Sub Menu: GENESIS - Aircraft Design Details
Introduction
Multipurpose Landing Gear
Telescopic Wing
Interconnected Propeller Drive
Modular Fuselage
Simplicity of Operation
Aerodynamics
Design Verification
Specifications
Comparison to the Competition
Safety
Reliability
Market
Frequently Asked Questions
Conclusion
Patents
Safety
Gevers Aircraft, Inc. * GENESIS *
Numerous innovations make this the safest aircraft ever built.
Telescopic Wings:
The extended wing lowers the stall speed, takeoff distance, landing distance, landing energy, glide angle, and increases the climb rate, climb angle, ceiling, glide distance, range, and endurance.
The retracted wing (in cruise) is much stronger than conventional designs.
Short wing and high wing loading improves tolerance to gust loads and improves ride quality.
In cruise, the outer half of the wing is protected from ice accumulation and is exposed only for landing.
Landing Gear:
Takeoff and landing crosswind limitations are nearly eliminated.
There is no maximum gear extend or retract speed.
The main gear is on the aircraft centerline so that any component failure does not cause directional control problems.
The pilot can see the gear and determine configuration and condition from his seat.
A gear-up or a water configuration landing on hard surface only effects the reinforced, removable ski panels. Prop tips do not touch the ground.
A water configuration landing on snow does no damage.
A gear-up landing on water or snow does no damage.
A ski-down landing attempt on hard surface or water gives the pilot a warning in time to abort. And if he continues, the damage is minimal.
The landing gear is attached to the engine mounts, so the main landing shock loads do not transfer through wing spars or fuselage.
Engine and Prop. Mounts, and Drive System:
Both props automatically provide equal thrust in the event of an engine failure.
The pilot has a greatly reduced work load during takeoff. He is not required to look in the cockpit for power reductions.
The rotational inertia is lower than conventional twin engine aircraft.
The engines are easily temperature controlled on the ground and in the air.
The engines are isolated from out of balance forces, gyroscopic forces, and object strike forces of the props.
The props are isolated from power pulses of the engines.
An overspeeding prop does not overspeed the engine.
Bystanders and passengers are protected from the props during ground operations.
In the event of a prop failure, the prop thrust lines can be brought close together to minimize asymmetric thrust.
The low CG due to the internal fuselage mounted engines improves the safety of high speed taxi turns - on land, snow, and water.
More available thrust than conventional aircraft during engine failure.
Little pilot action is required after an engine failure, and no tasks inside the cockpit.
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GENESIS SECTION SUB MENU:
Introduction
..
Multipurpose Landing Gear
..
Telescopic Wing
..
Interconnected Propeller Drive
..
Modular Fuselage
..
Simplicity of Operation
..
Aerodynamics
..
Design Verification
..
Specifications
..
Comparison to the Competition
..
Safety
..
Reliability
..
Market
..
Frequently Asked Questions
..
Conclusion
..
Patents
Contact Gevers Aircraft by e-mail at <
mgevers@iquest.net
>