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Rotor twin

Rotor twin

Rotor twin

Rotor twin

Rotor twin

Field Equipment. Notably, this was the world's first volume-production sequential twin turbocharger system. Double Points for VIPs! First, the exhaust ports are not peripheral but are located on the side of the housing, which eliminates overlap and allows redesign of the intake port area. It only actually displaces 1. Sales of the RX-8 peaked in at 23, but continued to decline throughwhen less than were produced. In order to carry out the Rotor twin of the total kinetic energy of the TRMS, it is necessary to calculate the kinetic energy corresponding to each of the three subsystems previously defined. Secondly, the rotors are sealed differently through the use of redesigned side seals, low-height apex seals and the addition of a second cut-off ring. The electrical part of Straps stock system is formed by the interface circuit and the DC motors of the Rotor twin and tail rotors.

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Namespaces Article Talk. Defense News6 August Categories : Helicopter components Tandem rotor helicopters. Archived from the original on 29 March The Libyan Chinooks flew transport and support missions into Chad to Rotor twin Libyan ground forces operating there in the s. Archived from the original twun 2 April A CHF Block 2 is planned to be introduced after Retrieved 5 January Archived from the original on 25 July Archived from the original on 14 July The surviving aircraft, Easy Moneyhas been restored and is on display at Redstone ArsenalAlabama. Inwork on the experimental Model was begun. The Boeing CompanyF. Tein achieve pitchopposite collective Rotor twin applied to each rotor; decreasing the lift ywin at one end, while increasing lift at the opposite end, Rotor twin tilting the helicopter forward or back. It would be some time before troops would be experts at using sling loads.

This faster separation virtually eliminates grain damage and loss.

  • Tandem rotor helicopters have two large horizontal rotor assemblies mounted one in front of the other.
  • The CH is among the heaviest lifting Western helicopters.
  • Double Points for VIPs!

The TRMS is an underactuated nonlinear multivariable system, characterised by a coupling effect between the dynamics of the propellers and the body structure, which is caused by the action-reaction principle originated in the acceleration and deceleration of the propeller groups.

Secondly, we present a design of a nonlinear cascade-based control algorithm that locally guarantees an asymptotically and exponentially stable behaviour of the controlled generalised coordinates of the TRMS. Currently, there are many possible uses for unmanned aerial vehicles UAVs , such as inspection operation, battle field operation, forest fire detection, meteorological observation, or search and rescue operation, among others. All these applications require achieving precise control systems.

This has motivated an increased interest in the last years from researchers in developing effective control algorithms for UAVs [ 1 — 4 ]. In many cases, the development of new control strategies requires the use of software and platforms which are able to simulate the operation of the UAVs in order to perform experimental tests for evaluating the different designs. The use of this kind of tools increases the productivity and reduces the development time.

For this purpose, different laboratory test rigs have been specifically designed for teaching and research in flight dynamics and control. The TRMS is a nonlinear, multivariable and underactuated system, characterised by a coupling effect between the dynamics of the propellers and the body structure, which is caused by the action-reaction principle originated in acceleration and deceleration of the motor-propeller groups.

All these features make the control of the TRMS to be perceived as a challenging engineering problem note that the TRMS, and other laboratory platforms with similar dynamics are more difficult to control than a real helicopter platform [ 6 ].

The achievement of an accurate system dynamics model is a challenging problem, whilst, at the same time, an important issue is to develop accurate and efficient control systems. The development of the dynamic model for the TRMS has been studied by an important number of researches. Ahmad et al. Rahideh and Shaheed have also contributed to the study of the TRMS dynamics by using both Newton- and Lagrange-based methods [ 10 ], and two models based on neural networks using Levenberg-Marquardt LM and gradient descent GD algorithms [ 11 ].

Finally, Tastemirov et al. On the other hand, the design of the control system for the TRMS has been widely discussed through several investigations. Rahideh et al. Other interesting works are those of Tao et al. Studies of Reynoso-Meza et al. The aim of the present research is to develop a nonlinear cascade-based control algorithm in order to locally guarantee an asymptotically and exponentially stable behaviour of the controlled generalised coordinates of the TRMS.

