Tokyo, Japan
Tokyo, Japan

Fuji Heavy Industries, Ltd. , or FHI, is a Japanese multinational corporation and conglomerate primarily involved in aerospace and ground transportation manufacturing, known for its line of Subaru automobiles. FHI's aerospace division serves as a defense contractor to the Japanese government, manufacturing Boeing and Lockheed Martin helicopters and airplanes under license along with being a global development and manufacturing partner to both companies.It traces its roots to the Nakajima Aircraft Company, a leading supplier of airplanes to the Japanese government during World War II. At the end of World War II, Nakajima was broken up by the Allied Occupation government, and by 1950 part of the separated operation was already known as Fuji Heavy Industries. FHI was incorporated on July 15, 1953 when five Japanese companies, known as Fuji Kogyo, Fuji Jidosha Kogyo, Omiya Fuji Kogyo, Utsunomiya Sharyo and Tokyo Fuji Sangyo, joined to form one of Japan's largest manufacturers of transportation equipment. Currently, FHI employs more than 15,000 people worldwide, operates nine manufacturing plants and sells products in 100 countries. It currently makes Subaru brand cars, and its aerospace division makes parts for Boeing, helicopters for the Japanese Self Defense Force, Raytheon Hawker, and Eclipse Aviation business jets. FHI is 16.16% owned by Toyota.In 2003, the company adopted the logo of its Subaru division as its worldwide corporate symbol.In June 2014, the company entered into a contract with Boeing, as one of five major Japanese companies contracted, to build parts for Boeing's 777X aircraft. Wikipedia.


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In this report, the global Aircraft Fairing market is valued at USD XX million in 2016 and is expected to reach USD XX million by the end of 2022, growing at a CAGR of XX% between 2016 and 2022. Geographically, this report is segmented into several key Regions, with production, consumption, revenue (million USD), market share and growth rate of Aircraft Fairing in these regions, from 2012 to 2022 (forecast), covering North America Europe China Japan Southeast Asia India For more information or any query mail at sales@wiseguyreports.com Global Aircraft Fairing market competition by top manufacturers, with production, price, revenue (value) and market share for each manufacturer; the top players including Alenia Aermacchi S.p.A. Avcorp Industries Inc. CTRM Aerocomposites Sdn Bhd. FACC AG Fuji Heavy Industries Ltd. Kaman Aerosystems Korean Air Aerospace Division Patria Aerostructures Oy PZL Swidnik S.A. ShinMaywa Industries Ltd. Strata Manufacturing PJSC Triumph Aerostructures UTC Aerosystems On the basis of product, this report displays the production, revenue, price, market share and growth rate of each type, primarily split into Composites Material Metal Material 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 Aircraft Fairing for each application, including Civil Aircraft Military Aircraft If you have any special requirements, please let us know and we will offer you the report as you want. Global Aircraft Fairing Market Research Report 2017 1 Aircraft Fairing Market Overview 1.1 Product Overview and Scope of Aircraft Fairing 1.2 Aircraft Fairing Segment by Type (Product Category) 1.2.1 Global Aircraft Fairing Production and CAGR (%) Comparison by Type (Product Category) (2012-2022) 1.2.2 Global Aircraft Fairing Production Market Share by Type (Product Category) in 2016 1.2.3 Composites Material 1.2.4 Metal Material 1.3 Global Aircraft Fairing Segment by Application 1.3.1 Aircraft Fairing Consumption (Sales) Comparison by Application (2012-2022) 1.3.2 Civil Aircraft 1.3.3 Military Aircraft 1.4 Global Aircraft Fairing Market by Region (2012-2022) 1.4.1 Global Aircraft Fairing 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 Aircraft Fairing (2012-2022) 1.5.1 Global Aircraft Fairing Revenue Status and Outlook (2012-2022) 1.5.2 Global Aircraft Fairing Capacity, Production Status and Outlook (2012-2022) 2 Global Aircraft Fairing Market Competition by Manufacturers 2.1 Global Aircraft Fairing Capacity, Production and Share by Manufacturers (2012-2017) 2.1.1 Global Aircraft Fairing Capacity and Share by Manufacturers (2012-2017) 2.1.2 Global Aircraft Fairing Production and Share by Manufacturers (2012-2017) 2.2 Global Aircraft Fairing Revenue and Share by Manufacturers (2012-2017) 2.3 Global Aircraft Fairing Average Price by Manufacturers (2012-2017) 2.4 Manufacturers Aircraft Fairing Manufacturing Base Distribution, Sales Area and Product Type 2.5 Aircraft Fairing Market Competitive Situation and Trends 2.5.1 Aircraft Fairing Market Concentration Rate 2.5.2 Aircraft Fairing Market Share of Top 3 and Top 5 Manufacturers 2.5.3 Mergers & Acquisitions, Expansion 7 Global Aircraft Fairing Manufacturers Profiles/Analysis 7.1 Alenia Aermacchi S.p.A. 7.1.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.1.2 Aircraft Fairing Product Category, Application and Specification 7.1.2.1 Product A 7.1.2.2 Product B 7.1.3 Alenia Aermacchi S.p.A. Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.1.4 Main Business/Business Overview 7.2 Avcorp Industries Inc. 7.2.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.2.2 Aircraft Fairing Product Category, Application and Specification 7.2.2.1 Product A 7.2.2.2 Product B 7.2.3 Avcorp Industries Inc. Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.2.4 Main Business/Business Overview 7.3 CTRM Aerocomposites Sdn Bhd. 7.3.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.3.2 Aircraft Fairing Product Category, Application and Specification 7.3.2.1 Product A 7.3.2.2 Product B 7.3.3 CTRM Aerocomposites Sdn Bhd. Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.3.4 Main Business/Business Overview 7.4 FACC AG 7.4.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.4.2 Aircraft Fairing Product Category, Application and Specification 7.4.2.1 Product A 7.4.2.2 Product B 7.4.3 FACC AG Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.4.4 Main Business/Business Overview 7.5 Fuji Heavy Industries Ltd. 7.5.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.5.2 Aircraft Fairing Product Category, Application and Specification 7.5.2.1 Product A 7.5.2.2 Product B 7.5.3 Fuji Heavy Industries Ltd. Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.5.4 Main Business/Business Overview 7.6 Kaman Aerosystems 7.6.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.6.2 Aircraft Fairing Product Category, Application and Specification 7.6.2.1 Product A 7.6.2.2 Product B 7.6.3 Kaman Aerosystems Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.6.4 Main Business/Business Overview 7.7 Korean Air Aerospace Division 7.7.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.7.2 Aircraft Fairing Product Category, Application and Specification 7.7.2.1 Product A 7.7.2.2 Product B 7.7.3 Korean Air Aerospace Division Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.7.4 Main Business/Business Overview 7.8 Patria Aerostructures Oy 7.8.1 Company Basic Information, Manufacturing Base, Sales Area and Its Competitors 7.8.2 Aircraft Fairing Product Category, Application and Specification 7.8.2.1 Product A 7.8.2.2 Product B 7.8.3 Patria Aerostructures Oy Aircraft Fairing Capacity, Production, Revenue, Price and Gross Margin (2012-2017) 7.8.4 Main Business/Business Overview For more information or any query mail at sales@wiseguyreports.com ABOUT US: Wise Guy Reports is part of the Wise Guy Consultants Pvt. Ltd. and offers premium progressive statistical surveying, market research reports, analysis & forecast data for industries and governments around the globe. Wise Guy Reports features an exhaustive list of market research reports from hundreds of publishers worldwide. We boast a database spanning virtually every market category and an even more comprehensive collection of rmaket research reports under these categories and sub-categories. For more information, please visit https://www.wiseguyreports.com


