The Rotating Wing Aircraft Meetings of 1938 and 1939 Were the First
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1.1.3 Helicopters
Information on the Company’s Activities / 1.1 Presentation of the Company 1.1.3 Helicopters Airbus Helicopters is a global leader in the civil and military The HIL programme, for which the Airbus Helicopters’ H160 rotorcraft market, offering one of the most complete and modern was selected in 2017, was initially scheduled for launch range of helicopters and related services. This product range in 2022 by the current military budget law. Launching the currently includes light single-engine, light twin-engine, medium programme earlier will enable delivery of the fi rst H160Ms to and medium-heavy rotorcraft, which are adaptable to all kinds of the French Armed Forces to be advanced to 2026. The H160 mission types based on customer needs. See “— 1.1.1 Overview” was designed to be a modular helicopter, enabling its military for an introduction to Airbus Helicopters. version, with a single platform, to perform missions ranging from commando infi ltration to air intercept, fi re support, and anti-ship warfare in order to meet the needs of the army, the Strategy navy and the air force through the HIL programme. The new fi ve-bladed H145 is on track for EASA and FAA Business Ambition certifi cation in 2020. To ensure these certifi cations, two fi ve- bladed prototypes have clocked more than 400 fl ight hours Airbus Helicopters continues to execute its ambition to lead the in extensive fl ight test campaigns in Germany, France, Spain, helicopter market, build end-to-end solutions and grow new Finland, and in South America. First deliveries of the new H145 VTOL businesses, while being fi nancially sound. -
United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021
UN Military Aviation Unit Manual United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021 Second Edition 2019 DEPARTMENT OF PEACE OPERATIONS DEPARTMENT OF OPERATIONAL SUPPORT UN Military Aviation Unit Manual Produced by: Office of Military Affairs, Department of Peace Operations UN Secretariat One UN Plaza, New York, NY 10017 Tel. 917-367-2487 Approved by: Jean-Pierre Lacroix, Under-Secretary-General for Peace Operations Department of Peace Operations (DPO). Atul Khare Under-Secretary-General for Operational Support Department of Operational Support (DOS) April 2021. Contact: PDT/OMA/DPO Review date: 30/ 04 / 2026 Reference number: 2021.04 Printed at the UN, New York © UN 2021. This publication enjoys copyright under Protocol 2 of the Universal Copyright Convention. Nevertheless, governmental authorities or Member States may freely photocopy any part of this publication for exclusive use within their training institutes. However, no portion of this publication may be reproduced for sale or mass publication without the express consent, in writing, of the Office of Military Affairs, UN Department of Peace Operations. ii UN Military Aviation Unit Manual Foreword We are delighted to introduce the United Nations Peacekeeping Missions Military Aviation Unit Manual, an essential guide for commanders and staff deployed in peacekeeping operations, and an important reference for Member States and the staff at United Nations Headquarters. For several decades, United Nations peacekeeping has evolved significantly in its complexity. The spectrum of multi-dimensional UN peacekeeping operations includes challenging tasks such as restoring state authority, protecting civilians and disarming, demobilizing and reintegrating ex-combatants. In today’s context, peacekeeping missions are deploying into environments where they can expect to confront asymmetric threats and contend with armed groups over large swaths of territory. -
Global Military Helicopters 2015-16 Market Report Contents
GLOBAL MILITARY HELICOPTERS 2015-16 MARKET REPORT CONTENTS MARKET OVERVIEW 2 MILITARY HELICOPTER KEY REQUIREMENTS 4 EUROPE 5 NORTH AMERICA 10 LATIN AMERICA & THE CARIBBEAN 12 AFRICA 15 ASIA-PACIFIC 16 MIDDLE EAST 21 WORLD MILITARY HELICOPTER HOLDINGS 23 EUROPE 24 NORTH AMERICA 34 LATIN AMERICA & THE CARIBBEAN 36 AFRICA 43 ASIA-PACIFIC 49 MIDDLE EAST 59 EVENT INFORMATION 65 Please note that all information herein is subject to change. Defence IQ endeavours to ensure accuracy wherever possible, but errors are often unavoidable. We encourage readers to contact us if they note any need for amendments or updates. We accept no responsibility for the use or application of this information. We suggest that readers contact the specific government and military programme offices if seeking to confirm the reliability of any data. 1 MARKET OVERVIEW Broadly speaking, the global helicopter market is currently facing a two- pronged assault. The military helicopter segment has been impacted significantly by continued defense budgetary pressures across most traditional