Bell 505

March 2, 2014 by Tim McAdams

Heli-Expo 2014, held last week in AnaheimCalifornia, is the annual worldwide helicopter convention. At the show, Bell Helicopter announced the Bell 505 JetRanger X. The latest generation of the JetRanger series that started 50 years ago. Scheduled for its first flight later this year, the company has started signing letters of intent. The new model is aimed at a wide variety of missions, including utility, corporate, private owners and training schools.

Based on the original Bell 206B, the Bell 505 JetRanger X is a five-seat, single-engine turbine helicopter with a cruise speed of 125 knots, range of 360 nautical miles and a useful load of 1,500 pounds. The fuselage has been updated to provide a sleek modern look that features increased cabin volume and side clam shell doors. The cockpit improvements include the Garmin G1000H Integrated Avionics Suite and wrap-around windscreens providing a wide field of view. The engine has been changed to the 504 shp Turbomeca Arrius 2R engine with dual channel Full Authority Digital Engine Control (FADEC), an engine data recorder and a 3000 hour TBO. The rotor system retains the two-bladed, high inertia system that gave the JetRanger its reputation for excellent autorotation capabilities.

Bell Helicopter has also announced it will build the helicopter at a newly constructed assembly facility at the Lafayette Regional Airport in Louisiana.  Also new is a website (www.bell505.com) where customers can custom build and order the helicopter online.

505

505a

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Mast moment

February 17, 2014 by Tim McAdams

A rigid (or sometimes called hinge-less) rotor system is capable of transmitting high bending forces to the main rotor shaft. When a pilot makes a cyclic movement causing the main rotor disc to tilt, the fuselage wants to follow. In flight, with a rigid rotor the mast bending moment is low. However, when the fuselage is in contact with the ground and cannot follow the main rotor disc the bending moment can be very high. 

This type of rotor system is used on the helicopters designed and built by the German manufacturer MBB (now Airbus Helicopters). Because large cyclic displacements on the ground have the potential to damage the mast assembly, a mast moment indicator (MMI) is installed. The gauge is a single dimension indicator that shows the total moment being applied to the mast. When the gauge reads high, the pilot has to figure out what direction to move the cyclic to reduce the mast moment. Over time, experience makes knowing how to keep the mast moment low a natural reaction, however, pilots new to these types of helicopters would have to be very careful not to exceed the limit. Recently, to help reduce any possible confusion a new style gauge has been developed. It is two dimensional (using a circle instead of a straight line) which makes knowing the correct direction to move the cyclic control easier. 

Normal pick-ups and set-downs require care as to not exceed the limits on the MMI. Generally, this is not difficult. However, slope landings and running landings can be more challenging. In these situations, the pilot needs to be comfortable with the MMI being close to limits and making very small cyclic adjustments. If a limit is exceeded, the amount (in percentage) and duration dictate how extensive an inspection or repair will be.

Older style MMI

Older style MMI

                   

Newer electronic single dimension MMI

Newer electronic single dimension MMI

 

 

 

 

Latest two dimension MMI

Latest two dimension MMI

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Teaching autorotations

February 1, 2014 by Tim McAdams

One of the most critical maneuvers that helicopter CFIs perform with their students is autorotations. It requires precision, timing and the ability to multitask.  Rotor RPM, airspeed and trim must all be maintained within allowed parameters while simultaneously finding a suitable landing area and maneuvering the helicopter into the wind. From 500 feet above ground level, a student has 20 to 30 seconds to process and manage all the factors and make the right decisions to achieve a successful outcome.

Allowing a student to perform an autorotation requires constant vigilance from the instructor. The best way for students to learn is by doing as much of the maneuver as possible, however, the instructor does not always have a lot of time to decide to take the controls before the student gets the helicopter in an unrecoverable situation. Sometimes, the difference between a successful practice autorotation and an accident is just a second or two.

During the first 2 months of 2012 three accidents happened from practice autorotations and the NTSB issued the following probable causes:

  • The flight instructor’s delayed remedial action during the pilot-receiving-instruction’s practice autorotation that developed a high rate of descent. Contributing to the accident was the pilot-receiving-instruction’s improper control inputs during the practice autorotation. 
  • The flight instructor’s failure to apply power during a practice autorotation in order to arrest a high rate of descent, which resulted in an in-flight collision with terrain. 

These two happened in a Robinson R22 and a R44. However, the following is from an AS350 with a more experienced instructor. 

