FARRIS ENGINEERING 1850-0L Curtiss Wright

( Brand: Farris Engineering ), ( Manufacturer Part Number: 1850-0L )

Review FARRIS ENGINEERING Curtiss Wright 18500l Used

The **Farris Engineering 1850-0L Curtiss-Wright 18,500 CFM (Cubic Feet per Minute) Industrial Blower** is a robust, high-performance axial flow fan engineered for demanding commercial, industrial, and institutional ventilation applications. Part of Farris Engineering s reliable and durable line of air-moving equipment, this model is specifically designed to deliver consistent, high-volume airflow with exceptional efficiency, making it an ideal choice for large-scale HVAC systems, industrial exhaust, fume extraction, and environmental control projects. Built around Curtiss-Wright s proven axial fan technology, the 1850-0L leverages a robust, single-stage impeller assembly that ensures smooth, laminar airflow while minimizing energy consumption. The fan s large diameter housing and precision-balanced blades optimize aerodynamic performance, reducing noise levels and operational strain while maintaining peak airflow capacity of up to **18,500 CFM** at standard operating conditions. Constructed from heavy-duty materials, including galvanized steel or stainless steel components where specified, this blower is engineered to withstand harsh environments, including exposure to moisture, dust, and temperature fluctuations, ensuring long-term reliability in both clean and contaminated air applications.

The **1850-0L** features a **direct-drive or belt-driven configuration**, allowing for flexible integration into existing mechanical systems, while its compact yet sturdy design minimizes installation complexity in tight spaces. The fan s robust motor typically a **Curtiss-Wright NEMA Premium or TEFC (Totally Enclosed Fan-Cooled) model** is engineered for extended operational life, with thermal protection and overload safeguards to prevent premature failure. Optional accessories, such as **vibration isolators, sound attenuators, or custom ductwork adaptors**, further enhance its versatility, making it adaptable for everything from warehouse ventilation and data center cooling to industrial process exhaust and agricultural air management. With a focus on **energy efficiency**, the 1850-0L incorporates aerodynamic refinements and variable pitch blade options, allowing operators to fine-tune performance for specific load requirements while reducing operational costs. Whether deployed in a manufacturing facility, commercial kitchen, or large-scale HVAC system, this blower delivers **uncompromising airflow reliability**, making it a cornerstone of efficient air movement solutions for industries demanding precision, durability, and high-performance ventilation.

The **Farris Engineering 1850-0L** (powered by a **Curtiss-Wright 18500L** engine) is a large, high-performance piston aircraft engine designed for specialized applications, particularly in military and experimental aviation. Below is a detailed breakdown of its pros and cons, followed by a conclusion and recommendation.

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### **Pros of the Farris 1850-0L (Curtiss-Wright 18500L Engine)**

1. **Extreme Power Output**

- The 18500L is one of the most powerful piston engines ever built, producing around **3,000 horsepower** (depending on modifications and fuel type). This makes it suitable for high-performance, high-thrust applications such as experimental fighters, bombers, or specialized testbeds.

- Capable of propelling large, heavily armed, or high-speed aircraft that conventional engines cannot handle.

2. **High Reliability (When Properly Maintained)**

- Curtiss-Wright engines, particularly those from the WWII era, were built with robust construction and were widely used in military aircraft (e.g., P-47 Thunderbolt, P-61 Black Widow). The 18500L is a further evolution of these designs, incorporating lessons from high-performance piston engines.

- With proper maintenance, these engines can achieve **high time-on-station** (though not as long as modern turbocharged engines).

3. **Fuel Flexibility**

- **100/130 aviation gasoline** (traditional for piston engines)

- **Jet fuel (JP-4, JP-8)** useful for military or hybrid applications

- **Alcohol-based fuels** (e.g., methanol, ethanol) can significantly increase power output (though with trade-offs in reliability and cooling requirements)

- This flexibility makes it adaptable for experimental or dual-use applications.

4. **Proven Airframe Compatibility**

- The engine was designed for the **Farris 1850-0L**, a custom-built aircraft intended for high-speed, high-altitude flight. While not a production aircraft, its design leverages lessons from past high-performance piston projects.

- Can be adapted to other airframes with sufficient power requirements (e.g., modified bombers, interceptor prototypes).

5. **Historical and Niche Appeal**

- For collectors, enthusiasts, or military historians, owning such an engine represents a piece of aviation history, particularly given its ties to experimental and military aviation programs.

- Useful for **restoration projects** of rare or experimental aircraft (e.g., some Cold War-era prototypes).

6. **Potential for High-Speed Flight**

- Piston engines like the 18500L were used in some of the fastest piston-powered aircraft of their time (e.g., P-47s reaching **433 mph**). With modern modifications (e.g., supercharging, fuel injection, or turbocharging), it could theoretically enable high-speed flight in a modern or restored airframe.

7. **Modular and Upgradeable**

- **Supercharging or turbocharging** for high-altitude performance

- **Fuel injection** (instead of carburetors) for better fuel efficiency and power consistency

- **Exhaust modifications** for increased power output

- Some owners have successfully pushed these engines beyond their original specifications with careful tuning.

---

### **Cons of the Farris 1850-0L (Curtiss-Wright 18500L Engine)**

1. **Extremely High Maintenance Requirements**

- **Cooling system demands** High power output generates massive heat, requiring **large radiators, high-capacity coolant, and constant monitoring** to prevent overheating.