markets, and a recent slide in global crude oil prices has impacted the demand for new civil helicopters as well as the level of activity for existing fleets engaged in the offshore oil & gas exploration sector. This situation has impacted industry OEMs significantly, many of which had been working towards strengthening the civil helicopter segment to partially offset the impact of budgetary cuts on the military segment. However, the medium- to long-term view of the market is promising given the presence of strong fundamentals and persistent, sustainable growth drivers. The market for military helicopters in particular is set to cross a technological threshold in the form of next-generation compound helicopters and tilt rotorcraft. -
Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks
Purdue University Purdue e-Pubs Department of Electrical and Computer Department of Electrical and Computer Engineering Technical Reports Engineering August 1991 Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks Tobias J. Pallett Purdue University School of Electrical Engineering Shaheen Ahmad Purdue University School of Electrical Engineering Follow this and additional works at: https://docs.lib.purdue.edu/ecetr Pallett, Tobias J. and Ahmad, Shaheen, "Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks" (1991). Department of Electrical and Computer Engineering Technical Reports. Paper 317. https://docs.lib.purdue.edu/ecetr/317 This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact [email protected] for additional information. Real-Time Helicopter Flight Control: Modelling and Control by Linearization and Neural Networks Tobias J. Pallett Shaheen Ahmad TR-EE 91-35 August 1991 Real-Time Helicopter Flight Control: Modelling and Control by Lineal-ization and Neural Networks Tobias J. Pallett and Shaheen Ahmad Real-Time Robot Control Laboratory, School of Electrical Engineering, Purdue University West Lafayette, IN 47907 USA ABSTRACT In this report we determine the dynamic model of a miniature helicopter in hovering flight. Identification procedures for the nonlinear terms are also described. The model is then used to design several linearized control laws and a neural network controller. The controllers were then flight tested on a miniature helicopter flight control test bed the details of which are also presented in this report. Experimental performance of the linearized and neural network controllers are discussed. -
Helicopter Physics by Harm Frederik Althuisius López
Helicopter Physics By Harm Frederik Althuisius López Lift Happens Lift Formula Torque % & Lift is a mechanical aerodynamic force produced by the Lift is calculated using the following formula: 2 = *4 '56 Torque is a measure of how much a force acting on an motion of an aircraft through the air, it generally opposes & object causes that object to rotate. As the blades of a Where * is the air density, 4 is the velocity, '5 is the lift coefficient and 6 is gravity as a means to fly. Lift is generated mainly by the the surface area of the wing. Even though most of these components are helicopter rotate against the air, the air pushes back on the rd wings due to their shape. An Airfoil is a cross-section of a relatively easy to measure, the lift coefficient is highly dependable on the blades following Newtons 3 Law of Motion: “To every wing, it is a streamlined shape that is capable of generating shape of the airfoil. Therefore it is usually calculated through the angle of action there is an equal and opposite reaction”. This significantly more lift than drag. Drag is the air resistance attack of a specific airfoil as portrayed in charts much like the following: reaction force is translated into the fuselage of the acting as a force opposing the motion of the aircraft. helicopter via torque, and can be measured for individual % & -/ 0 blades as follows: ! = #$ = '()*+ ∫ # 1# , where $ is the & -. Drag Force. As a result the fuselage tends to rotate in the Example of a Lift opposite direction of its main rotor spin. -
Helicopter Flying Handbook (FAA-H-8083-21B) Chapter 8
Chapter 8 Ground Procedures and Flight Preparations Introduction Once a pilot takes off, it is up to him or her to make sound, safe decisions throughout the flight. It is equally important for the pilot to use the same diligence when conducting a preflight inspection, making maintenance decisions, refueling, and conducting ground operations. This chapter discusses the responsibility of the pilot regarding ground safety in and around the helicopter and when preparing to fly. 8-1 Preflight There are two primary methods of deferring maintenance on rotorcraft operating under part 91. They are the deferral Before any flight, ensure the helicopter is airworthy by provision of 14 CFR part 91, section 91.213(d) and an FAA- inspecting it according to the rotorcraft flight manual (RFM), approved MEL. pilot’s operating handbook (POH), or other information supplied either by the operator or the manufacturer. The deferral provision of 14 CFR section 91.213(d) is Remember that it is the responsibility of the pilot in command widely used by most pilot/operators. Its popularity is due (PIC) to ensure the aircraft is in an airworthy condition. to simplicity and minimal paperwork. When inoperative equipment is found during preflight or prior to departure, the In preparation for flight, the use of a checklist is important decision should be to cancel the flight, obtain maintenance so that no item is overlooked. [Figure 8-1] Follow the prior to flight, determine if the flight can be made under the manufacturer’s suggested outline for both the inside and limitations imposed by the defective equipment, or to defer outside inspection. -
Paper Helicopters Preparation
Paper Helicopters Preparation CLASS LEVEL First – sixth class OBJECTIVES Content Strand and Strand Unit Energy & forces, Forces Through investigation the child should be enabled to come to appreciate that gravity is a force, SESE: Science Curriculum page 87. In this activity children explore how some things fall and how varying the size of the rotor blades, the shape of the rotor blades and the weight of a paper helicopter affect the way a helicopter spins. Skill development Through completing the strand units of the science curriculum the child should be enabled to design, plan and carry out simple experiments, having regard to one or two variables and the need to sequence tasks and tests, SESE: Science Curriculum page 79. This activity helps them understand fair testing by changing only one variable (i.e. shape only or length only) at a time. Investigating; experimenting; observing; analysing; measuring/timing; recording and communicating. CURRICULUM LINKS Mathematics Data / representing and interpreting data SESE: History Continuity and change over time/ technological and scientific developments over long periods BACKGROUND A previous activity on how things fall (i.e. the weight of the object is not a factor – Galileo and the Leaning Tower of Pisa) would help understanding of this activity, but not essential. MATERIALS/EQUIPMENT Paper, Ruler, Paper Clips, Scissors Templates of different sizes PREPARATION Test out a few thicknesses of paper/cardboard first to see that some of them spin. BACKGROUND The shape of the helicopter rotor blades make it spin INFORMATION when dropped from a height. Gravity pulls the helicopter down. The air resists the movement and pushes up each rotor separately, causing the helicopter to spin. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883
Journal of Aviation/Aerospace Education & Research Volume 13 Number 1 JAAER Fall 2003 Article 1 Fall 2003 Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883 Thomas Forenz Follow this and additional works at: https://commons.erau.edu/jaaer Scholarly Commons Citation Forenz, T. (2003). Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883. Journal of Aviation/Aerospace Education & Research, 13(1). https://doi.org/10.15394/ jaaer.2003.1559 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Forenz: Assessing the Evolution of the Airborne Generation of Thermal Lif Thermal Lift ASSESSING THE EVOLUTION OF THE AIRBORNE GENERATION OF THERMAL LIFT IN AEROSTATS 1783 TO 1883 Thomas Forenz ABSTRACT Lift has been generated thermally in aerostats for 219 years making this the most enduring form of lift generation in lighter-than-air aviation. In the United States over 3000 thermally lifted aerostats, commonly referred to as hot air balloons, were built and flown by an estimated 12,000 licensed balloon pilots in the last decade. The evolution of controlling fire in hot air balloons during the first century of ballooning is the subject of this article. The purpose of this assessment is to separate the development of thermally lifted aerostats from the general history of aerostatics which includes all gas balloons such as hydrogen and helium lifted balloons as well as thermally lifted balloons. -
Helicopter and Tiltrotor Noise Modeling Procedures Document