Patent
Fuji Heavy Industries and Kyb Corporation | Date: 2014-06-04

An electric power steering device includes a basic return command value calculation unit configured to calculate a basic return command value in a direction returning the steering wheel to a neutral position, on the basis of detection results of a steering angle detector detecting a steering angle of the steering wheel, a first correction gain calculation unit configured to calculate a first correction gain correcting the basic return command value, on the basis of detection results of a vehicle speed detector detecting vehicle speed, and a second correction gain calculation unit configured to calculate a second correction gain correcting the basic return command value, on the basis of a change amount of the steering torque detected by the torque sensor. The basic return command value is corrected by the first and second correction gains so as to calculate a return command value. The return command value is added to the assist command value so as to drive the electric motor.


Patent
Kyb Corporation and Fuji Heavy Industries | Date: 2016-04-20

An electric power steering device includes a basic return command value calculation unit configured to calculate a basic return command value in a direction returning the steering wheel to a neutral position, on the basis of detection results of a steering angle detector detecting a steering angle of the steering wheel, a first correction gain calculation unit configured to calculate a first correction gain correcting the basic return command value, on the basis of detection results of a vehicle speed detector detecting vehicle speed, and a second correction gain calculation unit configured to calculate a second correction gain correcting the basic return command value, on the basis of a change amount of the steering torque detected by the torque sensor. The basic return command value is corrected by the first and second correction gains so as to calculate a return command value. The return command value is added to the assist command value so as to drive the electric motor.


Patent
Fuji Heavy Industries and Takata Corporation | Date: 2015-02-03

An airbag unit is provided that can be quickly unfolded, and also retrofitted to an existing vehicle body. The airbag unit includes an airbag that covers, upon being unfolded, at least a part of a hood or a windshield outside a vehicle, a gas generator that ejects gas into the airbag, a cover bottom member that accommodates therein the airbag yet to be expanded and the gas generator, a cover lid member including a cover lid plate that covers the cover bottom member in which the airbag is accommodated, and a cowl cover attached to the cover lid plate between the hood and the windshield.


