Products & Services
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Supplier: SAE International
Description: limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A . Applications consider main rotor
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Supplier: SAE International
Description: text is limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A . Applications consider main
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Supplier: AgustaWestland
Description: The SW-4 is the light single-engine multi-mission helicopter, designed to operate in day and night VFR conditions; an excellent entry point to the light turbine helicopter segment for operational and training requirements. Operators benefit from modern technology, low operational cost
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Supplier: Airbus Group
Description: five blade main rotor allow greater lift and speed. With the shrouded Fenestron® tail rotor, the H155 benefits from a low sound signature and low maintenance. The shrouded rotor concept delivers additional control while increasing safety during ground operations,
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Supplier: Airbus Group
Description: The Tiger HAD is Airbus Helicopter's multi-role attack helicopter. It is designed to perform armed reconnaissance, air or ground escort, air-to-air combat, ground firing support, destruction and anti-tank warfare, day or night and in adverse conditions. The Tiger attack
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Supplier: AgustaWestland
Description: The unique characteristics of the AW609 TiltRotor combine the benefits of a helicopter and a fixed-wing aircraft into one aircraft. Taking off and landing vertically, flying above adverse weather conditions with up to nine people in comfort in a pressurised cabin at twice the speed and range
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Supplier: RedViking Group, LLC
Description: handle current and future requirements. With the ability to adapt to various rotor heads, blade connections and blade lengths, RedViking dynamic blade balance stands are capable of testing rotor blades from multiple aircraft and OEMs on a single tower.
- Display / User Interface: Application Software, Computer Interface
- Mechanical Test: Fatigue / Cyclic
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Description: 40 mil thick military grade polyurethane protective tape. Applications include advanced rotor blade protection on military helicopters. Tough thermoplastic polyurethane elastomer designed for extreme outdoor applications. Abrasion, erosion, scratch, puncture, and impact
- Width: 0.5 to 24 inches
- Thickness: 0.04 inches
- Features: Abrasion / Scratch Resistant, Protective Tape, Specialty / Other, UV / Weather Resistant
- Type: Non-adhesive
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Supplier: IHS ESDU
Description: measurement of loads taken at the position of maximum flapwise bending moment on the rotor. In the case of articulated rotors this has been found to be at approximately half rotor radius and on the lower surface of the blade. In the case of semi-rigid rotor it has
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Supplier: JTEKT North America, Inc.
Description: aircraft standard. Bearing for helicopter transmission Because the blade of the helicopter rotates at high speeds, the transmission supports a large load. We provide bearings compatible with under-race lubrication that enables operation for an extended period of time even after
- Application: Aerospace, Airframe / Aircraft Control
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Supplier: Plascore Incorporated
Description: composites Applications: PN2 aerospace honeycomb uses include aircraft galleys, flooring, partitions, aircraft leading and trailing edges, missile wings, radomes, antennas, military shelters, fuel tanks, helicopter rotor blades and navy bulkhead joiner panels. Availability: PN2
- Cell Size: 0.125 to 0.25 inch
- Compressive Strength: 54 to 2,145 psi
- Applications: Aerospace, Architectural / Construction, Automotive / Transportation, Industrial OEM, Marine, Structural Composites
- Core Material: Aramid Fiber (e.g., Nomex, Kevlar Fiber)
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Supplier: Boeing Company (The)
Description: over-the-horizon search, re-supply and retrograde, communications relay and surveillance capabilities. All with a low-risk approach, low operational costs and high flight readiness on a proven platform. Quick Facts Has 27.5-foot (8.38-meter) main rotor diameter with blade fold
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Supplier: Plascore Incorporated
Description: casings, fuel cells, fuselage components, helicopter rotor blades and navy bulkhead joiner panels. PAMG-XR1 5056 honeycomb is suitable for applications where materials conforming to AMS C7438 Rev A are required. Availability: PAMG-XR1 5056 aluminum honeycomb is available in four
- Cell Size: 0.125 to 0.375 inch
- Compressive Strength: 35 to 1,520 psi
- Applications: Aerospace, Architectural / Construction, Automotive / Transportation, Impact / Energy Absorption, Industrial OEM
- Core Material: Aluminum Alloy, Metal
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Supplier: Plascore Incorporated
Description: casings, fuel cells, fuselage components, helicopter rotor blades and navy bulkhead joiner panels, energy absorption, air/light directionalization and EMI/RFI shielding. PAMG-XR1 5052 honeycomb is suitable for applications where materials conforming to AMS C7438 Rev A are
- Width: 96 inches
- Length: 4 ft
- Application: Aerospace, Automotive, Building & Construction, Flooring Structure
- Features: Chemical / Corrosion Resistant
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Supplier: IHS ESDU
Description: contributions are further broken down, for the jet into jet mixing and shock noise and for the fan and compressor into blade passing frequency tones (including rotor-stator interaction effects), shaft-order tones and broad-band noise. Propeller and rotor noise are then