Additionally, the effectiveness of the proposed nonlinear feedback controller in terms of stabilisation and position tracking performance is demonstrated by means of numerical simulations. Finally, the paper is organised as follows. Section 2 introduces a description of the TRMS platform by illustrating the details of the dynamics model obtained into two phases: electrical and mechanical parts.

Section 3 describes the nonlinear cascade-based controller scheme proposed. The TRMS is composed of two propellers that are perpendicular to each other and placed in the extreme of a beam that can rotate freely in both vertical and horizontal planes. Each propeller is driven by a DC motor, thus forming the main and tail rotor of the platform. A main feature of the TRMS is that its movement, unlike a real helicopter, is not achieved by varying the angle of attack of the blades.

In this case, the movement of the platform is gotten by means of the variation in the angular velocity of each propeller, which is caused by the change in the control input voltage of each motor. This constructive simplification in the TRMS model substantially complicates the dynamics of the system, because a coupling effect between rotors dynamics and the body of the model appears.

This effect is caused by the action-reaction principle originated in acceleration and deceleration of the motor-propeller groups. In addition, the TRMS is an underactuated system. This implies that the number of variables that act as control inputs voltages applied to the main and the tail rotor; u m and u t respectively is lower than the number of degrees of freedom DoF of the system.

The development of an efficient control algorithm requires a model that represents the dynamic behaviour of the platform under study as accurately as possible. However, not all of them provide a model that represents the entire complex dynamic behaviour of this experimental platform.

For instance, models based on identification techniques have difficulties in representing the effects of coupling, which are characteristic in this platform [ 7 ], and neuronal networks and learning algorithms allow obtaining accurate models, but limited to a range of input values and frequencies [ 11 ]. Based on previous works developed for the dynamic model of this platform [ 13 , 22 — 24 ], a detailed dynamic model of the TRMS has been developed by dividing the whole dynamics of the system in their electrical and mechanical parts.

This approach allows not only to adequately capture the complex dynamics behaviour of the TRMS but also the development of novel control algorithms based on nested feedback loops that offer a higher performance than classical control schemes.

Moreover, the use of the Euler-Lagrange method in the modelling of the mechanical structure of the TRMS allows a higher adjustment with the real control laboratory platform in comparison with other analytical methods based on the Newtonian approach [ 25 ].

The dynamic modelling has been developed in two stages and validated by our research group by means of experimental identification trials. It is presented in the following subsections.

The first subsection illustrates the dynamic model of the electrical part, and the second depicts the dynamic model of the mechanical part of the system. The electrical part of the system is formed by the interface circuit and the DC motors of the main and tail rotors. This interface can be modelled as a linear relationship [ 13 ], obtaining the following result:. With regard to the DC motors, there are two identical permanent magnet motors, one in each rotor of the TRMS, with the only difference of the mechanical loads the propellers.

On the other hand, the electromechanical balance of the torques acting on each motor is expressed as:. After substituting the expression for the current intensity of the respective motors [obtained from Eqs. The dynamics of the electrical part of the TRMS is now expressed in a matrix form, using the following compact notation:. Finally, in order to complete the dynamic model of the electrical part of the TRMS, Tables 1 and 2 show the parameters used in the model, indicating the description of the parameters, their values and their corresponding units.

These values, which are based on the data presented in [ 13 ], have been experimentally tuned and validated in the dynamics identification tests that we have performed during our research. In the development of the dynamic model of the mechanical part, we consider the mechanics of the TRMS as an assembly of the following three components explained next. The first component is formed by the two rotors, their shields and the free-free beam that links together both rotors.

The second component consists in the counterbalance and counterweight beam, and finally, the third component is the pivoted beam. Figure 2 helps to clarify the different components considered in the dynamics of the mechanical part of the system.

