Appearance
A manufacturer of automotive fuel injection components (AISI 4140, Ø8 mm × 400 mm gun-drilled bores, HSS-Co M42 gun drills averaging 120 bores per regrind) implemented deep cryogenic treatment (−196°C, 24-hour soak, 0.5°C/min cooling, 150°C temper). Results: retained austenite reduced from 18% to 2% (XRD); hardness increased from 67.5 to 69.0 HRC; carbide volume fraction increased from 8.5% to 11.2%. Tool life increased from 120 to 280 bores per regrind (133% improvement); tool changes per shift reduced from 2 to 1; tooling cost per bore reduced by 35%. Surface finish and bore tolerance were unchanged.
Cryogenic Treatment Principles and Parameters
Cryogenic Treatment Types and Process Parameters
| Treatment Type | Temperature Range (°C) | Cooling Rate (°C/min) | Soak Time (hours) | Ramp to Tempering Rate (°C/min) | Tempering Temperature (°C) | Tempering Time (hours) | Total Cycle Time (hours) | Typical Equipment | Relative Cost per Tool |
|---|---|---|---|---|---|---|---|---|---|
| Shallow cryogenic (cold treatment) | −80 to −40 | 1–5 | 2–8 | Natural warm-up (0.5–2°C/min) | 150–200 | 1–2 | 6–12 | Mechanical freezer (dry ice or cascade refrigeration) | 1.0× (baseline) |
| Deep cryogenic (standard) | −196 to −180 | 0.1–1.0 | 12–36 | 0.3–0.5 | 150–200 | 2–3 | 24–48 | Liquid nitrogen cryogenic chamber with programmable controller | 2.0× |
| Deep cryogenic (extended) | −196 | 0.05–0.5 | 36–72 | 0.1–0.3 | 150–200 | 3–4 | 48–96 | Liquid nitrogen cryogenic chamber with advanced ramp control | 3.0× |
| Cryogenic + multiple temper | −196 | 0.1–1.0 | 24 | 0.5 | 150 (first) + 540 (second) | 2 + 2 | 52 | Cryogenic chamber + conventional tempering furnace | 2.5× |
Microstructural Changes by Tool Material
| Tool Material | Untreated Microstructure | Cryogenic-Induced Change | Transformation Mechanism | Temperature Required | Optimal Soak Time | Hardness Change (HRC) | Wear Resistance Improvement | Dimensional Stability Improvement |
|---|---|---|---|---|---|---|---|---|
| HSS (M2, M7) | Tempered martensite + MC/M6C carbides + 8–15% retained austenite | Retained austenite → martensite transformation; fine eta carbide (M₆C, M₂₃C₆) precipitation | Martensitic transformation (athermal); carbide precipitation (diffusion-controlled during tempering) | Below Mf (martensite finish, typically −80°C) | 12–24 hours | +1.0 to +2.0 | 30–60% improvement | 20–40% improvement |
| HSS-Co (M35, M42) | Tempered martensite with Co-enriched matrix + 8–18% retained austenite | Retained austenite transformation + eta carbide + Co clustering | Same as HSS; cobalt enhances carbide nucleation | Below Mf (−100 to −120°C for Co HSS) | 24–36 hours | +0.5 to +1.5 | 50–130% improvement | 25–45% improvement |
| Carbide (WC-Co, K10–K30) | WC grains (0.5–5 µm) in Co binder (6–12% by weight) | Co binder transformation: FCC → HCP partial transformation; Co densification; secondary carbide (η-phase) precipitation at WC-Co interfaces | Co binder structural refinement; stress relief at WC-Co interfaces | −196°C | 12–24 hours | +0.5 to +1.0 (macrohardness) | 15–40% improvement | 30–50% improvement |
| Carbide (WC-Co, micrograin K05–K15) | WC grains (0.2–0.8 µm) in Co binder (6–10%) | Co binder transformation + grain boundary carbide precipitation | Same as above; finer grain structure enhances effect | −196°C | 24–36 hours | +0.3 to +0.8 | 20–50% improvement | 30–50% improvement |
| CBN (PCBN) | CBN grains (1–10 µm) in metal or ceramic binder | Minimal microstructural change; residual stress relief in binder | Stress relief only | −80 to −196°C | 6–12 hours | No significant change | 0–15% improvement (from stress relief) | 10–20% improvement |
| PCD (polycrystalline diamond) | Diamond grains in Co binder | Co binder contraction (different CTE from diamond) — potential microcracking risk | Thermal contraction mismatch | NOT recommended for PCD | N/A | N/A | Risk of microcracking | N/A — not recommended |
Tool Life Improvement by Deep Hole Drilling Tool Type
| Tool Type | Tool Material | Workpiece Material | Bore Geometry | Untreated Tool Life (m) | Cryogenically Treated Tool Life (m) | Improvement (%) | Dominant Wear Mode (untreated) | Dominant Wear Mode (treated) | Data Source |