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Supplier: Plansee SE
Description: parts are exposed to and consequently increase their service life. Here are a few examples: Aviation and aerospace: propeller and helicopter blades Automotive industry: crankshaft counterweights and chassis weights Watch industry: bobs on watch rotors Sports equipment: golf
- Weight Type / Search Form: Balancing / Dynamic Balancing Weight, Counterweight / Counterbalance Weight
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When Leonardo sought a rapid, cost-efficient replacement for legacy rotor-blade restraint cradles on Royal Navy AW101 maritime helicopters, it turned to SFM Technology’s AeroAdditive team. Working on an accelerated schedule, SFM printed each cradle as two monolithic (read more)
Browse 3D Printers and Additive Manufacturing Machines Datasheets for BigRep -
mimic situations such as the air blast from helicopter rotor blades in a desert or an Arizona dust storm. MIL-STD environmental testing is performed inside our facility using 2 separate sand and dust chambers, and we also offer an outdoor setup for items as large as a pickup truck. The outdoor facility (read more)
Browse Environmental Exposure (Climatics) Testing Services Datasheets for E-Labs, Inc. -
Dexmet® Corporation, a part of PPG’s engineered materials division
MicroGrid Lightning Strike Material
Aircraft Lightning Strike Protection Our copper and aluminum MicroGrid® materials protect composite aircraft surfaces and rotor blades from lightning strikes. How Dexmet Lightning (read more)
Browse Lightning Protection Systems Datasheets for Dexmet® Corporation, a part of PPG’s engineered materials division -
Dexmet® Corporation, a part of PPG’s engineered materials division
Protecting Carbon Fiber Aircraft Surfaces
Aircraft Lightning Strike Protection Our copper and aluminum MicroGrid® materials protect composite aircraft surfaces and rotor blades from lightning strikes. How Dexmet (read more)
Browse Lightning Protection Systems Datasheets for Dexmet® Corporation, a part of PPG’s engineered materials division
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MAIN ROTOR STRAP INSPECTION SYSTEM
Critical surface inspection. under high magnification is. needed to assess the quality of. edge preparation of individual rotor. straps. These straps are later. stacked to make "strap packs",. whose function is to hold helicopter. rotor blades to their rotor heads. The carefully polished
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Advanced Defense Helicopter Interconnection Systems
Military helicopters are packing serious upgrades throughout their capabilities from new composite rotor blades and upgraded motor systems to utilizing the most recent sensors and electronics available in the industry. Higher speed rotor and altitude monitoring circuits smooth out rapid changes
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Structural Health Monitoring Using Genetic Fuzzy Systems
In this book, an alternative and powerful architecture, the genetic fuzzy system (GFS), is demonstrated for beams, composite tubes, and helicopter rotor blade health monitoring.
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Introduction to Radar Target Recognition
For a typical helicopter rotor blade the length is several metres, so it can be seen that the angular width over which the blade flash is near its peak is proportional to the wavelength.
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Journal of Aircraft > A Survey of Recent Developments in Rotorcraft Design Optimization
The use of composites in helicopter rotor blades is widespread, and optimization methods allow the tailoring of properties of com- posite cross sections for improved vibration, performance, and sta- bility characteristics.
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Basic Helicopter Aerodynamics 3rd Edition
A helicopter rotor blade performs the same function as a lifting wing but in a very different environment; and to note the similarities on the one hand and the distinctions on the other can be a considerable fillip to the learner’s interest …
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Failure Analysis of Engineering Structures: Methodology and Case Histories
The helicopter rotor blade failed by fatigue crack in the trailing edge center sheet, the crack originating at the bottom of a rivet hole.
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http://dspace.mit.edu/bitstream/handle/1721.1/9266/45613255-MIT.pdf?sequence=2
The actuator was developed in consideration of the requirements associated with the operation of a trailing edge servo-flap on a helicopter rotor blade .
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Journal of Aircraft > Recent Applications of Design Optimization to Rotorcraft-A Survey
With the partial ex- ception of hovering flight, the structural and aerodynamic problems of a helicopter rotor blade are intrinsically unsteady.
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Journal of Aircraft > Rotary Wing Aeroelasticity-A Historical Perspective
24Du Waldt, F. A., Gates, C. A., and Piziali, R. A., “Investiga- tion of Helicopter Rotor Blade Flutter and Flapwise Bending Re- sponse in Hovering,” Wright Air Development Center (WADC), Air Force Base, Wright–Patterson, Dayton, OH, Technical Rept.
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eScience on Distributed Computing Infrastructure
Aerodynamic and Aero-acoustic Analysis of Helicopter Rotor Blades in Hover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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Advanced In-Flight Measurement Techniques
Abstract For the design of a helicopter rotor blade , it is crucial to predict the dynamic behavior and occurring forces and moments.
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