Mikrolakih Zrakoplova) U Republici Hrvatskoj

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REPUBLIKA HRVATSKA Hrvatska agencija za civilno zrakoplovstvo Popis prihvaćenih tipova MLZ (mikrolakih zrakoplova) u Republici Hrvatskoj tip/model zrakoplova motor podvozje napomena klasa MLZ: gyro MTOsport Rotax 912 S, UL - klasa MLZ: I Airmax P-22 Sea Max Rotax 912 - ALPI AVIATION srl Pioneer 200 Rotax 912 - ALPI AVIATION srl Pioneer 300 Rotax 912 - CH601 Rotax 912 - greškom propušten u inicijalnom izdanju Evektor 97 Eurostar Rotax 912 - Ferrari Tucano Rotax 582 - Fly Synthesis (ex. Rodaro) Storch Rotax 582 - Fly Synthesis Storch HV/SV Rotax 912 - Pipistrel Sinus Rotax 912 - Pipistrel Virus Rotax 912 - Rodaro Kangaroo Rotax 503 - Rodaro Wallaby Rotax 503 - SILA 450C Rotax 912 - TL Ultralight TL-2000 Sting Carbon Rotax 912 - Ultralair Weedhopper JC 31/ Europa II Rotax 503 - Rotax 582 - klasa MLZ: II Apollo C15 Rotax 503 Apollo Racer GT/R Apollo Delta Jet /R Apollo Jet Star/R Rotax 582 Apollo Racer GT/R Apollo Jet Star/R Apollo Delta Jet /R Rotax 912 Apollo Racer GT/R Apollo Jet Star/R Apollo Delta Jet /R Apollo C15 D Rotax 503 Apollo Racer GT/R Apollo Jet Star/R Apollo Delta Jet /R Rotax 582 Apollo Jet Star/R Apollo Delta Jet /R Apollo Racer GT/R Pipistrel Spider samo uz pisano odobrenje proizvođača Rotax 912 Pipistrel Twister samo uz pisano odobrenje proizvođača Apollo Racer GT/R Apollo Delta Jet /R Apollo Jet Star/R 12. svibanj 2016. stranica 1 od 2 tip/model zrakoplova motor podvozje napomena Apollo C15D BMW Apollo Jet Star greškom propušten u inicijalnom izdanju Apollo C4M Rotax 503 Apollo Racer GT/R Rotax 582 Apollo Racer GT/R Rotax 912 Apollo Racer GT/R Apollo CX Rotax 503 Apollo Jet Star/R Apollo Racer GT/R Rotax 582 Apollo Jet Star/R Apollo Racer GT/R Rotax 912 Apollo Jet Star/R Apollo Racer GT/R Apollo CX14 Rotax 503 Pipistrel Spider samo uz pisano odobrenje proizvođača Apollo CXM Rotax 503 Apollo Racer GT/R Apollo Jet Star/R Rotax 582 Apollo Jet Star/R Apollo Racer GT/R Rotax 912 Apollo Racer GT/R Apollo Jet Star/R Keitek Hazard 13 Rotax 503 Pipistrel Spider Pipistrel Plus Rotax 582 Pipistrel Spider Pipistrel Plus Rotax 912 Pipistrel Spider Keitek Hazard 15 Rotax 503 Pipistrel Spider Rotax 582 Pipistrel Spider Rotax 912 Pipistrel Spider 12. svibanj 2016. stranica 2 od 2.