  • The flight instructor’s improper use of the collective control during a practice hovering autorotation, which resulted in a hard landing.

Even an excellent and experienced instructor who gets distracted, even for just a second or less, can damage an aircraft. Full touchdown autorotations (that is, not bringing the engine back in before ground contact) add another level of risk. Fortunately, most accidents that happen from practice autorotations are not fatal.

 

NTSB accident references:

NTSB Identification: WPR12TA120

NTSB Identification: ERA12CA179

NTSB Identification: ERA12CA137

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NTSB top 10

January 19, 2014 by Tim McAdams

On January 16, 2014 the National Transportation Safety Board released its 2014 Most Wanted List, the top 10 advocacy and awareness priorities for the agency for the year. With the high accident rate in the helicopter industry, helicopter operations have been added to the list. According to the NTSB, between January 2003 and May 2013, 1,470 helicopter accidents have occurred, with 477 fatalities and 274 serious injuries.

The NTSB understands that helicopters are used for a range of operations, each of which presents unique challenges. For example, helicopter emergency medical services (HEMS) operators transport seriously ill patients and donor organs to emergency care facilities, often creating pressure to conduct these operations safely and quickly in various environmental conditions.  These include flying in marginal weather, at night, and landing at unfamiliar areas. Air tour operators and airborne law enforcement units face similar issues.

These and other operational issues have led to an unacceptably high number of helicopter accidents and the NTSB stated there is no simple solution for reducing helicopter accidents. However, they have recommended some safety improvements to mitigate risk. For instance, helicopter operators should develop and implement safety management systems that include sound risk management practices, particularly with regard to inspection and maintenance. Moreover, establishing best practices for both maintenance and flight personnel that include duty-time regulations that take into consideration factors like start time, workload, shift changes, circadian rhythms, adequate rest time, and other factors shown by recent research, scientific evidence, and current industry experience to affect crew alertness. Operators should also make sure that their pilots have access to training that includes scenarios such as inadvertent flight into instrument meteorological conditions and autorotation. Also noted as invaluable when an accident occurs is a crash-resistant flight recorder system that will assist investigators, regulatory agencies, and operators in identifying what went wrong and how to keep it from happening again.

Recent NTSB investigations of 3 accidents resulted in the issuance of 27 safety recommendations pertaining to issues that include risk management, pilot training, maintenance, and flight recorders.  These include a June 2009 accident near Santa Fe, New Mexico, involving a helicopter on a search and rescue mission, an August 2011 HEMS accident near Mosby, Missouri and a December 2011 air tour accident near Las Vegas, Nevada.

During the last 10 years the NTSB has issued over 100 safety recommendations. If the high helicopter accident rate continues, the FAA could step in and enact regulatory changes that would force changes on the entire industry.

 

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High voltage

January 9, 2014 by Tim McAdams

The flight characteristics of a helicopter make it suitable for a variety of interesting missions. One such job is the repair of live high voltage lines. The voltage on these lines is typically between one hundred thousand to one million volts.

A typical configuration uses a platform mounted to the helicopter’s skids with a wire attached to the helicopter’s airframe. The lineman sits on the edge of the platform as the pilot hovers the helicopter next to the line that needs repair. In some cases, the pilot must maneuver the lineman within several inches of the power line. Because this is considered an external load operation, the platform can be jettisoned. However, the lineman’s harness is attached to the helicopter.

The helicopter and the high voltage wire have different electrical potentials, so to equalize them a metal wand is brought close to the wire. When the wand is close enough the voltage jumps across causing an arc. Once the wand makes contact with the wire, a clamp is connected to the platform with a 5 or 6 foot cable that is attached to the helicopter insuring the voltage potential remains equal. The wand is then removed and the repairs can begin. In the event of an emergency the clamp will break away from the power line. The helicopter now has a high electrical potential and the pilot must be careful to not let the helicopter get to close to an object (a tree, for example) that will allow the voltage a path to ground. This will significantly increase the current flow through the helicopter causing high heat and serious damage to equipment and personnel.

Several accidents have happened from engine failures or the rotor system coming in contact with part of the power line infrastructure. One such accident happen in August of 2013 and according to the NTSB the helicopter was conducting an electrical power line construction operation with a lineman standing outside on the skid. The wire was temporarily suspended by a hoist and the lineman was inserting a fiber shoe to attach the wire to the arm of the tower. While the helicopter was hovering next to the wire at about 200 feet above ground level the hoist slipped and the wire fell onto the top of the helicopter’s skid. Control was briefly lost and four of the helicopter’s main rotor blades impacted the tower resulting in substantial damage to the main rotor blades. The pilot quickly regained control and made an emergency landing in tall corn about 200 feet from the accident location.  Fortunately, the pilot did an excellent job and no one was injured.