|---|---|---|---|---|---|---|---|---|---|
| Single-lip gun drill (Ø8 mm) | HSS-Co M42 | AISI 4140 (28 HRC) | Ø8 × 400 mm | 95 (120 bores per regrind) | 224 (280 bores) | +133% | Flank wear VB > 0.3 mm | Flank wear (slower progression) | Case study (automotive fuel injection) |
| Single-lip gun drill (Ø12 mm) | Micrograin carbide K15 | AISI 4340 (32 HRC) | Ø12 × 600 mm | 180 | 252 | +40% | Flank wear + crater wear | Flank wear only | Production trial |
| Single-lip gun drill (Ø20 mm) | HSS M2 | SAE 1026 (180 HB) | Ø20 × 1,000 mm | 65 | 104 | +60% | Edge chipping + flank wear | Gradual flank wear | Production trial |
| BTA drill head (2-insert, Ø50 mm) | Carbide K20 | AISI 4140 (28 HRC) | Ø50 × 1,500 mm | 85 (per edge index) | 128 (per edge index) | +50% | Crater wear at chip breaker | Flank wear + crater wear (reduced) | Production trial |
| BTA drill head (3-insert, Ø80 mm) | Carbide K20 | SAE 1026 (180 HB) | Ø80 × 2,000 mm | 120 | 180 | +50% | Crater wear | Flank wear (slower) | Production trial |
| Gun drill (Ø6 mm) | HSS M35 | 316L stainless | Ø6 × 300 mm | 35 | 70 | +100% | Flank wear + built-up edge | Flank wear (BUE eliminated) | Production trial |
| Reamer (Ø25 mm) | Carbide K10 | AISI 4140 (28 HRC) | Ø25 × 500 mm | 200 | 300 | +50% | Edge rounding | Gradual edge wear | Production trial |
| BTA drill head (2-insert, Ø40 mm) | HSS-Co M35 | Inconel 718 (42 HRC) | Ø40 × 600 mm | 8 | 14 | +75% | Chipping + crater wear | Gradual wear | Research trial |
Implementation and Economic Analysis
Cryogenic Treatment Quality Control and Verification
| Quality Parameter | Measurement Method | Acceptance Criterion (HSS) | Acceptance Criterion (Carbide) | Test Frequency | Cost per Test | Interpretation |
|---|---|---|---|---|---|---|
| Retained austenite content | XRD (Cr-Kα, sin²ψ method) | < 5% (from initial 8–18%) | N/A (carbide has negligible austenite) | Sample basis (1 per batch) | $50–100 | Higher retained austenite → incomplete transformation → reduced benefit |
| Macrohardness | Rockwell C (HRC) | +0.5 to +2.0 HRC increase from baseline | +0.3 to +1.0 HRC increase from baseline | Sample basis (3 per batch) | $10–20 | Smaller increase → insufficient treatment or material already optimised |
| Microhardness traverse | Vickers (HV0.1–HV0.5) | Uniform hardness from surface to core (±20 HV) | Uniform hardness from surface to core | Sample basis (1 per batch) | $30–60 | Gradient indicates incomplete treatment penetration |
| Carbide volume fraction | Quantitative metallography (image analysis) | Increase of 2–5% by volume (eta carbide) | Secondary carbide precipitation at WC-Co interfaces | Sample basis (1 per batch) | $50–100 | No increase → insufficient cryogenic soak or tempering cycle |
| Magnetic permeability | Ferritescope or magnetic induction | > 95% ferromagnetic (martensite is ferromagnetic, austenite is not) | N/A | 100% (non-destructive) | $5–10 | Lower than 95% → excessive retained austenite |
| Dimensional change | Micrometer or CMM | ±0.002 mm per 100 mm length | ±0.001 mm per 100 mm length | Sample basis (5 per batch) | $10–20 | Excessive change → thermal shock (cooling too fast) |
| Tool life test | Production running (number of bores to tool failure) | > 30% improvement vs untreated baseline | > 15% improvement vs untreated baseline | New material qualification only | High (production time) | Primary validation — must be correlated with lab tests |
Economic Analysis of Cryogenic Treatment for Deep Hole Drilling Tools
| Tool Type | Tool Cost per Unit ($) | Cryogenic Treatment Cost ($) | Untreated Life (bores) | Treated Life (bores) | Regrind Cost ($) | Bores per Regrind (untreated) | Bores per Regrind (treated) | Total Bore Cost (untreated, per 1,000 bores) | Total Bore Cost (treated, per 1,000 bores) | Savings per 1,000 Bores ($) | Payback Period (bores) |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Gun drill (Ø8 mm, HSS M42) | 45 | 8 | 120 | 280 | 15 | 120 | 280 | 500 | 246 | 254 | 32 |
| Gun drill (Ø12 mm, carbide K15) | 85 | 12 | 180 | 252 | 25 | 180 | 252 | 611 | 476 | 135 | 89 |