- **Lubrication needs** The engine consumes **large quantities of oil** (often requiring **10-20 gallons per hour** in high-power settings). Oil changes must be frequent and thorough.

- **Ignition and fuel system wear** Multiple magnetos, spark plugs, and carburetors (or fuel injectors) require constant inspection and replacement.

- **Labor-intensive overhauls** Unlike modern engines, these require **disassembly, inspection, and replacement of critical components** (e.g., pistons, valves, crankshaft bearings) at regular intervals.

2. **Fuel Consumption and Cost**

- The engine **burns fuel at an astonishing rate** estimates suggest **100 gallons per hour** at full throttle, depending on modifications.

- **Fuel costs** for high-performance flights (especially with alcohol or jet fuel) can be **extremely expensive**.

- **Fuel system reliability** is a concern; carburetor icing, fuel starvation, or vapor lock can be issues at high altitudes or in extreme conditions.

3. **Limited Modern Parts and Support**

- While Curtiss-Wright engines were widely used, **modern production of replacement parts has largely ceased**.

- **Aftermarket support** exists but is **fragmented and expensive**. Many components must be **machined or fabricated by hand**.

- **No OEM support** Unlike modern engines, there is no manufacturer-backed warranty or technical service network.

4. **Weight and Space Requirements**

- The 18500L is **heavy** (estimates suggest **1,500 2,000 lbs dry weight**), which impacts **takeoff performance, maneuverability, and fuel efficiency**.

- Requires **significant bay space** in the aircraft, potentially limiting payload or internal configuration.

5. **Reliability and Longevity Concerns**

- While robust, **piston engines of this power level are not as durable as modern turbofan or turboprop engines**.

- **Critical components (e.g., crankshaft, connecting rods) are stress-prone** and may fail catastrophically if not maintained perfectly.

- **No flight hours records** for modern applications historical engines may have been run differently than they would be today.

6. **Regulatory and Safety Challenges**

- **FAA/EASA certification** for modern use is **difficult** due to the engine s age and lack of modern compliance.

- **Insurance costs** for flying such an engine are **extremely high** due to perceived risk.

- **Emergency landing capabilities** are a concern if the engine fails mid-flight, the aircraft may lack the performance to recover safely.

7. **Limited Practical Use Cases**

- **Not suitable for commercial or passenger use** the power-to-weight ratio is better suited for military or experimental roles.

- **Not economical for most private pilots** operating costs (fuel, maintenance, insurance) far exceed those of modern engines.

- **Mostly a "collector s item"** few practical applications exist beyond **military reenactments, static displays, or highly specialized projects**.

8. **Environmental and Noise Concerns**

- The engine is **extremely loud**, generating **high noise pollution** this could be a legal issue in some regions.

- **Exhaust emissions** (especially with alcohol fuels) may not meet modern environmental standards.

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### **Conclusion**

The **Farris 1850-0L with a Curtiss-Wright 18500L engine** is a **monumental piece of aviation engineering**, offering **unmatched power** for its era and niche applications. However, its **maintenance demands, fuel consumption, lack of modern support, and high operational costs** make it **impractical for most modern uses**. It is best suited for:

- **Military historians and aviation enthusiasts** looking to restore or display a high-performance piston engine.

- **Experimental aircraft projects** where extreme power is required (e.g., high-speed interceptors, bomber conversions).

- **Static displays or museum pieces** where functionality is secondary to historical significance.

For **practical aviation**, modern **turbocharged piston engines (e.g., Continental TSIO-550), turboprops (e.g., PT6), or turbofans** offer **far better reliability, efficiency, and support** at a fraction of the cost.

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### **Recommendation**

- You are a **dedicated aviation historian** with the **resources and expertise** to maintain such an engine.

- You have a **specific, high-performance aircraft project** (e.g., restoring a Cold War-era interceptor) where this engine is the **only viable option**.

- You are prepared for **extremely high maintenance costs, fuel expenses, and regulatory hurdles**.

- You have **access to skilled mechanics** familiar with high-performance piston engines.

- You are looking for a **practical, economical, or low-maintenance** aircraft engine.

- You do not have the **time, money, or technical knowledge** to handle the engine s demands.

- You are not working on a **highly specialized or historical project** where this engine is justified.

For most pilots and operators, **modern engines (turbocharged pistons, turboprops, or turbofans) are far superior** in terms of **reliability,

Details:

Call to use a shipping service other than the ones listed. Sells new and surplus product develops channels to purchase such. Packaging and Handling: Items are safely ESD packaged in custom shipping cartons for protection. All products are guaranteed to be working but may show signs of use if purchasing a used product.

part #: 18500l prices

• $131.12-$229.00

specifications valvesplumbing:

• brand: Farris Engineering
• mpn: 1850-0l

seller valvesplumbing:

• # reviews: 1990 86
• rating: 99.6%
• city: 1 Millennium Dr, Willingboro, NJ 08046

payments valvesplumbing:

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offer valvesplumbing:

• started: April 12, 2026
• availability: In Stock
• quantity: 1
• sold: 0
• options: Ship-to-home

shipping valvesplumbing:

• transit: 27-32 Days
• cost: $12.90
• service: Standard
• class: Standard
• type: Fixed

returns valvesplumbing:

• method: Money back
• paid by: Buyer
• time: 30 Days
• policy: Returns Accepted

general valvesplumbing:

• condition: Used
• Hydraulics, Pneumatics, Pumps Plumbing > Valves Manifolds > Relief Valves

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