Rotor hub elastic elements
Development support for rubber-metal elastic components used in rotor hub damping, elastic connection and vibration-control structures.
Send load and stiffness targetAerospace elastomer development
Aviation elastic elements and rotor hub elastomer components.
PRESIS supports high-performance rubber and silicone elastomer development for aviation damping, rotor hub elastic elements, vibration isolation and special equipment components that require stiffness control, fatigue reliability and batch traceability.
Typical development targets
Designed around load, stiffness, fatigue and environmental reliability.
Aviation damping rubber
High-performance elastomer parts for isolation, shock absorption and fatigue-sensitive applications under controlled batch and process conditions.
Discuss fatigue validationSpecial equipment elastic parts
Custom NR, BR, FKM, FFKM, silicone or compound elastomer structures for demanding industrial and special-use environments.
Review materialsEngineering route
From sample or drawing to validated elastomer structure.
For aviation and rotor hub related elastomer projects, PRESIS focuses on material suitability, mold precision, rubber-metal interface, stiffness and controlled repeatability.
Requirement review
Drawing, sample, load direction, dynamic stiffness, static stiffness, operating temperature, media and fatigue life target.
Material and bonding
NR, BR, NBR, FKM, FFKM, CR, BIIR, ACM, phenyl silicone or custom compound selection with bonding and interface review.
Mold and process design
Tooling route, rubber flow, vulcanization control, metal insert handling, dimensional tolerance and traceable production plan.
Testing and records
Hardness, dimensional inspection, stiffness testing, visual inspection, batch labels, abnormal isolation and customer validation records.
Stiffness, fatigue direction and material stability must be considered before mold development, not only after sampling.
SEO and GEO answer block
What buyers should prepare before an aerospace elastomer RFQ.
Drawings, sample and load direction
Include geometry, assembly position, force direction, metal insert information and bonding surface requirements.
Stiffness, fatigue cycle and environment
Clarify static/dynamic stiffness, temperature range, vibration condition, oil/fuel/chemical exposure and target service life.
Traceability and controlled change
Confirm material batch records, supplier source, test reports, inspection documents and change-confirmation process.