JPH04331697A - Aircraft - Google Patents

Abstract

PURPOSE:To meet a wide variety of airlift objects even if not providing various air-frames by holding a self-propelled vehicular part with the airlift objects in a recess and airlifting it by means of an aircraft part. CONSTITUTION:An airframe is divided into an aircraft part 1 and a self- propellable vehicular part 2 with airlift objects, while a recess space for slinging this vehicular part 2 is installed in a lower part of the aircraft part 1, and each hook 1a for slinging the vehicular part 2 is installed in all directions. when these airlift objects are passengers, these passengers are carried up to the aircraft part 1 from a terminal or a departure by the vehicular part 2 for passenger use, and the vehicular part 2 is slung up in the recess space via the hook 1a and a hook receiver 2 and airlifted as it is, and after landing, the vehicular part 2 is separated, carrying passengers directly to the terminal or the destination.

Description

[Detailed description of the invention]

0001

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a multipurpose aircraft.

0002

2. Description of the Related Art FIG. 3 is an explanatory diagram of the structure of a conventional aircraft. In the figure, conventional aircraft are manufactured specifically for passenger use, cargo use, livestock use, fuel use, etc., depending on the type of object to be transported by air, and are modified when repurposed. In addition, objects to be transported by air are transported to an aircraft by a bus, truck, forklift, etc., and loaded thereon, and after being transported by air, they are transferred to a bus, truck, forklift, etc., and transported to the destination.

0003

As mentioned above, in conventional aircraft, the structure of the aircraft is limited depending on the purpose, and it is necessary to prepare various types of aircraft depending on the objects to be transported by air. Furthermore, it takes a considerable amount of time to transport the objects to be transported by air to the aircraft, load them, and transfer them again.

0004

[Means for Solving the Problems] An aircraft according to the present invention aims to solve the above-mentioned problems, and includes a vehicle part that stores an object to be transported by air and moves on its own, and a vehicle part that is suspended in a recess to be transported by air. It is characterized by a configuration with an aircraft part.

[0005]

[Function] That is, in the aircraft according to the present invention, the vehicle part that stores the object to be transported by air and moves on its own is suspended in a recess by the aircraft part and transported by air, and various vehicle parts are prepared. It is possible to handle various types of airlifted objects, and the vehicle part can be lifted from the departure point by an aircraft midway with the airlifted objects on board, and transported by air, and can continue to the destination after landing. Therefore, there is no need to transship the airlifted items en route.

[0006]

DESCRIPTION OF THE PREFERRED EMBODIMENTS FIGS. 1 and 2 are structural diagrams of an aircraft according to an embodiment of the present invention. In the figure, the aircraft according to this embodiment can be used for a variety of purposes, and can eliminate loading and transshipment of objects to be transported by air.
As shown in FIG. 1, the fuselage is divided into a conventional aircraft part 1 and a self-propelled vehicle part 2 that stores objects to be transported by air. A concave space for suspending the vehicle part 2 is provided below the aircraft part 1, and hooks 1a for suspending the vehicle part 2 are provided at a total of four locations on the front, rear, left and right sides of the concave space. Also, although not shown, there are legs and wheels for takeoff and landing at the front and rear of the space. In addition, the vehicle part 2 is provided with hook receivers 2a at a total of four locations on the front, rear, left and right sides corresponding to the hooks 1a on the upper side, and on the lower side, hook receivers 2a are provided at four locations corresponding to the hooks 1a.
b is attached retractably and suspended within the concave space of the aircraft part 1 via a hook 1b and a hook receiver 2b so that its lower surface forms the same plane. In addition to this, efforts are being made to reduce air resistance during air transport.

As shown in FIG. 2, the vehicle part 2 has various structures depending on the purpose, and the passenger vehicle part 2 shown in FIG. 2(a) has improved airtightness, Sufficient consideration has been given to the suspension so that it can be driven on ordinary roads. Further, the cargo vehicle portion 2 shown in FIG. 2(b) is provided with a cargo lashing ring or the like inside, so that the cargo is secured when loading the cargo. In addition, the vehicle portion 2 for livestock shown in FIG. 2(c) is provided with a partition wall inside the loading platform to prevent the livestock from becoming violent during air transport, and is also designed to be airtight. In addition, the vehicle part 2 for fuel shown in FIG.
At the same time as the fuel is being transported by air, the fuel pipe 2c is connected to the aircraft section 1.
Fuel can also be supplied by connecting to the

[0008] As described above, this aircraft is divided into an aircraft part 1 and a self-propelled vehicle part 2, and the vehicle part 2 can be used for passengers, cargo, livestock, fuel, etc. depending on the type of object to be transported by air. If the object to be transported by air is a passenger, the passenger vehicle section 2 transports the passenger from the terminal or departure point to the aircraft section 1.
After landing, the vehicle part 2 is suspended from the concave space of the aircraft part 1 via the hook 1a and the hook receiver 2a, and after landing, the vehicle part 2 is removed and passengers can be transported directly to the terminal or destination. can. Also,
When the object 2 to be transported by air is baggage, livestock, or fuel, the cargo is similarly loaded into the dedicated vehicle section 2 and transported to the aircraft section 1.
After landing, the vehicle part 2 can be removed and the cargo can be transported directly to the destination.

[0009] Therefore, there is no need to prepare various types of aircraft depending on the type of object to be transported by air, but instead, it is sufficient to prepare various types of vehicle parts 2. In addition, by loading cargo onto the vehicle section 2 of the aircraft section 1 in advance, the next flight can be made immediately by simply replacing the vehicle section 2 upon arrival. In addition, since the vehicle part 2 can pick up passengers and luggage directly from the departure point and unload them at the destination,
There is no need for transshipment. In addition, vehicle part 2 for fuel
By using , the waiting time and effort for refueling is eliminated.

0010

[Effects of the Invention] The aircraft according to the present invention is configured as described above, and can handle various airborne objects by preparing various vehicle parts, so there is no need to prepare various aircraft bodies. . Also, considerable time is saved as there is no need to transship the airlifted objects en route.

[Brief explanation of drawings]

FIG. 1 is a front view of an aircraft according to an embodiment of the present invention.

FIG. 2 is a front view of the self-propelled vehicle portion.

FIG. 3 is a front view of a conventional aircraft.

[Explanation of symbols]

1 Aircraft part 1a Hook 2 Vehicle part 2a Hook holder 2b Wheels 2c Fuel piping

Claims (1)

[Claims] 1. An aircraft comprising: a vehicle part that stores an object to be transported by air and moves on its own; and an aircraft part that suspends the vehicle part in a recess and transports it by air.