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General Aviation Aircraft Propulsion: Power and Energy Requirements
UNCLASSIFIED General Aviation Aircraft Propulsion: Power and Energy Requirements • Tim Watkins • BEng MRAeS MSFTE • Instructor and Flight Test Engineer • QinetiQ – Empire Test Pilots’ School • Boscombe Down QINETIQ/EMEA/EO/CP191341 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Contents • Benefits of electrifying GA aircraft propulsion • A review of the underlying physics • GA Aircraft power requirements • A brief look at electrifying different GA aircraft types • Relationship between battery specific energy and range • Conclusions 2 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Benefits of electrifying GA aircraft propulsion • Environmental: – Greatly reduced aircraft emissions at the point of use – Reduced use of fossil fuels – Reduced noise • Cost: – Electric aircraft are forecast to be much cheaper to operate – Even with increased acquisition cost (due to batteries), whole-life cost will be reduced dramatically – Large reduction in light aircraft operating costs (e.g. for pilot training) – Potential to re-invigorate the GA sector • Opportunities: – Makes highly distributed propulsion possible – Makes hybrid propulsion possible – Key to new designs for emerging urban air mobility and eVTOL sectors 3 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Energy conversion efficiency Brushless electric motor and controller: • Conversion efficiency ~ 95% for motor, ~ 90% for controller • Variable pitch propeller efficiency
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Apis Contest Taurus(Electro)
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The Power for Flight: NASA's Contributions To
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Battery Electric Aircraft Feasibility Investigation Including a Battery-In-Wing Conceptual Design
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1.1 Electric VTOL
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Wh/Kg Batteries
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Charging Forward New Evtol Concepts Advance “Look! up in the Sky! It’S a Car — It’S a Plane — No, It’S My Uberair!”
The two-seat Lilium Eagle made its first flight in April. Each canard features two rows of three electric ducted fans, while each wing houses four sets of three fans. (Lilium graphic) Charging Forward New eVTOL Concepts Advance “Look! Up in the sky! It’s a car — It’s a plane — No, it’s my UberAIR!” By Kenneth I. Swartz o those immersed in the world of traditional helicopters, manager of special projects, Nikhil Goel, described Uber’s plans it may take a little time to fully comprehend what Uber for moving urban transportation to the skies with electric TElevate’s on-demand urban air transportation vision vertical takeoff and landing (eVTOL) aircraft. actually entails. The Uber Elevate white paper released the following month, Ever since Uber’s ride hailing service (worth $68B at its last funding “Fast-Forwarding to a Future of On-Demand Urban Air round) launched its smartphone app in 2011, the San Francisco- Transportation,” elaborated plans for an urban air transportation based transportation and technology company has expanded to service using thousands of eVTOL aircraft — eventually 450 cities in 73 countries, and now serves 60 million monthly users. autonomously piloted — with very low direct operating costs, low noise and zero “tailpipe” emissions. The white paper gave Today, Uber’s portfolio includes several transportation services, commercial expression to research by NASA scientists and but all of its vehicles use the same congested urban roads, other researchers who hypothesized nearly a decade ago that a tunnels and bridges. new era of transformational vertical flight could dawn with the advent of distributed electric propulsion.
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NASA Green Flight Challenge: Conceptual Design Approaches and Technologies to Enable 200 Passenger Miles Per Gallon
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D1.1: Concept of Modular Architecture for Hybrid Electric Propulsion of Aircraft December, 2017
Ref. Ares(2017)5981497 - 06/12/2017 D1.1: Concept of Modular Architecture for Hybrid Electric Propulsion of Aircraft December, 2017 Deliverable D1.1.: Concept of Modular Architecture for Hybrid Electric Propulsion of Aircraft Disclaimer The information, documentation and figures in this deliverable are written by the MAHEPA project consortium under EC grant agreement no. 723368 and do not necessarily reflect the views of the European Commission. The European Commission is not liable for any use that may be made of the information contained herein. | MAHEPA Consortium | Page 2 of 87 Deliverable D1.1.: Concept of Modular Architecture for Hybrid Electric Propulsion of Aircraft EXECUTIVE SUMMARY The purpose of this report is to introduce the concept of a modular propulsion system architecture, suitable to cover a wide set of implementations on different hybrid-electric aircraft. The core components identified allow for modularity of power creation, power routing and power delivery from an arbitrary number of power generation modules (technology agnostic) to an arbitrary number of electric drive motors. In this novel approach to conceptual design of hybrid-electric powertrains, two research achievements are particularly worth mentioning. The first is the identification of functionality, power and data interfaces for each module. In total seven types of modules have been identified as the foundation of every serial hybrid architecture, forming an effective toolset for the conceptual design of the next generation hybrid-electric aircraft. To demonstrate the versatility of this concept, several well-known hybrid-electric aircraft projects were represented using the developed modules. A reliability-driven shaping of powertrain architectures is the second notable achievement of this research work.
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