Yeovil, United Kingdom
Yeovil, United Kingdom

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Global Military Helicopters market competition by top manufacturers, with production, price, revenue (value) and market share for each manufacturer; the top players including Geographically, this report is segmented into several key Regions, with production, consumption, revenue (million USD), market share and growth rate of Military Helicopters in these regions, from 2012 to 2022 (forecast), covering North America Europe China Japan Southeast Asia India On the basis of product, this report displays the production, revenue, price, market share and growth rate of each type, primarily split into Attack Helicopters Transport Helicopters Observation Helicopters Maritime Helicopters Multi-mission and Rescue Helicopters Training Helicopters On the basis on the end users/applications, this report focuses on the status and outlook for major applications/end users, consumption (sales), market share and growth rate of Military Helicopters for each application, including Fighting Transportion Detection Other Global Military Helicopters Market Research Report 2017 1 Military Helicopters Market Overview 1.1 Product Overview and Scope of Military Helicopters 1.2 Military Helicopters Segment by Type (Product Category) 1.2.1 Global Military Helicopters Production and CAGR (%) Comparison by Type (Product Category) (2012-2022) 1.2.2 Global Military Helicopters Production Market Share by Type (Product Category) in 2016 1.2.3 Attack Helicopters 1.2.4 Transport Helicopters 1.2.5 Observation Helicopters 1.2.6 Maritime Helicopters 1.2.7 Multi-mission and Rescue Helicopters 1.2.8 Training Helicopters 1.2.4 Type II 1.3 Global Military Helicopters Segment by Application 1.3.1 Military Helicopters Consumption (Sales) Comparison by Application (2012-2022) 1.3.2 Fighting 1.3.3 Transportion 1.3.4 Detection 1.3.5 Other 1.4 Global Military Helicopters Market by Region (2012-2022) 1.4.1 Global Military Helicopters Market Size (Value) and CAGR (%) Comparison by Region (2012-2022) 1.4.2 North America Status and Prospect (2012-2022) 1.4.3 Europe Status and Prospect (2012-2022) 1.4.4 China Status and Prospect (2012-2022) 1.4.5 Japan Status and Prospect (2012-2022) 1.4.6 Southeast Asia Status and Prospect (2012-2022) 1.4.7 India Status and Prospect (2012-2022) 1.5 Global Market Size (Value) of Military Helicopters (2012-2022) 1.5.1 Global Military Helicopters Revenue Status and Outlook (2012-2022) 1.5.2 Global Military Helicopters Capacity, Production Status and Outlook (2012-2022) 7 Global Military Helicopters Manufacturers Profiles/Analysis 7.1 Boeing 7.1.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.1.2 Military Helicopters Product Category, Application and Specification 7.1.2.1 Product A 7.1.2.2 Product B 7.1.3 Boeing Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.1.4 Main Business/Business Overview 7.2 Sikorsky Aircraft 7.2.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.2.2 Military Helicopters Product Category, Application and Specification 7.2.2.1 Product A 7.2.2.2 Product B 7.2.3 Sikorsky Aircraft Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.2.4 Main Business/Business Overview 7.3 AgustaWestland 7.3.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.3.2 Military Helicopters Product Category, Application and Specification 7.3.2.1 Product A 7.3.2.2 Product B 7.3.3 AgustaWestland Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.3.4 Main Business/Business Overview 7.4 Bell Helicopter 7.4.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.4.2 Military Helicopters Product Category, Application and Specification 7.4.2.1 Product A 7.4.2.2 Product B 7.4.3 Bell Helicopter Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.4.4 Main Business/Business Overview 7.5 Eurocopter 7.5.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.5.2 Military Helicopters Product Category, Application and Specification 7.5.2.1 Product A 7.5.2.2 Product B 7.5.3 Eurocopter Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.5.4 Main Business/Business Overview 7.6 Lockheed Corporation 7.6.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.6.2 Military Helicopters Product Category, Application and Specification 7.6.2.1 Product A 7.6.2.2 Product B 7.6.3 Lockheed Corporation Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.6.4 Main Business/Business Overview 7.7 Hindustan Aeronautics Limited (HAL) 7.7.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.7.2 Military Helicopters Product Category, Application and Specification 7.7.2.1 Product A 7.7.2.2 Product B 7.7.3 Hindustan Aeronautics Limited (HAL) Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.7.4 Main Business/Business Overview 7.8 Kamov Design Bureau 7.8.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.8.2 Military Helicopters Product Category, Application and Specification 7.8.2.1 Product A 7.8.2.2 Product B 7.8.3 Kamov Design Bureau Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.8.4 Main Business/Business Overview 7.9 Kawasaki Heavy Industries 7.9.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.9.2 Military Helicopters Product Category, Application and Specification 7.9.2.1 Product A 7.9.2.2 Product B 7.9.3 Kawasaki Heavy Industries Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.9.4 Main Business/Business Overview 7.10 Korea Aerospace Industries (KAI) 7.10.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.10.2 Military Helicopters Product Category, Application and Specification 7.10.2.1 Product A 7.10.2.2 Product B 7.10.3 Korea Aerospace Industries (KAI) Military Helicopters Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.10.4 Main Business/Business Overview 7.11 Mil Moscow Helicopter Plant 7.12 Mitsubishi Heavy Industries 7.13 NHIndustries (NHI) 7.14 Hughes Aircraft 7.15 Piasecki Helicopter For more information, please visit https://www.wiseguyreports.com/sample-request/1142899-global-military-helicopters-market-research-report-2017


