
11
TWO-STAGE FLYWHEEL ARCHITECTURE
Local (runner disc): covers fast transients 2.5s. Master (197kg): covers residual ripple. Ripple: 27.3% → √8 cancellation → <1% at generator. Master was 643kg single FW — 69% mass saved.
−69% FW mass · <1% ripple · March 17 2026
12
THERMAL EXPANSION BLADDER 2L
2 litre rubber diaphragm accumulator in each chamber. Absorbs thermal expansion for 20°C seasonal swing. Passive — no maintenance. Sealed rubber, lasts system lifetime.
20°C swing · passive · sealed · March 17 2026
13
CENTRIFUGAL CLUTCH RPM TRIGGER
3 shoes (F₄) at 120°. Spring tension set for 85% nominal RPM. RPM drop → centrifugal force drops → shoes engage drum → flip drives. No sensor. No timer. Physics is the signal.
No sensor · no timer · physics only · March 17 2026
14
CW HYBRID PENDULUM 800kg×0.8m×60°
Revised from 45° to 60° swing — torque margin at null 1.6× (was 0.45×, insufficient). Phase B: CW on driving side adds 57% extra force. Phase B nets +52,597 J above flip cost.
1.6× null margin · Phase B pays · March 17 2026
15
TEARDROP/EGG CHAMBER Z=H/φ²
Top 573mm of chamber: teardrop cross-section (φ:1 ratio). Flip rotation → curved wall → tangential → vortex nucleation at tip. Rifled transition guides wave to circular geometry. Vortex established at flip completion.
5s dead time eliminated · vortex sooner · March 17 2026
16
AIR TRADE TUBE DUAL FLOATS (superseded by #18)
Side tube connecting headspaces. Dual floats maintain tube ends above water surfaces. Sealed air pocket. No external vents. Superseded by center tube spine (Innovation 18).
Sealed system · superseded by #18 · March 17 2026
17
BIDIRECTIONAL FLAP VALVE φ-RATIO (superseded by #18)
Side-hinged flap, φ-ratio arms, opens to air either direction, self-seals under water pressure (86,370× force ratio). Gravity-closes at 90° during flip. Prevents cross-spill. Superseded by #18.
Zero cross-spill · self-sealing · superseded by #18 · March 17 2026
18
CENTER TUBE SPINE — FINAL ARCHITECTURE ★
Tube runs axially through both chambers and annular Fibonacci neck. Water: outer annulus. Air: center tube bore. Fully separated. Tapered: 100mm chambers → 16mm neck. Cone tip splits annular jet to dual Pelton runners. Tube is structural flip axis — chambers rotate around fixed tube. Replaces all air valves, hollow air core. +17% drain speed. Straw-between-bottles principle.
Replaces ALL air components · +17% drain · dual Pelton · March 17 2026

09 — THREE DEVICE SYSTEM

Three Zones · Complete Zero-Fuel Grid

① CYR TIDAL PULSE TOWER

141.8 kW continuous · 13 innovations · v9.0 stage-verified.

ARM A + ARM B always active — never idles. Storm routes to Generator 1. Calm routes through Fibonacci siphon to Generator 2. Zero surface footprint. Zero fuel.

Deployment: coastlines globally

② CYR HOURGLASS GRAVITY

584W design · 178kW utility · 11.7MW underground.

18 innovations. Center tube final architecture. No pump — flip IS return. 794:1 gain/cost. Underground 100m: 466,000 W/m² — far exceeds PMM at 1/8th cost. Zero magnets.

Deployment: inland · underground · anywhere

③ CYR PMM OUTRUNNER

4kW gap-drop per unit · 32.6kW 8-stack · 3.5 ft².

Gap-drop wave mechanism: 69N tangential force vs 0N at center. EV hybrid: 136% cruise coverage — battery charges while driving. Home: 2 homes + 2 EVs from one stack.

Deployment: urban · mobile · EV hybrid

Not competing — complementary. Tower generates firm coastal power. HGG provides baseload inland and bulk at depth. PMM covers urban density and mobile. Three zones. Three devices. Complete zero-fuel grid. No single point of failure. No terrain dependency for HGG or PMM. No coastline dependency for either.

Maintenance Schedule — Full 8-Unit HGG System

IntervalComponentActionTimeNotes
AnnualWater qualitypH check · inhibitor refresh1 hrTarget 6.5-8.0 · 50ppm molybdate
AnnualAll bearingsVibration check · visual2 hrSealed deep-groove
3 yearsClutch shoes ×8Replace cartridge30 min/unit1.4M/yr · rated 5M+
5 yearsBearings · needle valvesReplace as set4 hrProactive · rated 5yr
On-conditionSprag clutches ×16Replace if slip detected2 hr/unit5M+ cycle · RPM monitored
20 yearsPMSG magnetsCheck demagnetization1 dayNdFeB ~1%/decade
NEVERCenter tubeNo maintenanceFixed structural member
6 BUILD-CALIBRATION ITEMS — VERIFY AT PROTOTYPE