Heavy Lift and Long Duration Co-axial Unmanned Aerial Vehicles

Slides:



Advertisements
Similar presentations
UAV’s: Planes of the New Millennium
Advertisements

IPS 3 for Marine Commercial (Rating 3) & IPS 3 Semi planing
A Brief Introduction to Helicopters
MicroCART Micro processor C ontrolled A erial R obotics T eam Abstract MicroCART is a group of EE/CprE students tasked with developing an autonomous helicopter.
The Helicopter.
Мi-38 Utility Helicopter. of © 2014 Russian Helicopters, JSC All rights reserved Mi-38 concept Advanced technologies, components, systems and materials.
Klapmuts and Mecotec Engineering. Advantages No more lifting of heavy crates Less stress for hangers as well as birds (thus better meat quality) A fully.
ODS3F –Observation and Detection Systems For Forest Fire Monitoring
Unmanned Aerial Vehicles Presentation. Customization for each client Each order is specifically designed to meet each clients’ aerial needs. On-board.
Helicopter Performance, Limitations, and Load Calculations
Helicopter Safety for SAR Operations. Helicopter Rescue Checklist, Before you Call Before you consider using a helicopter for a rescue: Have we cross-trained.
Helicopter Flight. US Marine Corps Scarlet and Gold.
AVIATION HISTORY Lecture 3c: Helicopters By Zuliana.
Range (nm) Payload (kg) Payload (lb) Endurance (hr) As a total system, Vigilante.
From design… …development… … CFD analyses…
INNOCON Innovative solutions to the modern real time Arial surveillance challenges.
Automatic Control & Systems Engineering Autonomous Systems Research Mini-UAV for Urban Environments Autonomous Control of Multi-UAV Platforms Future uninhabited.
Chapter I. Introduction. Naval Architecture: the science and engineering of designing ships and other kinds of waterborne crafts. Kinds of ships Sub systems.
Moody F061 ISE Conceptual System Design “Sets the Stage” State the problem Identify the need Conduct advanced system planning & feasibility analysis.
HELICOPTER FOR U.N. MISSIONS Mi-171A2Mi-171A2. IMPROVED PERFORMANCES IMPROVED PERFORMANCES UP-TO-DATE AVIONICS UP-TO-DATE AVIONICS NEW LEVEL OF SAFETY.
INTERNATIONAL WORKSHOP ON MARINE POLLUTION CONTROL 8 th June 2006, Athens (GR) OIL SEA HARVESTER TST4-CT ww.osh-project.org THE OIL SEA HARVESTER.
You Can Fly! WELCOME TO MIT!  Instructors: Sameera Ponda and Kostas Speridakos.
Aviation “The Power of Flight” Engineering Technology Mr. Austin Engineering Technology Mr. Austin.
Subject: Science Topic: Flight Technology Grades: Teacher Notes.
UAV Helicopter Project 12-May-08 Presented by Mark Diel Whirled Air Incorporated Stanford University.
Aircraft Recognition Lecture Leading Cadet Training Airmanship 2 5.
Better Robots 1 The Goal: More Robots Enabling Fewer Soldiers Military “robots” today lack autonomy –Currently, many soldiers control one robot –Want few.
AeroVironment, Inc.  May, A Look at Safe, Quiet, Clean, Efficient Personal Travel by Air Personal Air Vehicle Conference Burlingham,
Aircraft Services Company Aircraft Services Company.
Partnership in Unmanned Marine Systems GATE Electronics TR Technologies TURKEY.
HELICOPTER By Vinod Kumar K.
Computational Mechanics and Robotics The University of New South Wales