From the previous division, and bearing in mind the notation used in Figures 3 and 4 , the development of the dynamic model is achieved by means of the application of the Euler-Lagrange formulation. It can be summarised in the following steps:. The problem of direct kinematics of the TRMS consists in determining the spatial position of the three subsystems considered, according to the reference system located in the upper part of the platform see Figures 3 and 4. Using the Denavit-Hartenberg method, we can express the position of a point on each subsystem P 1 , P 2 , P 3 parameterised by R 1 , R 2 , R 3 , which represents the distances between the considerate points and the reference system associated to each subsystem.

In order to carry out the evaluation of the total kinetic energy of the TRMS, it is necessary to calculate the kinetic energy corresponding to each of the three subsystems previously defined.

Starting with the first subsystem, its kinetic energy, T 1 , yields:. On the other hand, the kinetic energy for the second subsystem, T 2 , results in:. On the other hand, the kinetic energy for the third subsystem, T 3 , gives the following result:.

Finally, the total kinetic energy of the TRMS, T , is obtained as the sum of the kinetic energy of each subsystem Eqs. One obtains the following result:. Following a similar procedure to the one used in the computation of the kinetic energy, the total potential energy of the TRMS, V , consists of the sum of the potential energy of each of the three subsystems, the free-free beam including rotors and shields , the counterbalance beam and the pivoted beam.

The following result is obtained:. The last step in the mechanical dynamic model of the TRMS is obtaining the equations of motion of the system. The first step is the computation of the Lagrangian of the system, defined as the difference between the total kinetic energy, defined in Eq.

The following expressions illustrate several partial results necessary to achieve the equations of motion represented by Eqs. On the other hand, the sum of the external torques in the horizontal axis is as follows:. Upon merging Eq. If we use matrix notation, the dynamic model of the mechanical part of the TRMS can be expressed in a compact form:. Finally, after substituting Eqs.

Finally, in order to complete the dynamic modelling for the mechanical part of the TRMS, Tables 3 — 5 show in detail the parameters used in the model. For each parameter, its description, its value and the corresponding units is included. The initial approximation of these values was based in the developments described in [ 13 ].

Additionally, some values of the parameters have been tuned by carrying out several identification trials. In this section, the proposed nonlinear control for the TRMS platform is described. The proposed control is based on the division between the electrical and mechanical dynamics of the system and uses a cascade-type nonlinear control algorithm. Figure 5 displays the proposed control scheme. As it can be observed, the proposed design is composed of two independent stages or control loops that are utilised to achieve stabilisation and precise trajectory tracking tasks for the controlled position of the generalised system coordinates.

It should be noted that the proposed solution has been designed to overcome one of the limitations of the TRMS, which is the fact of being an underactuated system. As result of this fact, it only has two control actions the input voltages of the main and tail rotors to control the four degrees of freedom of the system the pitch and yaw angles, and the angular velocities of the propellers. In this way, in order to meet this objective, once the dynamics of the TRMS have been decoupled, a nonlinear multivariable inner loop is closed to control the vector of the angular velocities, and then, a nonlinear multivariable outer loop is closed to control the vector of the generalised coordinates of the system.

This solution, based on a control scheme with two nested loops, allows a simplification in the design procedure as a result of its division into two simpler processes. Moreover, the scheme can be implemented more easily and safely than the standard controllers. In the following subsections we describe the specifications and objectives of each control loop, defined as the inner loop or electrical controller and the outer loop or mechanical controller.

The magnitude of the input control voltage vector, u t , necessary to achieve an asymptotically stable convergent behaviour of the tracking error trajectories, is calculated as the following nonlinear control law:.

Finally, the coefficients of the matrix K P e are chosen so as to render the closed-loop characteristic polynomial vectors into a Hurwitz polynomial vector with desirable roots. As a previous step for determining the mechanical control law, a simplification in the dynamic mechanical modelling of the TRMS has been considered.

In this way, the dynamic equation of the mechanical part of the TRMS can be rewritten as:. The controller design matrices K D m and K P m have been selected based in the philosophy used for the electrical controller.

They must be selected to render closed-loop characteristic polynomial vectors into a Hurwitz polynomial vector with desirable roots. On the other hand, the values used in the simulation of the dynamic model of the TRMS, electrical parameters main and tail rotors , mechanical parameters and dimensional parameters of the platform are detailed in Tables 1 — 5. This choice of the starting position has been made to demonstrate the exponential convergence of the desired trajectories.