| Gun drill (Ø20 mm, HSS M2) | 65 | 10 | 65 | 104 | 20 | 65 | 104 | 1,308 | 865 | 443 | 23 |
| BTA head (Ø50 mm, 2-insert carbide) | 180 | 25 | 85 (per edge) | 128 (per edge) | 35 | 85 | 128 | 2,529 | 1,773 | 756 | 33 |
| BTA head (Ø80 mm, 3-insert carbide) | 250 | 35 | 120 (per edge) | 180 (per edge) | 50 | 120 | 180 | 2,083 | 1,472 | 611 | 57 |
| Gun drill (Ø6 mm, HSS M35) | 35 | 7 | 35 | 70 | 12 | 35 | 70 | 1,343 | 729 | 614 | 11 |
| Reamer (Ø25 mm, carbide K10) | 120 | 18 | 200 | 300 | 30 | 200 | 300 | 750 | 550 | 200 | 90 |
| BTA head (Ø40 mm, HSS-Co M35, Inconel) | 220 | 30 | 8 | 14 | 55 | 8 | 14 | 34,750 | 22,143 | 12,607 | 2.4 |
FAQ
What is the difference between shallow and deep cryogenic treatment for deep hole drilling tools?
The difference between shallow and deep cryogenic treatment lies in the minimum temperature reached, the soaking time at that temperature, and the resulting microstructural changes. Shallow cryogenic treatment (also called cold treatment) typically operates at −80°C to −40°C, achieved using dry ice (solid CO₂, sublimation temperature −78.5°C) or cascade mechanical refrigeration. The primary effect is the transformation of retained austenite to martensite in HSS tools. At −80°C, the driving force for martensitic transformation is sufficient to convert 60–80% of the retained austenite, reducing the retained austenite content from 10–18% to 3–8%. The soak time is relatively short (2–8 hours) because the martensitic transformation is athermal (time-independent) — it occurs almost instantaneously once the temperature is below the Mf (martensite finish) temperature. Shallow treatment does NOT cause significant carbide precipitation because the diffusion-controlled eta carbide (M₆C, M₂₃C₆) formation requires temperatures near −196°C to create the high vacancy concentration and dislocation density that serve as nucleation sites during subsequent tempering. Deep cryogenic treatment (−196°C to −180°C, achieved using liquid nitrogen) provides two distinct microstructural benefits: (1) retained austenite transformation — at −196°C, virtually all retained austenite (95–99%) transforms to martensite, reducing retained austenite to < 2%. This is important for HSS tools because retained austenite is a soft phase that can undergo stress-induced transformation during cutting, causing dimensional instability and reducing wear resistance. (2) Eta carbide precipitation — the deep cryogenic soak (12–36 hours) creates a high density of lattice defects (vacancies, dislocations) in the martensitic matrix. During subsequent tempering (150–200°C), these defects serve as nucleation sites for the precipitation of fine eta carbides (M₆C, M₂₃C₆), typically 5–20 nm in diameter. These fine carbides increase the carbide volume fraction by 2–5% and provide secondary hardening that improves wear resistance by 30–130% depending on the HSS grade. The cooling rate is critical for deep cryogenic treatment: the recommended rate is 0.1–1.0°C/min for HSS and 0.5–1.5°C/min for carbide. Faster cooling causes thermal shock and can crack carbide tools (due to differential thermal contraction between WC grains and the Co binder) or cause distortion in HSS tools. Slower cooling increases the total cycle time without additional benefit. For carbide tools (WC-Co), cryogenic treatment does not cause austenite transformation (there is no retained austenite in cemented carbide). Instead, the benefit comes from: Co binder transformation (partial FCC → HCP transformation that strengthens the binder); Co binder densification (thermal contraction creates compressive stress in the binder, improving WC grain retention); and stress relief at WC-Co interfaces. The practical recommendation is: deep cryogenic treatment (−196°C, 24-hour soak) for all HSS deep hole drilling tools (provides both austenite transformation and carbide precipitation); shallow treatment (−80°C, 4–8 hours) only for carbide tools where the maximum benefit is needed without the risk of thermal shock; and deep cryogenic treatment (−196°C, 12–24 hours) for carbide tools where maximum wear resistance improvement is required.
