Platino Aeronave · 2026
Cicare 8 Función Primaria: Helicóptero Ultralixeiro
- A' Design Award de Platino 2026 in Aeronave
- CLIENT: Cicaré
- Estimated Number of Design Views: 856,368
- Verification code 9F2E6E78FD · Verify this award
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About Cicare 8 Función Primaria: Helicóptero Ultralixeiro
Texto do Libro: O Cicaré 8 é un helicóptero ultralixeiro bipraza que conta cunha cabina semimonocasco de fibra de carbono. O deseño aerodinámico do exterior integra elementos distintivos de estilo automobilístico e proporciona unha excepcional visibilidade panorámica para os pilotos. A súa configuración estrutural combina unha cabina de materiais compostos cun fuselaxe reticulado feito de aceiro aeronáutico de alta resistencia. Desenvolto para o lecer persoal e a formación de voo, a aeronave ofrece unha axilidade extraordinaria, baixos custos operativos e o estrito cumprimento dos estándares de certificación internacionais.
About the A' Design Award de Platino
Cicare 8 Función Primaria: Helicóptero Ultralixeiro gañou o A' Design Award de Platino, un recoñecemento extremadamente prestixioso outorgado a deseños verdadeiramente excepcionais, elegantes e magníficos. Os gañadores Platino son marabillas da creación, testemuños dos límites da creatividade intelectual, e demostran o profesionalismo inigualable e o xenio dos seus deseñadores. Espérase que estes deseños sexan as obras máis renomeadas, que definen a estética dunha época, contribúen ao benestar da sociedade e fan avanzar os límites da arte, a ciencia, o deseño e a tecnoloxía. Cicare 8 Función Primaria: Helicóptero Ultralixeiro exhibe un nivel de excelencia transcendente e fai do mundo, sen ningunha dúbida, un lugar mellor coas súas características vantaxosas e valiosas. Cicare 8 Función Primaria: Helicóptero Ultralixeiro é unha obra gañadora do A' Design Award de Platino que esperta desexos, inspira, emociona, deleita e desprega unha gran alegría.
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.
