UAV Flame Effect System with Powdered-Fuel Fluidization
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Unmanned aerial vehicles (UAVs) with flame emitting systems for controlled burns are prohibitively expensive due to the weight and cost of thick-walled tanks and valves, limiting their applicability.
Innovation Solution
A flame effect system using a hopper for powdered fuel, a propellant tank, and a nozzle, with a fluid path and igniter, reduces weight and cost by utilizing powdered fuel and a controller for controlled combustion.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a thick-walled tank and valves are used to store liquid fuel, then fuel leakage risk is reduced, but system weight and cost increase significantly
Solution Approach 1:
The patent changes the physical state of fuel from liquid to powder form. This parameter change eliminates the need for thick-walled pressure-containing tanks and complex valves, as powder fuel can be stored in simple gravity-fed hoppers. The powder fuel flows through fluidized beds and combustion chambers without requiring high-pressure containment, thereby dramatically reducing system weight while maintaining safety through the inherent properties of powder fuel handling.
Solution Approach 2:
The patent replaces the mechanical liquid fuel delivery system (pumps, high-pressure valves, thick-walled tanks) with a gravity-based powder fuel delivery system. Powder fuel is fed through gravity into a fluidized bed where it mixes with oxidizer and combusts. This substitution eliminates heavy mechanical components while achieving reliable fuel delivery and combustion control.
2Reliability
If a thick-walled tank and valves are used to store liquid fuel, then fuel leakage risk is reduced, but system cost increases prohibitively
Solution Approach 1:
Changing fuel from liquid to powder form fundamentally simplifies the containment and delivery system. Instead of expensive aerospace-grade pressure vessels and sealed valve assemblies, the system uses simple gravity-fed hoppers and fluidized bed combustors. This parameter change makes the system manufacturable at much lower cost while maintaining fuel safety through the inherent characteristics of powder fuel.
Solution Approach 2:
The patent employs simpler, less expensive components that can be easily manufactured and replaced if needed. The hopper and fluidized bed system uses basic materials and straightforward mechanics rather than expensive, complex liquid fuel systems. This approach aligns with using simpler, more cost-effective components that achieve the same functional outcome.
3Weight of moving object
If a large lift capacity UAV is used to support the flame emitting system, then the system weight is accommodated, but operational cost increases
Solution Approach 1:
The patent's parameter change from liquid to powder fuel fundamentally reduces the flame emitting system weight. Powder fuel systems eliminate heavy pressure tanks and pumps, allowing the entire flame system to weigh significantly less. This weight reduction enables deployment on smaller, more economical UAV platforms, thereby reducing operational costs while maintaining the controlled burn capability.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The system reduces the weight and cost of UAVs by eliminating the need for thick-walled tanks and valves, enabling efficient and controlled flame effects while minimizing the risk of fuel leakage.
Implementation Method 1
the propellant tank is configured to expel the propellant through the fluid path to fluidize the powdered fuel within the fluid path and to drive the fluidized powdered fuel through the nozzle
Implementation Method 2
The igniter is configured to activate to initiate a combustion reaction between the fluidized powdered fuel and oxygen in the atmosphere
Data Source
AI summary
A flame effect system for an unmanned aerial vehicle (UAV) includes a hopper configured to store a powdered fuel, a propellant tank configured to store a propellant, and a nozzle configured to expel the powdered fuel into an atmosphere. Furthermore, the flame effect system includes a fluid path extending from the propellant tank to the nozzle. The hopper is fluidly coupled to the fluid path at an intersection between the propellant tank and the nozzle, the hopper is configured to enable the powdered fuel to flow into the fluid path, and the propellant tank is configured to expel the propellant through the fluid path to fluidize the powdered fuel within the fluid path and to drive the fluidized powdered fuel through the nozzle.

