Patent Application
20100314180
The present invention relates to a wheeled vehicle adapted for mobilizing aircrafts.
Most modern airplanes have reverse thrust capabilities, mainly for assisting them to slow down the planes, and reducing the landing distance, but not for the purpose of moving out of the parking bay. Due to the fact that there are no ‘reverse’ gears, the airplanes need to be pushed/pulled by a towing vehicle. There are several aircrafts tow-vehicles known in the art. For example, U.S. Pat. No. 5,302,074 discloses a wheeled vehicle for transporting aircraft on the ground, that includes an engagement and hoisting unit supported by a vehicle chassis. The unit is brought into a position close to the nose wheels of the aircraft, both in front of and behind the contact points between the nose wheels and the ground. The unit is lifted by a cylinder acting between it and the chassis and makes contact with the treads of the nose wheels on both sides of the contact points, raising the nose wheels off the ground, thereby allowing to tow the aircraft.
US 20030165375 discloses a traction vehicle, as well as an engagement and hoisting device, which is characterized in that the nose-wheel holder and the stand are shaped as two separate units and comprise members arranged in a circular arc and defining a vertical axis of rotation for these units and that the nose-wheel holder is substantially U-shaped with its opening turned towards the aircraft, when the nose-wheel holder is situated to be moved into a position to receive the nose wheel.
U.S. Pat. No. 6,283,696 discusses an aircraft towing vehicle that includes a lifting and locking device for the nose landing gear of the aircraft being towed. The device has two support elements which reach behind the nose wheels and can be displaced along straight-line guiding rails by a linear drive so as to pull the nose wheels of the aircraft onto a lifting platform and to lock it into place thereon. At the end of each guiding rail a guiding pin is provided which, in cooperation with a guiding track embodied in the support element, controls the rotation of the support element into a release position in which the nose landing gear is able to pass through.
All the above described tow-vehicles, as well as other tow-vehicles known in the art are attached to the nose wheel(s). Unfortunately, there are several drawbacks associated with this approach, e.g. requirement for a wide steering angel, applying extensive towing load upon the front undercarriage which is not designed for such loads and is sensitive to fatigue effects, etc. Such solutions are not suitable whenever longer towing, for example to the beginning of the runway, is required. In order to accommodate this problem the normal solution is the use of the planes' own engines while taxiing the long distance.
The present invention seeks to provide a solution that eliminates these problems.
It is an object of the present invention to provide a mobilizing device for use in moving airplanes either for short distances, e.g. at the airport gate vicinity, and/or for longer distances, e.g. till the start of the runway.
Other objects of the invention will become apparent as the description of the invention proceeds.
According to a first embodiment of the present invention there is provided a mobilizing apparatus for moving an airplane positioned on the ground, wherein the mobilizing apparatus comprises at least one pair of main wheels and engagement means, and is characterized in that the engagement means is adapted to enable engagement of the mobilizing apparatus to the airplane so that the axis along which the at least one pair of the mobilizing apparatus main wheels is essentially located, is along an axis formed between the central wheels of the airplane to be moved, so that the mobilizing apparatus main wheels are positioned essentially parallel to a virtual axis or a plurality of virtual axis connecting respective airplane central wheels upon engaging the mobilizing apparatus to the airplane to be moved. Preferably, the mobilizing apparatus is further characterized in that once it is engaged to the airplane, there is no substantial steering movement of the mobilizing vehicle relative to the airplane.
According to a preferred embodiment of the invention, the mobilizing apparatus further comprises at least one front wheel. Preferably, the at least one front wheel is a caster wheel. The term “caster wheel” as used herein and throughout the specification and claims, is used to denote a wheel that may be moved in any direction without affecting the direction at which the mobilizing apparatus itself is moving.
By yet another preferred embodiment of the invention, the mobilizing apparatus further comprises harness means to enable harnessing the front portion of the mobilizing apparatus to the airplane's front undercarriage.
According to another preferred embodiment, the mobilizing apparatus is further adapted to allow the airplane and the mobilizing apparatus being engaged thereto, to be steered by a person located at the airplane's cockpit. Preferably, the steering of the airplane and the engaged mobilizing apparatus by the person located at the cockpit is done by steering the airplane front undercarriage.
As will be appreciated by those skilled in the art although the steering of the airplane with the mobilizing apparatus attached thereto is done via the airplane front wheel, still, the load of moving the airplane's major mass is undertaken by the at least one pair of main wheels of the mobilizing apparatus.
According to another preferred embodiment of the invention, the at least one pair of main wheels are jointly driven. By this embodiment the driving force is divided between each of the at least one pair of main wheels in accordance with current driving conditions (e.g. turns to be taken, etc.). Such joint drive could be mechanical differential or hydraulic system (where the supply of the hydraulic fluid is common to all of mobilizing apparatus main wheels), or any other type of joint drive that is known in the art per se.
The present invention will be understood and appreciated more fully from the following detailed example taken in conjunction with the drawings.
Let us consider now the example illustrated schematically in
The mobilizing vehicle 100 further comprises engagement means 130 to allow engaging the vehicle to the airplane. The engagement means could be any suitable means that are known in the art per se, not necessarily similar to those illustrated in this Fig., but preferably such that would allow 3 degrees of freedom via the airplane's back/rear undercarriage. The can be engaged with the airplane's central undercarriage or to the rear undercarriage as illustrated in the example of this Fig. The mobilizing vehicle main task is to allow the whole system (i.e. the airplane+mobilizing vehicle) to move fast or slow, in the forward or backward direction, while the steering of that system is preferably done from the cockpit by the pilot of the airplane, using the airplane's own steering system. The engagement means are characterized in that it allows the engagement of the mobilizing vehicle and the airplane to each other without relative steering motion between the body of the mobilizing vehicle and the airplane.
The mobilizing vehicle may further comprise one or more front wheels (not shown in this Fig.), which are typically caster wheels used primarily to provide required stability for the mobilizing vehicle while being driven.
The mobilizing vehicle may further comprise a driving station 140 for a driver/operator to drive the vehicle.
This arrangement allows moving the airplane for short drives typically of tens of meters (e.g. from its parking position to the airport gate, or to a point at which the airplane starts moving by using its own engines) or for longer drives typically hundreds of meters up to a couple of kilometers or so (e.g. till the start of the runway).
Let us now consider another example as illustrated in
It is to be understood that the above description only includes some embodiments of the invention and serves for its illustration. Numerous other ways of carrying out the methods provided by the present invention may be construed by a person skilled in the art without departing from the scope of the invention, and are thus encompassed by the present invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 199333 | Jun 2009 | IL | national |