With regard to the controller design parameters, it must be remarked that they have been selected to make the dynamics of the inner loop much faster than the outer loop dynamics, all this in order to ensure the functioning of the cascade controller [ 26 ].

The resulting values are as follows:. Figures 6 and 7 show the performance of the proposed control scheme. The exponential convergence of the desired trajectories is observed, with the error bounded to a small neighbourhood to zero, and the robustness against large initial errors. Another graph that shows the excellent performance of the outer control loop is shown in Figure 8 , where the auxiliary control input vector of the mechanical proportional-derivative PD controller Eq.

Retrieved 12 February Tandem rotor helicopters, however, use counter-rotating rotors , with each cancelling out the other's torque. The surviving aircraft, Easy Money , has been restored and is on display at Redstone Arsenal , Alabama. Army CHD built was delivered to the U. The CHD shares the same airframe as earlier models, the main difference being the adoption of more powerful engines.

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CMH Pub Archived from the original on 12 June Retrieved 19 August The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books. Whirlybirds, A History of the U. Helicopter Pioneers. University of Washington Press, Los Angeles Times. Archived from the original on 26 October Retrieved 5 July Flight International. Archived from the original on 11 October Retrieved 29 March Archived from the original on 30 March Retrieved 13 November The Philadelphia Inquirer.

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Zenith Imprint. Archived from the original on 27 December Retrieved 9 March Advocacy and Public Policymaking. Archived PDF from the original on 12 June Number Volume New-build CHD ready for co-production. Archived from the original on 4 November Archived from the original on 14 May Retrieved 6 February Aviation Week , 28 February Archived from the original on 29 September Retrieved 29 September Archived from the original on 24 November Retrieved 23 November Archived from the original on 24 September Retrieved 30 June Nordbayern online in German.

Archived from the original on 20 August Retrieved 10 August Schoenborn v. The Boeing Company , F. Archived from the original on 1 December Archived from the original on 1 April Arlington National Cemetery site. Archived from the original on 2 May Retrieved 21 June Korean Helicopter Crashes into Bridge, 3 Killed". People's Daily, 30 May The Daily Telegraph , 30 May The Seattle Times.

Associated Press. Retrieved 26 July Honolulu Star-Bulletin. Archived from the original on 8 August The Oregonian , 8 January Retrieved 27 July National Air Force Museum of Canada. Royal Air Force Museum. Newark Air Museum. United States Army Aviation Museum. Castle Air Museum. Creator 3-in Average rating0out of 5 stars. Add to Wishlist. Build the Twin Rotor Helicopter and then rebuild it into a Jet or Hovercraft toy for more fast-moving adventures.

The Twin Rotor Helicopter features large synchronized rotors, tinted cockpit with 2 seats, opening side and rear cargo bay doors and a working winch, plus an ROV submarine that fits into the cargo bay.

Turn the gear wheel to spin the helicopter's huge synchronized rotors. Open the helicopter's rear cargo bay door and load up the included ROV submarine. Deliveries and Returns. Express shipping available at checkout. Custom parts orders are sent separately from merchandise and take additional time to process and deliver. Unopened merchandise may be returned for a full refund within 90 days of receipt of your order.

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The Mazda Wankel engines are a family of Wankel rotary combustion car engines produced by Mazda. Wankel engines were invented in the early s by Felix Wankel , a German engineer. Over the years, displacement has been increased and turbocharging has been added. Mazda rotary engines have a reputation for being relatively small and powerful at the expense of poor fuel efficiency. The engines became popular with kit car builders, hot rodders and in light aircraft because of their light weight, compact size, tuning potential and inherently high power-to-weight ratio —as is true for all Wankel-type engines.

Since the end of production of the Mazda RX-8 in , the engine is produced only for single seater racing , [ citation needed ] with the one-make Star Mazda Championship being contested with a Wankel engine until the series transitioned to using a Mazda-branded piston engine in These metrics function similarly to the bore and stroke measurements of a piston engine.