Even when everything goes right, high voltage power lines create a very strong electromagnetic field. This field produces an induced current that anyone close to the line will feel along their skin. As such, the pilot and lineman wear a special suit with a metal weave that allows the current to flow around the skin. Even with the suit, the sensation has been described as a feeling of pins and needles.

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BK117

December 23, 2013 by Tim McAdams

The BK117 is a twin-engine, medium size helicopter developed jointly by Messerschmitt Bolkow Blohm (MBB) of Germany and Kawasaki of Japan. In early 1977 the two companies signed an agreement to share costs and produce two prototypes each. Although development took longer than originally planned, Japanese and German authorities certified the helicopter in late 1982 followed by the United States in early 1983.

The BK117 is a compact design with a total length of 43 feet and a main rotor diameter of 36 feet. MBB used a hinge-less rotor system with four main rotor blades attached to a titanium hub. A high tail rotor and rear clamshell doors made the BK117 very popular in the EMS industry.

The first version was the BK117 A-1 powered by two Lycoming gas turbine engines. Two major problems with the A1 were the low gross weight (6280 lbs) and a lack of tail rotor thrust and stability. In 1985 MBB introduced the A3, with a larger tail rotor, an optional yaw stabilization augmentation system (YSAS) and a gross weight increase to 7,055 pounds. A year later came the A-4, with increased take-off limits and an improved tail rotor hub. All A-series BK117s use the 650 shp Lycoming LTS-101- 650B1 turbine engine de-rated to 550 shp.

In 1987 MBB introduced the B1, which used the more powerful 750 shp LTS-101- 750B1 engine (still de-rated to 550 shp) and the YSAS became standard equipment. Next was the B2, with a beefier landing gear, shorter pitch change horns to improve main rotor response time and a gross weight increase to 7,385 pounds. Also available at the same time was a C1 model with Turbomeca Arriel 1E engines rated at 708 shp for better hot and high performance.

BK117

BK117

 

 

 

 

 

 

 

 

 

In 1992, MBB and the helicopter division of Aerospatiale merged to form Eurocopter. Under the newly formed company, the BK117 underwent several upgrades including a new forward cockpit design with modern avionics. It carries the FAA designation BK117 C2, but is marketed as the EC145. Powered by a pair of Turbomeca Arriel 1E2 engines rated at 738 shp each, the gross weight jumped to 7903 lbs. In 2006, the US Army signed a contract for 345 EC145 aircraft for use as a light utility helicopter. Known as the UH 72A (Lakota), the program has been a major success for the US Army.

UH 72A Lakota

UH 72A Lakota

EC145

EC145

 

Scheduled for certification in 2014 is the EC145 T2 featuring new FADEC equipped Arriel 2E engines delivering 1039 shp each. Additional improvements include a Fenestron tail rotor, a 4-axis autopilot and a gross weight increase to 8047 lbs.

EC145 T2

EC145 T2

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Volocopter

December 7, 2013 by Tim McAdams

Over the years there have been many different inventors and engineers who have attempted to built vertical lift aircraft. The single main rotor with a smaller anti-torque rotor emerged as the most popular. With recent advances in technology, innovative engineers have been attempting to build a practical electric-powered helicopter. As it turns out, the single main rotor design is not the most efficient – efficiency is necessary for an electric-powered helicopter to be capable of lifting a reasonable payload. As such, engineers are designing very different vertical lift vehicles. One of these is the 2-person Volocopter and its first successful flight was November 17, 2013.

Designed and built in Germany, the Volocopter has an especially unique design. It uses 18 rotors, each powered by its own electric motor. They are mounted on a light weight carbon fiber ring above the cabin. Several on-board computers monitor and control the speed of each rotor system to achieve directional control – eliminating the need for any type of mechanical linkage. The system is designed so that if one of the motors fails (actually, several can fail at the same time) the aircraft can still safely land. Additionally, there is a ballistic parachute system for added safety.