Patent
Fuji Heavy Industries and Takata Corporation | Date: 2015-02-03

An airbag unit is provided that can be easily installed and removed. The airbag unit includes an airbag that covers, upon being unfolded, at least a part of a hood or a windshield outside a vehicle, a gas generator that ejects gas into the airbag, a cover bottom member that accommodates therein the airbag yet to be expanded and the gas generator, a cover lid member that covers the cover bottom member in which the airbag is accommodated, and a bracket removably supported by the body of the vehicle, and removably supporting the cover bottom member and the cover lid member.


Grant
Agency: European Commission | Branch: FP7 | Program: CP-FP | Phase: AAT.2012.3.3-6. | Award Amount: 1.81M | Year: 2012

JEDI ACE aims to provide an innovative concept of an integrated ice protection system: an inte-grated approach, consisting of combined passive anti-icing coating, active de-icing devices and ice sensors. The system will be applicable to aircraft wings and will support an important technological milestone: the composite wing concept, which today includes also morphing properties. The JEDI ACE consortium, consisting of European and Japanese partners, determined three technical objectives for the integrated ice protection system: 1. An active de-icing device based on electro-thermal and/or mechanical actuation, combined with supporting passive anti-icing coatings 2. An ice sensor system for real-time measurements of ice accretion on aircraft structures, 3. An integrated ice protection system with complementary components for excellent operation properties. The work in JEDI ACE will result in validated design concepts and lab-scale prototypes for the future generation of integrated ice protection systems. The design will contribute to: prevention of ice buildup on leading edges, improved in-flight ice assessment, improved aircraft safety reduced energy consumption during de-icing procedures, reduced de-icing procedures on ground, compliance with design constraints of composite wings including morphing properties, compliance with bleed-air free engines and all-electric aircrafts, compliance with other surface and coating requirements like resistance against erosion The JEDI ACE consortium will develop evaluation devices for all determined objectives on the basis of newest scientific knowledge, combined with appropriate test sessions to validate the performance of the components and deliver the design concept of an integrated ice protection system. This ambitious goal will be achieved by combining the specific SoA competencies through close multinational collaboration.


Patent
Hitachi Ltd. and Fuji Heavy Industries | Date: 2012-03-07

A downwind type wind turbine having a transformer (5, 25) stored in a support post (4) or in a nacelle (3, 23) includes the nacelle (3, 23) which supports a rotor (1) and stores therein a generator (9), a support post (4) which supports the nacelle (3, 23) and a main transformer (5, 25) disposed between the generator (9) and an electric power system (8) and the main transformer (5, 25) is stored in the nacelle (3, 23) or in the support post (4).


Patent
Keihin Corporation and Fuji Heavy Industries | Date: 2014-05-29

A hydraulic pressure control apparatus includes a first pressure regulating valve for reducing an initial oil pressure (line pressure) of a working oil, a solenoid-operated valve for converting the oil pressure, which has been reduced in pressure, into a solenoid pressure, and a second pressure regulating valve for converting the line pressure of the working oil into an actuating pressure responsive to the solenoid pressure. The three valves share a single body. Further, an outlet passageway is formed along a thicknesswise direction of the body, with a relief valve being formed upwardly of the outlet passageway.


Patent
Keihin Corporation and Fuji Heavy Industries | Date: 2016-10-06

A hydraulic pressure control apparatus includes a first pressure regulating valve for reducing an initial oil pressure (line pressure) of a working oil, a solenoid-operated valve for converting the oil pressure, which has been reduced in pressure, into a solenoid pressure, and a second pressure regulating valve for converting the line pressure of the working oil into an actuating pressure responsive to the solenoid pressure. The three valves share a single body. Further, an outlet passageway is formed along a thicknesswise direction of the body, with a relief valve being formed upwardly of the outlet passageway.


Patent
Fuji Heavy Industries | Date: 2014-06-24

[Object] To provide a shift control device that, in a shift control device of a vehicle equipped with an idling-stop mechanism and a shift-by-wire mechanism, is capable of preventing setting off at a timing that the driver does not expect when returning from an idling-stop state. [Solution] The SBW-CU (40) that constitutes the shift control device (1), in the case of selection information for selecting the R range being output during an idling stop, switches the shift range of the automatic transmission (10) to the R range when the vehicle is braked, and switches the shift range to the N range or the P range when the vehicle is not braked and the shift range of the automatic transmission (10) is the D range. Also, the SBW-CU (40), in the case of selection information for selecting the R range being output during an idling stop, maintains the shift range without switching it when the vehicle is braked and the shift range of the automatic transmission (10) is other than the D range.

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