As Wankel engines became commonplace in motor sport events, the problem of correctly representing each engine's displacement for the purposes of competition arose. Rather than force the majority of participants driving piston engine cars to halve their quoted displacement likely resulting in confusion , most racing organizations simply decided to double the quoted displacement of Wankel engines.

The key for comparing the displacement between the 4-cycle engine and the rotary engine is in studying the degrees of rotation for a thermodynamic cycle to occur. The rotary engine is different. Obviously, there is a disparity. How can we get a relatable number to compare to a 4-stroke engine? That's a well-reasoned number and now gives something that can be compared to other engines. The 13B therefore compares well to a 2.

Although never produced in volume, the 40A was a valuable testbed for Mazda engineers, and quickly demonstrated two serious challenges [ citation needed ] to the feasibility of the design: "chatter marks" in the housing, and heavy oil consumption.

The chatter marks, nicknamed "devil's fingernails", [ citation needed ] were caused by the tip-seal vibrating at its natural frequency. The oil consumption problem was addressed with heat-resistant rubber oil seals at the sides of the rotors. The engine and car were both shown at the Tokyo Motor Show. Hollow cast iron apex seals reduced vibration by changing their resonance frequency and thus eliminated chatter marks.

It used dry-sump lubrication. One-, three-, and four-rotor derivatives of the L8A were also created for experimentation. The 10A series was Mazda's first production Wankel, appearing in The rotor housing was made of sand-cast aluminum plated with chrome, while the aluminum sides were sprayed with molten carbon steel for strength.

Cast iron was used for the rotors themselves, and their eccentric shafts were of expensive chrome-molybdenum steel. These cars, and their revolutionary engine, were often called L10A models.

The 10A featured twin side intake ports per rotor, each fed by one of four carburetor barrels. Only one port per rotor was used under low loads for added fuel economy. A single peripheral exhaust port routed hot gas through the coolest parts of the housing, and engine coolant flowed axially rather than the radial flow used by NSU.

A bit of oil was mixed with the intake charge for lubrication. These engines had both side- and peripheral-located intake ports switched with a butterfly valve for low- and high-RPM use respectively. Its construction was very similar to the The final member of the 10A family was the This variant featured a cast-iron thermal reactor to reduce exhaust emissions and re-tuned exhaust ports.

The new approach to reducing emissions was partly a result of Japanese Government emission control legislation in , with implementation starting in The die-cast rotor housing was now coated with a new process: The new Transplant Coating Process TCP featured sprayed-on steel which is then coated with chrome. A prototype engine is on display at the Mazda Museum in Hiroshima , Japan.

The 13A was designed especially for front wheel drive applications. Another major difference from the previous engines was the integrated water-cooled oil cooler. This was the end of the line for this engine design: the next Luce was rear wheel drive and Mazda never again made a front wheel drive rotary vehicle. The 12A series was produced for 15 years, from May through In , a 12A became the first engine built outside of western Europe or the U.

S to finish the 24 hours of Le Mans. In , a new process was used to harden the rotor housing. The Sheet-metal Insert Process SIP used a sheet of steel much like a conventional piston engine cylinder liner with a chrome plated surface.

The side housing coating was also changed to eliminate the troublesome sprayed metal. The new "REST" process created such a strong housing, the old carbon seals could be abandoned in favour of conventional cast iron.

Early 12A engines also feature a thermal reactor, similar to the 10A, and some use an exhaust port insert to reduce exhaust noise. A lean-burn version was introduced in in Japan and in America which substituted a more-conventional catalytic converter for this "afterburner".

A major modification of the 12A architecture was the 6PI which featured variable induction ports. A passive knock sensor was used to eliminate knocking , and later models featured a specially-designed smaller and lighter "Impact Turbo" which was tweaked for the unique exhaust signature of the Wankel engine for a 5-horsepower increase.

It had increased reliability from previous series, and it introduced a single distributor. This was the beginning of the single distributor rotary engines: the earlier 12A and 10A were both twin distributor Wankels.

