The heavy lift industry is in desperate need of a modern aerial lift solution. The current heavy lift industry relies almost exclusively on old, outdated, and largely obsolete airframes developed in the 1950s. No new generation of heavy-lift rotorcraft have been developed since. We believe there exists tremendous market potential to develop a modern heavy-lift rotorcraft incorporating technological innovations that have taken place during this stagnant development history. Pochari Technologies has incorporated a number of important and differentiating features that enable the crane to stand out from the current heavy-lift fleet. The key features that differentiate this modern aerial crane are its unmanned flight control system, modular configuration to enable vehicle-based transport, and most importantly, a unique fuselage-less design that saves considerable weight as well as minimizing footprint. In addition, this design incorporates significantly higher disc loading than previous heavy-lift hovercraft, this at first glance may seem to be a disadvantage due to tthe increased power required, but this decision is carefully made to enable significantly reduced rotor diameter. Conventional rotorcraft are designed to maximize range for long-distance missions, heavy-lift rotorcraft in comparison require only short endurance for short radius operation, refueling can be performed periodically, thus higher fuel burn does not compromise the performance and is well worth the reduction in rotor diameter to enable landing in confined areas. One of the key advantages to the aerial crane design is the substantially reduce empty weight fraction. Since our design eliminates the fuselage, tail rotor boom and landing gear, the empty weight fraction is reduced to 30-35% depending on the exact model, compared to 50% for traditional rotorcraft, this increase in payload makes the machine much more competitive as it reduces hourly cost per pound lifted.
The Aerial crane is designed to shine in lifting applications that require significantly greater operating radius, unlimited mobility, greater operating flexibility, quick setup and turn around time, and where ground-based cranes simply cannot perform. Prime applications include pre-fabricated modular construction, installing offshore wind turbines, installing wind turbines in mountainous terrain, moving air conditioning units atop a building, pouring concrete in mountainous regions, transporting an excavator atop a high rise building for demolition, transporting shipping containers from ports, installing solar farms, bridge construction, moving large stones from a quarry, mining operations, offshore oil and gas rig construction, or moving large stationary power generators or transformers from rural areas. The aerial crane shines in virtually any situation where heavy objects, building materials, or construction equipment need to moved fast, and most importantly anywhere regardless of terrain conditions. Currently, conventional helicopters are prohibitively expensive to purchase and operate: Enter the Aerial crane. Designed solely as a heavy lift craft, not as a manned helicopter, we bypass all of the costly requirements that make helicopters so expensive. By eliminating the pilot, we can remove the entire cockpit section, reducing insurance and personnel costs. In addition, all of the necessary instruments and flight control systems are replaced with a simple remote-control system. The elimination of a crash worthy fuselage and cabin section save considerable weight, adding to the lift capacity. By designing the aerial crane to be moved and transported by truck, instead of ferrying over by flying, we can avoid operating over populated areas, enabling less stringent certification and insurance requirement. Even if ferrying over non-populated areas is feasible, the cost and time can be significant as jobsites are often located far removed remote locations all around the globe. The specialized nature of the aerial crane mean the number of units worldwide is small relative to the number of jobs conterminously being performed at any given time, resulting in a constant need to transport the crane long distances. The nature of aerial crane missions is generally short term, resulting in low utilization rates unless the crane can be immediately transported to another jobsite. Once the rotor blades are removed, all that remains is the compact drive module and shaft, once the shaft is disconnected at the base, the module can be placed inside a small box truck. The benefit of the coaxial design is the minimal mainframe footprint, the powerplant and gearbox occupy minimal volume, the shaft extends a considerable distance, but once it is disconnected, the entire unit occupies very minimal space, enabling convenient transport.
The aerial crane’s operation is strictly limited to job sites with a defined radius of operation, which is only occupied by trained personnel, if any time the aerial-crane is going operate over populated areas, all occupants are evacuated. Ferrying or flying over populated areas is made redundant by the inherent modularity of the system which permits easy ground transport. By eliminating the need for more stringent traditional manned aviation certification, the cost is reduced by an significant margin. By eliminating the extremely high safety and performance standards required for passenger-carrying aircraft, manufacturing costs are dramatically reduced, additionally, the reduced accident rate attributable to the unmanned and partially autonomous flight control reduces the perceived hazard of rotorcraft operating in heavy-lift settings. The aerial crane will be sold for only $1,000,000, only twice the cost of the equivalent capacity tower crane. The capacity of the aerial-crane is 10 tons, or 20,000 lbs, 9000 kg. The range without aerial refueling is 50 miles or one hour of operation. That means our aerial crane can carry 10 tons, over 50 miles! The crane can operate for up to 24 hours at a time with aerial refueling provides by a ducted fan drone. Conventional cranes are nearly made obsolete in the face of the aerial crane.
The aerial crane is transported to the jobsite by a specialized truck which serves as a landing platform. If a road is not located nearby, the crane is set up and flown over a non-populated route to the jobsite. The crane itself cannot land on terrain, the reason is landing gear adds a significant amount of weight, therefore we decided to eliminate all onboard landing gear. The crane is required to land directly on the truck-based platform. Once landed on the truck-based platform, the rotor blades can be removed, allowing the main module (power module), consisting of the powerplant, gearbox, driveshaft, and flight control system, to be placed flat down and carried on a flatbed truck. Set-up time is less than an hour. To control the crane, a portable screen displays footage taken from a camera placed underneath the drive module aiming down towards the load, displaying the position of the suspending load, enabling the operator to precisely place the load in the required destination. Flight controls are performed with a joke stick device, with directional controls provided by tilting the joystick in the desired direction, yaw control is provided by a separate joystick, and collective or altitude control provided by sliding the yaw or cyclic joystick up and down. Flight controls are designed to remove most of the workload from the operator, freeing the operator to focus on load placement. Unlike conventional rotorcraft which are extremely difficult to control, the aerial crane is as easy to fly as a consumer quadcopter.