Currently, the biggest limitation is battery life. The battery allows a flight time of 20 minutes, however, the company believes that advances in battery technology will extend the flight time in the near future. As an interim solution, the Volocopter will be built as a hybrid which will allow several hours of flight time. This is achieved by using a combustion engine to power a generator that supplies the batteries and motors with electricity.

The manufacturer, E-volo, claims the production aircraft will be extremely cost effective to operate, very quiet and easy to fly. More information can be found on their website: www.e-volo.com.

vc200_first-flight_13

vc200_first-flight_04

 

 

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Main rotor rotation

November 24, 2013 by Tim McAdams

In basic terms, a helicopter’s main rotor system is what provides lift and thrust. The rotational speed (rpm) is held constant and the pitch angle of the blades is varied to change the amount of lift and thrust. Engineers look at many different variables when designing a rotor system and one is the direction the rotor spins, clockwise or counter clockwise (when viewed from above). Unlike the tail rotor, from an aerodynamic efficiency standpoint there is no difference between the two directions. As it turns out, in most cases the direction of rotation can be associated with the country of origin. For example, as a general rule, helicopters manufactured in the United States (and some other countries like Germany) turn counter clockwise, while French and Russian designed helicopters spin clockwise.

However, from a piloting viewpoint there are some differences. The biggest one comes from Newton’s third law that states for every action, there is an equal and opposite reaction. As such, the torque applied to the rotor system causes the helicopter’s fuselage to spin the opposite direction. This is the primary reason for the tail rotor, or more accurately called the anti-torque rotor. It applies a force opposing the main rotor torque to stop the fuselage from spinning. The more power the pilot demands, the higher the torque and the more thrust the anti-torque rotor must produce to control yaw. In the cockpit, it is the pedals that control the anti-torque rotor’s pitch and therefore its thrust. What this means to the pilot is in a clockwise turning main rotor, right pedal must be added as power is increased and left pedal when power is reduced. For a counter clockwise spinning rotor system it is just the opposite.

Some of the other differences that are not as noticeable to the pilot are translating tendency and dissymmetry of lift. Translating tendency is the tendency of the helicopter to drift in the direction of tail rotor thrust. A clockwise turning rotor will cause the helicopter to drift to the left. Dissymmetry of lift refers to a difference in lift across the rotor system as one blade advances into the wind (headwind) and the other side retreats (tailwind). Again, depending on which way the rotor spins the advancing side will be on the right or left side of the rotor disc.

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Electric flight

November 11, 2013 by Tim McAdams

In 2010, Sikorsky Aircraft introduced “Project Firefly,” an all electric helicopter technology demonstrator based on the S-300C airframe. The intent was to have it flying a year later and set a world record for the first all electric manned helicopter flight. Unfortunately, the company did not make the target date and last year the first all electric powered helicopter flight was achieved by pilot and designer Pascal Chretien in France.

Chretien took a different approach than Sikorsky, rather than use a heavy existing airframe he designed a new lightweight highly energy efficient aircraft. As an electrical engineer and commercial rated helicopter pilot he knew what areas to target. A tail rotor can consume 10 percent of available power, so to eliminate the tail rotor Chretien used a coaxial main rotor system. He employed a second generation asymmetrical rotor blade design which provided a 19% increase in lift over his initial blades. Powered by a lightweight (128 pounds) Lithium ion polymer pouch cell battery pack the two DC powered electric motors provided a total of 43 hp, enough power to lift the required 545 pounds. Each rotor system has its own motor and yaw is controlled by varying the electrical signal to each motor.

In July and August of 2011, the aircraft made 29 flights totaling 99.5 minutes with some flights lasting 6 minutes. Then on 12 August 2011, the world’s first un-tethered manned flight of a helicopter powered only by an electric motor took place at Venelles, France. Chretien hovered above the ground for 2 minutes 10 seconds entering the Guinness World Book of Records.

 

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Bleed air

November 1, 2013 by Tim McAdams

Turbine powered helicopters use bleed air for heating, demisting and other systems like sand filters. Bleed air is taken from the compressor section of the engine. For example, the Arriel 1 series engines use a two stage compressor section.

Arriel 1 compressor section

Arriel 1 compressor section

The first stage uses an axial compressor to increase the speed and pressure of the ambient air.

Capture2

The second stage uses a centrifugal compressor to further compress the air and raise the temperature. This is where bleed air is taken from the engine.

Capture3

Prior to entering the combustion chamber the air is extremely hot from compression alone. For cabin heating, the bleed air is mixed with outside air to cool it.

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