The improved 12B was quietly introduced in The 13B is the most widely produced engine. It was the basis for all future Mazda Wankel engines, and was produced for over 30 years. The 13B has no relation to the 13A. The 13B was designed with both high performance and low emissions in mind. Early vehicles using this engine used the AP name. The so-called Dynamic Effect Intake featured a two-level intake box which derived a supercharger -like effect from the Helmholtz resonance of the opening and closing intake ports.

The 13B-T was turbocharged in It features the newer four-injector fuel injection of the 6PI engine, but lacks that engine's eponymous variable intake system and 6PI. Mazda went back to the 4 port intake design similar to what was used in the '74—'78 13B. In '86—'88 engines the twin-scroll turbocharger is fed using a two-stage mechanically actuated valve, however, on '89—'91 engines a better turbo design was used with a divided manifold powering the twin-scroll configuration.

The 13B-RE from the JC Cosmo series was a similar motor to the 13B-REW but had a few key differences, namely it being endowed with the largest side ports of any later model rotary engine.

A twin- turbocharged version of the 13B, the 13B-REW , became famous for its high output and low weight. Notably, this was the world's first volume-production sequential twin turbocharger system. In Le Mans racing, the first three-rotor engine used in the was named the 13G.

The main difference between the 13G and 20B is that the 13G uses a factory peripheral intake port used for racing and the 20B production vehicle uses side intake ports.

It was renamed 20B after Mazda's naming convention for the in November It was the world's first volume-produced twin-turbo setup. A for the Furai concept car which was released on 27 December, During a Top Gear photo shoot in , a fire in the engine bay combined with a delay to inform the fire crews, the car was engulfed and the entire car destroyed.

This information was withheld until made public in The most prominent 4-rotor engine from Mazda, the 26B, was used only in various Mazda-built sports prototype cars including the and B in replacement of the older 13J. In the 26B-powered Mazda B became the first Japanese car and the first car with anything other than a reciprocating piston engine to win the 24 Hours of Le Mans race outright.

The 26B engine displaced 2. The engine design uses peripheral intake ports, continually variable geometry intakes, and an additional third spark plug per rotor. It was designed to reduce exhaust emission and improve fuel economy , which were two of the most recurrent drawbacks of Wankel rotary engines.

The Renesis design features two major changes from its predecessors. First, the exhaust ports are not peripheral but are located on the side of the housing, which eliminates overlap and allows redesign of the intake port area. This produced noticeably more power thanks to an increased effective compression ratio; however, Mazda engineers discovered that when changing the exhaust port to the side housing, a buildup of carbon in the exhaust port would stop the engine from running.

To remedy this, Mazda engineers added a water jacket passage into the side housing. Secondly, the rotors are sealed differently through the use of redesigned side seals, low-height apex seals and the addition of a second cut-off ring. Mazda engineers had originally used apex seals identical to the older design of seal. Mazda changed the apex seal design to reduce friction and push the new engine closer to its limits. It only actually displaces 1. Finally, it was on the Ward's 10 Best Engines list for and All the Mazda rotary engines have been praised because of their light weight.

Also known as the Renesis II, made its first and only appearance in the Mazda Taiki concept car at the Tokyo Auto Show, but has not been seen since. Mazda was fully committed to the Wankel engine just as the energy crisis of the s struck.

The company had all but eliminated piston engines from its products in , a decision that nearly led to the company's collapse. Though not reflected in the graph at right, the RX-8 was a higher-volume car than its predecessors. Sales of the RX-8 peaked in at 23,, but continued to decline through , when less than were produced. On November 16, , Mazda CEO Takashi Yamanouchi announced that the company is still committed to producing the rotary engine, saying, "So long as I remain involved with this company Currently, [ when?

Mazda last built a car powered by a rotary engine in , the RX-8, but had to abandon it largely to poor fuel efficiency and emissions. It has continued to work on the technology, however, as it is one of the company's signature features. Mazda officials have previously suggested that if they can get it to perform as well as a reciprocating engine they will bring it back, to power a conventional sports car.

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