How much tool life improvement can be expected from cryogenic treatment for different deep hole drilling tools?
Tool life improvement from cryogenic treatment varies significantly with tool material, workpiece material, and the dominant wear mode. Based on documented studies and production trials, the expected improvements by tool category are: (1) HSS-Co gun drills (M35, M42) — the largest improvements are seen in this category, typically 50–130% increase in tool life. The improvement is maximised when the dominant wear mode is flank wear (abrasion) or crater wear (diffusion). The mechanism is the combination of retained austenite transformation (increases hardness by 1.0–2.0 HRC) and eta carbide precipitation (increases wear resistance through fine carbide dispersion). The largest reported improvement in the case study was 133% for M42 gun drills in AISI 4140 steel. (2) Carbide gun drills and BTA inserts — typical improvements of 15–50% for carbide tools. The improvement is lower than HSS because the primary wear resistance of carbide comes from the WC grain structure rather than the binder phase. The cryogenic effect on carbide is limited to: Co binder strengthening (FCC → HCP transformation, estimated to improve binder hardness by 10–20%); Co binder densification (reduces binder extrusion during cutting); and thermal stress relief (reduces residual tensile stress in the binder). The improvement is highest (40–50%) in applications where the dominant wear mode is crater wear (diffusion-controlled) or edge chipping. The improvement is lowest (15–25%) where the dominant wear mode is abrasion of WC grains. (3) PCD and CBN tools — improvements are minimal (0–15%) for CBN and not recommended for PCD. CBN tools already have high hardness and wear resistance; the cryogenic effect is limited to stress relief of the metal or ceramic binder. PCD should NOT be cryogenically treated because the different thermal contraction coefficients of diamond and cobalt binder cause microcracking at the diamond-binder interface. (4) Regrindability — an important consideration for deep hole drilling tools is that cryogenic treatment is a one-time process applied to the tool before its first use. The treatment affects the entire tool volume, so reground tools retain the benefits: after regrinding, the tool life per regrind remains 30–130% higher than untreated tools. However, the first regrind may show slightly less improvement than the original (10–20% reduction) because the most highly stressed surface layer has been removed. Subsequent regrinds stabilise at 70–90% of the first-life improvement. The practical expectation for production implementation is: HSS gun drills — 2.0–2.5× tool life; carbide gun drills — 1.3–1.5× tool life; BTA carbide inserts — 1.3–1.5× tool life per edge; and reground tools — retain 70–90% of the first-life improvement.
How does cryogenic treatment of carbide tools differ from HSS tools?
