Платинаста Авион · 2026
Cicare 8 Примарна функција: Ултралесен хеликоптер
- Платинаста награда A' Design Award 2026 in Авион
- CLIENT: Cicaré
- Estimated Number of Design Views: 856,368
- Verification code 9F2E6E78FD · Verify this award
Colors
About Cicare 8 Примарна функција: Ултралесен хеликоптер
Текст: Cicaré 8 е двоседен ултралесен хеликоптер со полу-моноструктурна кабина изработена од јаглеродни влакна. Аеродинамичкиот надворешен дизајн интегрира препознатливи елементи во автомобилски стил и обезбедува исклучителна панорамска прегледност за пилотите. Неговата структурна конфигурација комбинира композитна пилотска кабина со мрежеста носечка конструкција изработена од високоцврста аеронаутичка челична легура. Развиен за лична рекреација и обука за летање, овој летал нуди извонредна агилност, ниски оперативни трошоци и строго почитување на меѓународните стандарди за сертификација.
About the Платинаста награда A' Design Award
Cicare 8 Примарна функција: Ултралесен хеликоптер е добитник на Платинастата награда A' Design Award, високо престижно признание што се доделува на навистина исклучителни, елегантни и величествени дизајни. Платинастите добитници се чуда на создавањето, сведоштва за границите на интелектуалната креативност и ја покажуваат неспоредливата професионалност и генијалност на нивните дизајнери. Се очекува овие дизајни да бидат најпознатите дела што ја дефинираат естетиката на една епоха, придонесуваат за општествената благосостојба и ги поместуваат границите на уметноста, науката, дизајнот и технологијата. Cicare 8 Примарна функција: Ултралесен хеликоптер покажува трансцендентно ниво на извонредност и со своите корисни карактеристики го прави светот подобро место. Cicare 8 Примарна функција: Ултралесен хеликоптер е дело што ја освои Платинастата награда A' Design Award и што ги разбудува желбите, инспирира, радува и предизвикува голема радост.
Press Kit
- Unique Properties
- The Cicare 8 transforms aeronautical engineering into a sophisticated industrial product. The design introduces a new brand identity through a carbon fiber semi monocoque cabin that balances aggressive aesthetics with functional ergonomics. Key contributions include optimized internal volumes for comfort and expanded glazing for panoramic visibility of the skid tips. The digital workflow ensures surface continuity and high end finishes. By exposing the tubular tail the design maintains the brand DNA with an honest structural aesthetic that emphasizes lightness and agility.
- Dimensions & Packaging
- Technical Specifications
Dimensions:
Rotor: 6400mm
Length: 6900mm
Height: 2700mm
Cabin:
2-seater (Side-by-side)
Engines:
EPA SA-917TI: 135HP (Max) / 115HP (Cont.)
Rotax 915 iS: 141HP (Max) / 135HP (Cont.)
Weight:
Empty: 300kg
MTOW: 480kg - 525kg
Performance:
Max Speed: 157km/h
Cruise: 120km/h
Endurance: 2.4h
Key Features:
Carbon fiber semi-monocoque
First 600kg class ULM type-certified helicopter - Tags
- Ultralight Helicopter, Helicopter, Carbon Fiber Cabin, Aeronautical Design, Two-Seater Aircraft, Industrial Design, Innovative Cockpit, Cicare Aviation, Pirincho Cicare, Indalecio Sabbioni
- Production Technology
- The cabin is a carbon fiber and epoxy resin semi monocoque manufactured using vacuum bagging to optimize the strength to weight ratio.
The structure integrates a spatial reticulated airframe made of aeronautical sae 4130 steel. The tail boom utilizes aluminum 2024 t6 struts designed to withstand high maneuvering stresses.
The design utilized a digital workflow from 3d modeling to CNC machined molds ensuring aerospace grade surface continuity and structural integrity. - Design Challenge
- The main challenge was bridging a 60-year-old artisanal legacy with modern industrial design. A key creative conflict was aesthetic: I proposed a minimalist approach, exposing the iconic tubular tail to reduce weight and costs, whereas the founder sought a fluid, integrated and covered look.
We had to balance visibility against structural rigidity while integrating a carbon fiber cabin with a steel frame. - Research
- The research bridged artisanal excellence with industrial precision through systemic design. The initial phase involved qualitative interviews with directors engineers pilots and technicians. These insights guided the ergonomic optimization of the cabin. The methodology integrated iterative prototyping with advanced 3d modeling validated by flight tests. Results led to a carbon fiber semi monocoque cabin with structural safety and visibility of the skid tips. This research was fundamental in securing global certifications and boosting international sales.
- Inspiration
- the cicare 8 is inspired by the engineering of augusto cicare, translating a 60 year heritage of artisanal excellence into a sophisticated industrial product. the design finds its motive in feline facial features, where window frames resemble the alert eyes of a predator. this organic morphology creates an aggressive profile that communicates agility and establishes a unique identity. driven by market demand for side by side seating, it integrates carbon fiber and a digital workflow while maintaining the brand dna.
- Project Duration
- the design process was conducted from 2013 to 2015 in saladillo buenos aires argentina. the aircraft was exhibited at major airshows including aero friedrichshafen and eaa airventure oshkosh where it received the lindbergh award for its outstanding fit and finish. in 2016 it earned the sello de buen diseno and the innovar award. a key milestone was achieved with the german ltf ulh certification making it the worlds first 600kg class ulm type certified helicopter.
- Operation Flow
- Access is intuitive through wide doors leading to a side by side cockpit optimized for leg comfort.
Pilots interact with a unique patented adjustable control system and a state of the art instrument panel.
The flight experience is defined by panoramic visibility including a specific design focus that allows viewing the skid tips from the inside for safer landings.
The centrifugal clutch ensures a seamless linkage between engine and transmission providing a gradual engagement imperceptible to passengers. - Patents
- Patented. Main Rotor Control System. Patent No. Arg 248.899. Cicaré. Argentina.
Cabin design Copyrights belong to Indalecio Sabbioni, 2015.