DARPA ARES Program Ken Dorsett 25October 2014.
Wind Tunnels Aeronautical and Non-aeronautical applications.
FRR Presentation IF AT FIRST YOU DON’T SUCCEED, TRY AGAIN… AND AGAIN AND AGAIN AND AGAIN.
AEM 5333 UAV Search and Surveillance. Mission Description Overhead surveillance and tracking – Humans on foot – Moving vehicles Onboard GPS transceiver.
Rotorcraft Vision 2025 April 14, 2000 George Price NASA Ames Research Center
Pollution prevention preparedness and response Kristján Geirsson Environment Agency of Iceland EPPR-meeting 10 Nov
Doris Hamill UAV Business Development Lead NASA Langley Research Center and Hampton Roads First Responders.
Projectile Kinetic Energy Reduction System (PKERS)
Introduction to IWA. The IWA is based on a patented, next generation design called the Internal Wing Aircraft. The concept brings three separate wings.
Presented by:- Suman Kumar. INTRODUCTION : Quad-rotor helicopters are emerging as a popular unmanned aerial vehicle configuration because of their simple.
Final Design Team 6 December 2 nd, UAV Team Specializations David Neira – Power & Propulsion Josiah Shearon – Materials Selection & Fabrication.
AVIATION HISTORY WEEK 10 Helicopters.  Introduction  How a helicopter flies  The advantages of Helicopter.
AVIATION HISTORY Helicopters. Introduction  Helicopter is an aircraft than can take- off and land vertically.  Nowadays, they became one of the most.
Drone Categorization October Outline Platforms Multi-rotor Fixed Wing Helicopter Baloon Simulators Power Systems Electric Gas/Nitro Proprietary.
Progress Report of the Russian Federation Project 2013 “Development of Safety Systems in Implementation of Economic and Infrastructural Projects in the.
7 조 강창호 강애량 김창규 오혜영 최재영 이홍일 MQ-9B. 1. Goal of Project 2. Project members 3. Schedule 4. Analysis of UAS 4.1 Requirement analysis 4.2 Air vehicle.
Mini Autonomous Flying Vehicle CASDE is part of the National effort to develop a Micro Air Vehicle. CASDE has chosen a Mini Vehicle, in the short term,
By: Stuti Vyas( ) Drashti Sheth( ) Jay Vala( ) Internal Guide Mr. J. N. Patel.
QUADCOPTER.
The Challenges of Maritime Security - Drones at Sea Rune Storvold, Senior Scientist Northern Research Institute (Norut) DESSI Conference on Security Investment.
Commercial Drones: Highways in the Sky, Unmanned Aerial Systems (UAS), Market Shares, Strategies, and Forecasts, Worldwide, 2015 to 2021 Published: Jan.
SME Associates LLC Providing Innovative Solutions DRONE MONITORING JAMES P. MENGE PE, CHP 1.
Fire Service Incidents. Today’s fire service does much more than fight fires. The Fire Service has become the primary source of emergency response and.
Kazan Helicopters PJSC
Ground School 3.06 Weight & Balance.
Full Motion Video in ArcGIS
Conceptual Design Report
Conestoga Valley High School Aerospace Technology
SAE Heavy Lift Cargo Plane
THE OIL SEA HARVESTER SYSTEM :
Network for connecting robots, sensors, drones, unmanned surface
A Brief Introduction to Helicopters
Conestoga Valley High School Aerospace Technology
Drone And Drone Delivery
Dr. Victor M. Mwongera PhD in Aerospace Engineering
Helicopter Safety for SAR Operations
President of Eco-Trust Society
Extreme Altitude Mountain Rescue Vehicle
Presentation transcript:

Heavy Lift and Long Duration Co-axial Unmanned Aerial Vehicles Puma Aero Marine Heavy Lift and Long Duration Co-axial Unmanned Aerial Vehicles

HEAVY LIFT DRONE COAXIAL HELICOPTER: (VTOL-UAV) “The boss” HEAVY LIFT DRONE COAXIAL HELICOPTER: (VTOL-UAV)

BOSS VTOL-UAV Objectives: A rugged, stable, quiet, and cost effective all weather heavy lift platform to handle a wide variance of payloads. The Puma Aero Marine’s “BOSS” coaxial helicopter heavy lift drone (VTOL-UAV) is designed for both the public and private sectors. The “BOSS” can perform the following missions and many more: Heavy Exterior lifts (mobile sky crane loads to 1,206.3 kg./2,660 lbs./ 1.2 Metric Tons) Agricultural: aerial application using Variable Rate Technology Surveillance: Sea Hawk SHN-X9 Radar for detecting oil spills and/or surface ice Aerial firefighting: For rapid initial attack air tanker missions Search and Rescue Missions Airborne Laser Mine Detection System Seafood harvesting platform for side scan sonar devices to detect sea life

SURVEILANCE DRONE COAXIAL HELICOPTER: (VTOL-UAV) “The PUMA” SURVEILANCE DRONE COAXIAL HELICOPTER: (VTOL-UAV)

PUMA VTOL-UAV OBJECTIVES: A rugged, stable, quiet, and cost effective all weather surveillance platform designed primarily for the public sector. to handle a wide variance of payloads: A low cost VTOL-UAV platform with the capability of flying 68.1 kg. (150 lbs.) of surveillance equipment or other moderate weight sensors on eight (8) hour missions An inexpensive, reliable, environmentally friendly COAXIAL VTOL-UAV designed primarily for the public sector Easily operated by anyone with computer gaming skills, which receives its commands from a computer keyboard and override control by a fly by wire joystick. The operation could be from any operational base, dispatch center, mobile truck based unit, a vessel or carry around hand held unit Development of a model for use by private users such as Utilities/Farming/Forestry/Fishing and other industries requiring the use of aerial sensing systems.

Summary - Puma vtol-uav’s Puma Aero Marine of Florida and Bosonda International Ltd of California has developed an inexpensive, reliable, environmentally friendly line of COAXIAL VTOL-UAV (drone helicopter) platforms. The Puma VTOL-UAV’S are an inexpensive, reliable, and environmentally friendly line of COAXIAL VTOL-UAV (drone helicopter) platforms The heavy lift “BOSS” is designed for missions that require heavy lift capabilities. This can include missions that require large sensor packages, agricultural applications, sky crane lift duties, firefighting and search/rescue missions etc. The standard lift “PUMA” VTOL-UAV is designed primarily for missions requiring a moderate weigh sensor platform and extended duration flights Both Puma VTOL-UAV designs are complete and is now gearing up for dynamic endurance testing of a full scale transmission and rotor head with blades. The next stage is to build and complete test flying prototypes within three months after completion of the endurance testing. The prototypes and any initial production models will require approximately two months flight and support equipment evaluations.

Design Features - Coaxial VTOL-UAV   High Useful Load: The absence of a tail rotor in the Coaxial permits all of the engine power to be used by the rotor system for lifting purposes. Therefore, in comparison with a tail rotor configuration, the useful load of the Coaxial is higher. Multi-rotor configurations have substantially higher weight and higher transmission and shaft power losses than the Coaxial. The tandem configuration rotor system gives the Coaxial a useful load advantage over the tandem or any other multi-rotor configuration. Safe Deck and Ground Characteristics: In cross winds, on a rolling pitching and heaving ship’s deck, the handling of the Coaxial is much simpler than any other type, especially in takeoff and landings. Low Empty Weight: The feature that makes the fuselage independent of the lifting system dynamics permits the design of the fuselage to be strictly functional as related to mission requirements. This is the one feature that separates a Coaxial system from any other type.

Complete Symmetry of the Rotor System: The symmetry of the Coaxial Rotor System permits the same aerodynamic efficiency and controllability for flight in any direction; a feature only found in the Coaxial.   Simplified Rotor System: The Coaxial utilizes the semi-rigid type of rotor system without the need for the use of mechanical stabilizing devices, thus resulting in a simpler rotor system design and possessing excellent flying qualities. Freedom from Control Cross-Coupling: Control cross-coupling exists in all other rotor configurations, causing control complexity, dangerous flight attitudes, and vibration. Lack of control cross-coupling in the Coaxial yields multiple advantages in weight and performance compared to single rotor with a tail rotor and dual rotor systems.