Cryogenic treatment of carbide (WC-Co) tools differs fundamentally from HSS treatment because the material systems are entirely different — carbide is a ceramic-metal composite (cemented carbide) while HSS is a ferrous alloy. The key differences are: (1) Microstructural changes — in HSS, the primary effects are transformation of retained austenite to martensite (ferrous phase transformation) and precipitation of fine eta carbides during subsequent tempering. In carbide, there is no austenite to transform. The primary effects are: Co binder phase transformation (cobalt undergoes a partial FCC → HCP allotropic transformation at low temperatures; the HCP phase has higher strength and lower stacking fault energy, improving the binder's mechanical properties); Co binder densification (the thermal contraction of the binder creates hydrostatic compressive stress around WC grains, improving grain retention); and WC-Co interface modification (relief of residual tensile stress at the WC-Co interface reduces the tendency for WC grain pullout). (2) Optimal parameters — for HSS, the optimal deep cryogenic treatment is −196°C for 24–36 hours with slow cooling (0.1–1.0°C/min) followed by tempering at 150–200°C. For carbide, the optimal treatment is −196°C for 12–24 hours with slower cooling (0.5–1.5°C/min) followed by tempering at 150–200°C. The shorter soak time for carbide is because the Co binder transformation is relatively fast (diffusion distance in Co is short) and the benefit does not increase significantly beyond 24 hours. The cooling rate is more critical for carbide than HSS because carbide is more susceptible to thermal shock cracking from differential thermal contraction between WC (CTE = 5.5 × 10⁻⁶/K) and Co binder (CTE = 13.0 × 10⁻⁶/K). (3) Expected improvement — HSS tools typically see 30–130% tool life improvement, while carbide tools see 15–50%. The lower absolute improvement for carbide reflects the fact that carbide is already a highly wear-resistant material, and the cryogenic treatment enhances a system that is already near-optimal. (4) Risk of damage — carbide tools have a genuine risk of thermal shock cracking if the cooling rate is too fast or if the tool has internal defects (pores, microcracks). The risk is highest for tools with high cobalt content (> 12% Co) because the larger volume fraction of high-CTE binder creates higher internal stress during cooling. The risk is lower for fine-grain carbide (grain size < 1 µm) because the shorter WC-Co interface length distributes the stress more uniformly. (5) Practical implementation — carbide tools can be cryogenically treated either as finished tools (ready-to-use) or as pre-forms before final grinding. Treatment before final grinding is preferred because: any dimensional changes from the treatment are removed by the final grinding operation; the grinding operation benefits from the improved dimensional stability of the treated material; and the risk of thermal shock cracking is lower because the tool still has grinding stock. In practice, most carbide deep hole drilling tools (gun drills, BTA inserts) are treated as finished tools because they are precision-ground to tight tolerances and cannot be post-ground economically. The recommended procedure for finished carbide tools is: deep cryogenic treatment at −196°C with cooling rate < 1°C/min, 24-hour soak, warm-up at 0.3–0.5°C/min to room temperature, followed by tempering at 150°C for 2 hours. This procedure minimises the risk of thermal shock while providing the maximum microstructural benefit.
Is cryogenic treatment cost-effective for deep hole drilling tools?
Cryogenic treatment is highly cost-effective for deep hole drilling tools based on economic analysis of production applications. The key economic factors are: (1) Cost per tool — the cryogenic treatment cost per tool is relatively low: $5–15 for small gun drills (Ø6–12 mm), $15–35 for large gun drills and BTA heads (Ø20–80 mm), and $25–50 for complete BTA drill heads with multiple inserts. These costs represent 10–20% of the tool purchase price for HSS tools and 7–15% for carbide tools. (2) Tool life improvement — the documented improvements (50–133% for HSS, 15–50% for carbide) translate directly into reduced tooling cost per bore because the tool cost is amortised over more bores. The economic benefit is amplified for deep hole drilling because: tool change downtime ($50–200 per event for machine idle time) is reduced proportionally; regrinding frequency is reduced (saving regrind labour and transportation costs); and scrap from tool failure near end-of-life is reduced because the more gradual wear progression of treated tools provides more consistent bore quality. (3) Payback period — the payback period for cryogenic treatment of deep hole drilling tools is remarkably short: 2–90 bores depending on tool type and cost structure. For the M42 gun drill case study, the $8 treatment cost was recovered in 32 bores (less than one shift of production at typical cycle times). For the most extreme case (Inconel 718 BTA drilling, where tool cost per bore is very high), the payback period was 2.4 bores — the $30 treatment paid for itself within one production cycle. (4) Annual savings — for a typical production deep hole drilling operation with 5,000–50,000 bores per year, the annual savings from cryogenic treatment range from $500–$50,000 depending on tool type, production volume, and the percentage improvement. The case study automotive fuel injection application (50,000 bores/year, $254 savings per 1,000 bores) generated annual savings of approximately $12,700 from a one-time treatment investment of approximately $400 (50 gun drills at $8 each). (5) Non-economic benefits — reduced tool changes per shift (improved operator utilisation and reduced non-cutting time); more consistent bore quality (treated tools maintain edge sharpness longer, reducing the gradual drift in bore diameter and surface finish as the tool wears); and reduced inventory requirements (fewer tools in the tool crib because each tool lasts longer). The practical recommendation is: cryogenic treatment is cost-effective for any deep hole drilling operation where the annual production volume exceeds 500–1,000 bores per year. For lower volumes, the tooling cost savings may not justify the treatment overhead and logistics. The treatment is most cost-effective for HSS tools (higher percentage improvement) and for applications with high tooling cost per bore (small-diameter gun drills, difficult materials like stainless steel and superalloys).