Grant
Agency: European Commission | Branch: H2020 | Program: RIA | Phase: MG-1.1-2014 | Award Amount: 5.28M | Year: 2015

The European industry is currently a world leader in aviation and to maintain its leading position and competitiveness in the dynamic global market, Europes industry must develop quickly and efficiently high quality products by meeting time-critical market demands and customers needs. Industrial competition is becoming fiercer not only from established regions, such as the USA, but from new emerging challengers, such as Brazil, Canada, etc. Technological leadership and innovation is becoming the major competitive differentiator, most notably in terms of costs, and environmental performance. The market demands shorter cycles of new technology integration and, on the other hand, competitors enter the market with aggressive prices. It is forecasted that in 2050, innovative products and services demanded by the market will be based on state of the art design, manufacturing and certification processes with a significant reduction of the environmental impact. Recent studies have shown that the development and deployment of new structural technologies will have the greatest impact in the reduction of weight and operational costs compared to other technologies. Against this background, composite materials technology is of fundamental importance to current and future aircraft structures where high specific properties and integration of multiple functionalities are essential to improve weight, fuel efficiency, reduce CO2 emissions, and certification costs. The vulnerability of composite structures to localised, dynamic, sudden, and unexpected loads, may result in unpredictable complex localized damage and a loss of post-impact residual strength. The aim of the EXTREME project is to develop novel material characterisation methods and in-situ measurement techniques, material models and simulation methods for the design and manufacture aerospace composite structures under EXTREME dynamic loadings leading to a significant reduction of weight, design and certification cost.


Patent
AgustaWestland Ltd | Date: 2012-10-10

An aerofoil (12a, 12b, 12c, 12d) has a main portion of aerofoil cross section, an inner spanwise root end where the aerofoil is in use secured to a supporting structure, and at an outermost spanwise end outboard of the main portion, beyond a tip station, a tip region, and the tip region including a tip edge, the planform configuration of the tip edge lying on a first Bezier curve constructed from at least four control points P1, P2, P3 and P4, the control points P1, P2, P3 and P4 each lying on the periphery of a polygon which bounds the tip region, Bezier control point P1 being located on a leading edge of the aerofoil at the tip station, which is at a spanwise position between 93.5%R and 95.9%R, where first and second sides of the polygon meet, the first side being at the tip station extending perpendicularly to a blade reference axis, which extends spanwise of the main portion of the aerofoil, and the second side being a tangent to the leading edge of the aerofoil at control point P1, which extends between control point P1 to a position where the second side meets a third side of the boundary polygon at a position outwardly of the tip edge, the third side being parallel to the first side and extending between the position where the third side meets the second side, to where the third side and a fourth side meet, control point P2 being located on the second side at a position between 30% and 80% along the second side from P1, control point P3 being located on the third side at a position between 30% and 90% along the third side from where the second and third sides meet, and control point P4 being located at the outermost tip edge point at a trailing edge of the aerofoil, where R is the effective aerofoil span.