The powerplant consists of 6x in-house developed turboshafts. The compressor is all centrifugal, to reduce cost, as centrifugal compressors are easily machined by any machine shop with a 5 axis CNC. A centrifugal compressor design is much simpler, eliminating stators. The power turbine is a “Blisk” design cast or machined out of Haynes Hastelloy X. A Blisk design reduces cost and complexity by machining or casting the entire unit in one single component, both blades and disc, eliminating the need to machine individual blades and “firtree” in the disk. The mass flow rate is 3.5 kg/sec. Bearings are standard high-speed oil lubricated roller bearings. The turboshaft is rated for 1000 takeoff-horsepower, and 850 continuous. The turboshaft is multi-fuel capable, with both gaseous and liquid fuel combustors available. In regions where liquid natural gas is readily available for low cost, a gaseous version is available. In regions where liquid fuels are inexpensive, diesel fuel is used since no high-altitude gelling requirements are present. Liquid hydrogen is also an available fuel option. The main rotor gearbox includes a bevel gear for the co-axial rotor drive, and epicyclic gears for reduction. The turboshafts are placed around a 4 stage large epicyclic gearbox, providing 250x reduction from 50,000 rpm down to 200 rpm for the main rotor. The rotor system incorporates Pochari Hydrogen’s innovative independent rotor control, where hydraulic pitch-link actuators provide rotor pitch actuation without a swashplate. Hydraulic fluid is transmitted via slip-ring for the lower rotor, and via an on-board hydraulic pump for the upper rotor. All flight controls are fly-by-wire. Each actuator is independently activated electronically via remote control. The second option, which the design team is considering as a simpler solution, is a conventional swashplate rotor pitch actuator system. The main rotor hub is manufactured from lay-up sheets of 300,000 psi T800 Toray aerospace-grade carbon fiber. The main rotor grips are titanium, as well as main rotor shaft. The gearbox housing is Aluminum 7075. The bevel gear and epicyclic gears are made of 4340 steel. The rotor system is semi-articulating, with elastomeric bearings providing lead-lag and flap. The main rotor blades are made of Toray T800 carbon fiber and Nomex honeycomb, with a stainless steel leading edge and straight non-swept tips to reduce manufacturing cost, the blade root is also a basic straight end instead of a narrower root design typically found in modern helicopter rotor blades. with a weight of 250 lbs each. Assembly and prototype testing is performed in Chennai, India, with certain components coming from all over China. Turbomachinery is manufactured in China by Shandong Yili Power Technology Co Ltd. and Zhenjiang Supersoar Machinery Co Ltd.
Cranes will be available for purchase in early 2025-2030 depending on financing. The purchase price is $990,000 for the turbine version, and $800,000 for the electric version. The hourly operating cost is $720/hr for the turbine version, and $330/hr for the electric version.
Specifications: Unmanned heavy lift mobile aerial crane (non-certified experimental) Use over populated areas is strictly prohibited
Crane is designed solely as a heavy lift machine for construction sites and worksites with only trained personnel present.
Powerplant: Gas turbine or fully electric.
Fully Electric corded version for short radius: 500 feet. The electric powerplant consists of 16x 300 hp axial flux electric motors arranged in a stack of four arranged around an epicyclic gearbox horizontally. Three Aluminum alloy 1350 2000 MCM power cables (weighing 3100 lbs, only half the weight carried by the aerial crane) are carried by an intermediate lifter craft 100 ft above the ground-based power unit, the cable then spans from the lifter craft to the aerial crane up to 500 feet. When more radius is needed, the ground power unit can be moved closer, think of the aerial electric crane as a tower crane on wheels.
A gas turbine-powered version for long working radius, 50 miles, 80 km.
Powerplant specifications for turbine version: 6x 800 shp dual centrifugal compressor dual power turbine reverse flow turboshaft. Turbine inlet temperature: 1560 °F
Combustor: Dual-fuel gaseous-liquid reverse flow
Compression ratio: 14:1
Compressor: Three centrifugal 304 stainless steel
Power turbine: 1x HP, 1x LP Dual 40 blade Blisk Hastelloy X
Specific fuel consumption: 0.55 lbs/shp-hr
Weight: 250 lbs
Shaft ouput speed: 55,000 rpm
Power output: 1000 shp take off, 850 continuous
Fuel consumption at 70% torque: 280 gallons/hr
Fuel consumption at 130% torque: 402 gallons/hr
6x 23″ x 265″ 250 lbs/ea
Gearbox: 250x reduction helical gear epicyclic, helical bevel gear for coaxial.
System weight and capacity:
Gross take-off weight: 33,000 lbs
Unit empty weight with 1-hour fuel: 10,500 lbs
Net lift capacity: 22,500 lbs
Maximum operating altitude without airspace permission: 400 ft
Maximum non-stop endurance: 24 hours.
Maximum travel distance over ocean or non-populated area: 480 miles, 770 km.
Overall unit width and length: 51′
Overall unit height: 190″
Power module dimensions: 35″ width by 68″ height
Power module weight without rotors: 6700 lbs
Rotor drive module dimensions: 88″ width, 130″ length
Power module with drive module separated can be easily transported in a box truck.
Purchase price: $990,000
Hourly operating cost: $750/hr
Pochari Hydrogen’s in-house development 1000-1500 horsepower turboshaft.