What are the risks of cryogenic treatment for deep hole drilling tools?
The risks of cryogenic treatment for deep hole drilling tools fall into three categories: thermal shock damage, incomplete treatment, and material incompatibility. (1) Thermal shock cracking — this is the most serious risk, particularly for carbide tools. The mechanism is differential thermal contraction between the carbide phase (WC, CTE = 5.5 × 10⁻⁶/K) and the cobalt binder (CTE = 13.0 × 10⁻⁶/K). During rapid cooling, the binder contracts more than the carbide grains, creating tensile stress at the WC-Co interface. If the cooling rate exceeds approximately 2°C/min for carbide, the interfacial stress can exceed the binder's yield strength, causing microcrack formation at the WC-Co interface. In extreme cases, visible cracks propagate through the tool. The risk factors are: high cobalt content (> 12% Co); large WC grain size (> 5 µm); pre-existing internal defects (porosity, microcracks from grinding); and complex tool geometry with sharp internal corners (coolant holes, chip breaker grooves). The mitigation strategy is: controlled slow cooling (0.5–1.5°C/min); pre-treatment inspection (dye penetrant or ultrasonic) to identify tools with pre-existing defects; and post-treatment inspection (dye penetrant or eddy current) for all carbide tools. For HSS tools, thermal shock cracking is rare because the material has higher toughness and thermal conductivity than carbide, but distortion can occur if the tool has thin sections or asymmetrical geometry. (2) Incomplete treatment — this occurs when the cooling rate is too fast (causes less complete microstructural transformation) or the soak time is too short (insufficient time for carbide precipitation in HSS). The symptoms are: retained austenite > 5% (HSS tools); tool life improvement < 20% (significantly below the expected 30–130% for HSS); and no measurable hardness increase. The root causes are typically: insufficient soak time (equipment limitation or process parameter error); inadequate temperature (chamber does not reach −196°C throughout the load); or rapid cooling that skips the temperature range where the beneficial transformations occur. The mitigation is: process validation with thermocouple-instrumented tools (minimum 3 tools per batch) to verify that all tools reach and maintain the target temperature; and batch quality control (XRD for retained austenite, hardness testing, and production tool life testing for the first 3–5 batches). (3) Material incompatibility — PCD tools should NOT be cryogenically treated. The diamond phase has a very low CTE (1.0 × 10⁻⁶/K) while the cobalt binder has a high CTE (13.0 × 10⁻⁶/K). The thermal contraction mismatch during cryogenic cooling creates severe tensile stress at the diamond-cobalt interface, causing microcracking and delamination of the diamond layer. PCD tool life after cryogenic treatment is typically 30–50% of the untreated baseline due to this damage. CBN tools can be cryogenically treated with minimal risk because the CBN grains have a CTE (4.5 × 10⁻⁶/K) closer to the binder materials, but the improvement is minimal (0–15%). (4) Dimensional changes — HSS tools can experience dimensional changes of ±0.002 mm per 100 mm length from the retained austenite → martensite transformation (martensite has a slightly larger specific volume than austenite). This is typically within tolerance for deep hole drilling tools but should be measured for precision-ground tools. Carbide tools show minimal dimensional change (< 0.001 mm per 100 mm) from cryogenic treatment.
This article provides an overview of cryogenic treatment for deep hole drilling tools. Process parameters, expected benefits, and implementation details depend on the specific tool material, geometry, and application. The technical data presented here reflects published research and documented case studies as of 2026.