Patent
AgustaWestland Ltd | Date: 2014-03-26

A gearbox including a housing, an input member rotatably supported in the housing, a rotatable shaft supported in the housing, gearing providing a power transmitting connection between the input member and the rotatable shaft; and an oil feed member held against rotation relative to the housing, wherein the oil feed member has at least one helical formation for causing oil within the gearbox to be fed axially of the oil feed member, on rotation of the rotatable shaft.


A system for reducing the transmission of vibration from a first vibrating body to a second body, the system having a first part connected to the first vibrating body, a second part connected to the second body and an electro-hydrostatic actuator connected to the first and second parts, the electro-hydrostatic actuator being operable to continuously oscillate the first and second parts 10 relative to each other at a frequency substantially corresponding to the frequency of vibration of the first vibrating body.


Patent
AGUSTAWESTLAND Ltd | Date: 2012-02-16

A helicopter tail rotor gearbox including a housing, an output shaft for connection to a tail rotor rotatably supported in the housing and having an open end therein, an input member rotatably supported in the housing, gearing providing a power transmitting connection between the input member and output shaft, a pitch control shaft for effecting a change in the pitch of the tail rotor, the pitch control shaft being disposed at least partially within the output shaft, rotatable therewith, and movable relative thereto along the rotational axis of the output shaft, an actuating member for effecting axial movement of the pitch control shaft, the actuating member being movable axially of the output shaft but held against rotation therewith, and a bearing assembly positioned in between the pitch control shaft and the actuating member for permitting relative rotation therebetween, wherein the gearbox includes at least one formation for diverting oil, dispersed within the housing in use, towards the open end of the output shaft.


Patent
AGUSTAWESTLAND Ltd | Date: 2014-02-25

A device for holding a bearing member relative to a fixed body, including a first part having a formation for engagement with a corresponding formation on a fixed body to hold the first part relative to the fixed body, and a receiving formation for receiving and slidably supporting a generally elongate second part, wherein a first end of the second part is configured for engagement with a part of a bearing member to hold the bearing member relative to the fixed body, and wherein a second, opposite, end of the second part supports an abutment member which prevents the first and second parts separating from each other, wherein the device includes biasing means for biasing the first end of the second part away from the first part.


Patent
AgustaWestland Ltd | Date: 2013-08-16

A gearbox including a housing; an input member rotatably supported in the housing; a rotatable shaft supported in the housing; gearing providing a power transmitting connection between the input member and the rotatable shaft; and an oil feed member held against rotation relative to the housing; wherein the oil feed member has at least one helical formation for causing oil within the gearbox to be fed axially of the oil feed member, on rotation of the rotatable shaft.


Grant
Agency: GTR | Branch: Innovate UK | Program: | Phase: Collaborative Research & Development | Award Amount: 1.37M | Year: 2013

HiPerTilt led by AgustaWestland with the University of Liverpool and Bristol will develop world leading aerodynamic models, processes, techniques and new designs/products integral to the design and development of next generation tilt-rotorcraft in the UK. Tilt-rotorcraft offer the potential to revolutionise vertical lift passenger transport by delivering higher speeds, freeing up existing airport ‘regional aircraft’ capacity. These advances will deliver a game changing reduction in design time, an order of magnitude improvement within the UK.


Grant
Agency: GTR | Branch: Innovate UK | Program: | Phase: Business, Innovation & Skills Financed | Award Amount: 2.13M | Year: 2013

AgustaWestland is continuing research into helicopter active rotor technology; this will provide a step change in passenger ride comfort. With support from the Aerospace Growth Partnership (AGP), the Aerospace Technology Institute (ATI) and the Technology Strategy Board, AgustaWestland in Yeovil will carry out manufacture and test activities on an experimental active rotor system in preparation for flight test in 2014. The novel nature of the demonstrator system will require innovative new testing techniques to ensure the rotor can be flown safely. AgustaWestland will be supported extensively by the UK academic community and the aerospace supply chain.

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