ACRP Problem Statement: 89 Recommended Allocation: $250,000 Helicopter and Tiltrotor Noise Modeling Procedures Document Click here to see problem statement in IdeaHub: http://ideascale.com/t/UKsrZBVBS (Note: you must be a registered user in myACRP/IdeaHub.) TAGS: Airport Planning, Environment, Noise Impacts, Operations, Policy, Public Relations STAFF COMMENTS No comments. AVERAGE INDUSTRY RATING SUMMARY Committees1 Airport Community2 Achievable 3.00 3.50 Applicable 2.50 3.50 Implementable 2.00 3.50 Understandable 2.50 3.00 OVERALL 2.50 3.38 Notes: 1. Includes TRB aviation committees and committees from ACI-NA and AAAE. 2. Includes airport employees serving on active ACRP project panels. CLICK HERE TO SEE DETAILED INDUSTRY RATINGS CLICK HERE TO SEE DETAILED INDUSTRY COMMENTS ACRP OVERSIGHT COMMITTEE (AOC) DISPOSITION The average AOC rating among its voting members was 2.1 on a scale of 1 to 5. There was on discussion. The problem statement was not selected for ACRP funding and will be returned to the idea collection phase of ACRP’s IdeaHub. ACRP Problem Statement: 89 Helicopter and Tiltrotor Noise Modeling Procedures Document TAGS: Airport Planning, Environment, Noise Impacts, Operations, Policy, Public Relations OBJECTIVE The objective of this research effort is to develop written documentation on best available methods to model community noise generated from helicopter and tiltrotor operations. The document should address integrated and simulation modeling techniques, and methods for collecting and analyzing noise source data, and outline noise source development protocols. The language and format of the document shall be suitable for standards submission. BACKGROUND Existing noise modeling standards [SAE-AIR-1845; ICAO, Doc-29] for prediction of fixed wing community noise have been promulgated internationally and serve as the technical justification and defensible rationale upon which numerous noise models such as the Aviation Environmental Design Tool (AEDT) and the Integrated Noise Model (INM) rely. -
Military Use Handbook
National Interagency Fire Center Military Use Handbook 2021 This publication was produced by the National Interagency Coordination Center (NICC), located at the National Interagency Fire Center (NIFC), Boise, Idaho. This publication is also available on the Internet at http://www.nifc.gov/nicc/logistics/references.htm. MILITARY USE HANDBOOK 2021 INTRODUCTION ................................................................................................. ………………… ..................................................................................................................................................... CHAPTER 10 – GENERAL ........................................................................................................ 1 10.1 Purpose ............................................................................................................... 1 10.2 Overview .............................................................................................................. 1 10.3 Ordering Requirements and Procedures .............................................................. 1 10.4 Authorities/Responsibilities .................................................................................. 2 10.5 Billing Procedures ................................................................................................ 3 CHAPTER 20 – RESOURCE ORDERING PROCEDURES FOR MILITARY ASSETS ............... 4 20.1 Ordering Process ................................................................................................. 4 20.2 Demobilization -
1 American Institute of Aeronautics and Astronautics EXTENDED
EXTENDED CAPABILITIES OF ZERO-PRESSURE AND SUPERPRESSURE SCIENTIFIC BALLOONING PLATFORMS E. Lee Rainwater*, Raven Industries, Inc., Sulphur Springs, Texas USA Debora A. Fairbrother†, NASA Wallops Flight Facility, Wallops Island, Virginia USA Michael S. Smith‡, Raven Industries, Inc., Sulphur Springs, Texas USA ABSTRACT Updated Heavy Lift Designs Balloons with maximum payloads of up to 3625 kg The 1.7 million cubic meter (60 million cubic foot) (8000 lb) have been available for many years. However, scientific balloon platform, designed and manufactured the reliability of such balloons is compromised when by Raven Industries, Inc. and funded by NASA, has flown at the maximum payload. Raven Industries, in successfully flown a payload of 680 kg (1500 lb) to a cooperation with NASA and the National Scientific float altitude of over 48.7 km (160 kft). This record- Balloon Facility (NSBF), has developed a new 1 MCM breaking flight, performed in August, 2002, greatly (36.7 MCF) heavy-load balloon design which utilizes extended the performance envelope of scientific bal- three-layer co-extruded film technologies developed for looning platforms with regard to its ability to lift sig- the ULDB program. This balloon promises to utilize the nificant payloads to extreme altitudes. This has, in turn, full gross inflation capacity of NSBF’s launch equip- generated significant interest from the scientific com- ment, while delivering the near-100% reliability associ- munity regarding the increased altitude and duration ated with existing medium-capacity balloons. capabilities of scientific ballooning platforms. Zero-pressure Ultra-high Altitude Balloons (UHABs) In order to explore future capabilities and establish a ULDB film technology also found practical application future direction for ultra high-altitude platforms, NASA 1 and Raven have partnered in a study to determine the in the 60 MCF “Big 60” balloon .