04/07/2026
Titanium vs Stainless Steel Screws in UAV Applications
During the development of unmanned aerial vehicles (UAVs), many teams focus on flight control, motors, batteries, and weight reduction of the fuselage. However, what truly determines the long-term reliability of a device often involves those seemingly insignificant titanium screws and stainless steel screws. Many people believe that titanium screws are lighter and more expensive, so they must be better; others think that stainless steel screws are mature and stable, sufficient for most applications. In fact, in engineering design, this is not a simple matter of material selection.
The real question to be answered is not which material is better, but which material's non-standard screws are more suitable for your product.
Take the most common Ti-6Al-4V (TC4/Grade 5) in the UAV industry as an example. Its density is approximately 4.43 g/cm³, which is about 40% to 45% lighter than the density of 304 or 316 stainless steel, which is approximately 7.9 to 8.0 g/cm³. Therefore, it has a significant weight reduction advantage in long-duration UAVs, VTOL aircraft, and high-performance racing UAVs. Additionally, TC4 has an average tensile strength of 895 to 930 MPa and a yield strength of about 825 to 880 MPa, with very excellent specific strength. But materials always have two sides. The elastic modulus of TC4 is approximately 114 GPa, significantly lower than the 190 to 200 GPa of stainless steel, meaning it will undergo greater elastic deformation under the same load; moreover, titanium alloy screws need to pay attention to the risk of thread locking (Galling), so during assembly, reasonable surface treatment, lubrication methods, and locking processes are usually required. If only a few grams of weight are to be reduced by choosing titanium alloy screws, but the structural design and actual working conditions are ignored, it may not be the best solution.
In contrast, stainless steel remains one of the most widely used materials in the UAV industry. 304 and 316 stainless steel have excellent corrosion resistance and tensile strength typically ranging from 515 to 620 MPa, suitable for most structural connections; if the equipment requires higher strength, many engineers will choose 17-4PH or A286. Among them, 17-4PH, after hardening treatment, can reach tensile strengths of 1000 to 1300 MPa while maintaining good corrosion resistance and dimensional stability, thus often used in gimbal mechanisms, precision brackets, and load-bearing components; A286 also combines high strength, good fatigue resistance, and high-temperature resistance, and is very common in long-term vibration, high-cycle load, and aerospace fasteners. Therefore, what truly determines the material selection is not the material price, but what function the non-standard screws in the entire machine perform and what working environment they need to face.
Therefore, when customers ask us which material to choose for non-standard screws, we usually do not directly answer "titanium alloy" or "stainless steel", but hope to first consult the drawings. Because material selection cannot be separated from the product itself. Only by understanding what function this non-standard screw is performing and what working environment it needs to face can we make an informed decision.
For example, folding UAVs need to maintain the consistency of the arm position during each unfolding, folding, and flight process. Therefore, the folding hinge shaft not only needs to withstand continuous vibration and cyclic loads but also needs to consider positioning accuracy and wear resistance.
Many designs initially use standard bolts as hinge shafts because they are convenient to purchase and have lower costs. But as the number of flights increases, engineers often find that the hinge gap gradually widens, the positioning consistency after unfolding decreases, and in severe cases, the arm may slightly shift, affecting flight stability and subsequent maintenance. Therefore, in such structures, we prefer to use custom non-standard screws such as shoulder screws. The shoulder part is responsible for rotation and positioning, while the threaded part is responsible for locking, enabling a single screw to perform both the rotating shaft and connection functions. For drones with high requirements for lightweight, TC4 (Ti-6Al-4V) material is usually chosen, with a density of approximately 4.43 g/cm³. Compared to stainless steel with a density of about 7.9-8.0 g/cm³, it can reduce the weight by approximately 44%, while the tensile strength can reach 895-930 MPa. If combined with solid lubrication coating and the customized shoulder length for the hinge thickness, it not only reduces friction and wear but also enhances the service life and repetitive positioning stability of the folding mechanism.
If the customer has not yet determined the material for the non-standard screws, there is no need to worry. You only need to provide product drawings, samples, assembly photos, or tell us the working environment, load conditions, service life, and performance requirements of the product. We can conduct a comprehensive assessment based on the mechanical properties, weight, corrosion resistance, processing technology, cost, and maintenance of different materials, and assist you in choosing a more suitable material, rather than directly recommending a more expensive or common solution.
At the same time, according to the project requirements, Sh*titong can also provide:
Dimension and tolerance inspection: thread go-no-go gauge inspection (GO/NO GO gauge)
Head diameter/thickness deviation (±0.05mm) total length tolerance (such as M6 screws ±0.2mm)
Tensile strength (ISO 898-1): 8.8 grade: ≥800MPa | 12.9 grade: ≥1220MPa
Hardness test (HRC/HV): 8.8 grade: HRC 22-32 | 12.9 grade: HRC 39-44
Torque test: failure torque ≥ 90% of the nominal value (such as M6 8.8 grade screws ≥ 10Nm)
Salt spray test (ASTM B117): Dacromet: 1000h without rust
Metallographic structure analysis: 8.8 grade screws: tempered sorbite (observed under a 500x microscope) | 12.9 grade screws: prohibited untempered martensite (to prevent brittle fracture)
Environmental adaptability: high and low temperature cycling (-40℃~120℃, 20 cycles after the thread does not deform)
Non-standard screws not only need to be processed, but also need to meet the quality requirements for subsequent verification and mass production.
What the customer truly needs is not a factory that can produce non-standard screws, but an engineering partner who can discuss the design of the drone solution together. Instead of asking "How much is this non-standard screw?", we would rather hear the customer say: "Here is our non-standard screw drawing. Can you help us review if there are any more suitable materials, structures, surface treatments, and inspection schemes?" 。 A truly suitable non-standard screw for the product is not made of the most expensive material, but is the result of the most reasonable engineering choice after a thorough understanding of the product structure.
If you are developing a drone project, please send us the non-standard screw drawings, samples or application requirements. We are willing to work with you to complete this engineering judgment, covering material selection, structural optimization, surface treatment and testing requirements.