CN201334115Y

CN201334115Y - Ascensional force bay-type aircraft

Info

Publication number: CN201334115Y
Application number: CNU2008202117823U
Authority: CN
Inventors: 王洪涛
Original assignee: Individual
Current assignee: Individual
Priority date: 2008-12-24
Filing date: 2008-12-24
Publication date: 2009-10-28
Anticipated expiration: 2018-12-24

Abstract

The utility model discloses an ascensional force bay-type aircraft. An aircraft body is divided into an upper bay and a lower bay through a horizontal partition board in the aircraft body; a plurality of partition boards perpendicular to the horizontal partition board are arranged in the lower bay so that the lower bay is divided into a plurality of small bays; and power operation rooms are arranged at the rear end part of the upper bay and at the middle part of the lower bay respectively. The utility model has the advantages of compact structure and reasonable design, can adopt any energy sources, can adjust the bays with different conditions in the flying process in the air, and achieves the purposes of adjusting the balance of the aircraft, increasing ascensional force, hovering in the air and the like due to the change of the ascensional force generated by the bays through an operating device according to different conditions, such as chaotic airflow, unusual weather, insufficient fuel and the like, encountered in the flying process. The aircraft can adjust the ascensional force of the bays when taking off and landing, enables the ascensional force provided by the bays to adapt to the weight of the aircraft to match the power of the aircraft, and achieves the effect of short distance take-off and landing or vertical take-off and landing.

Description

Lift compartment-type aircraft

Technical field

The utility model relates to a kind of aircraft, especially a kind of aircraft that lift can be provided voluntarily.

Background technology

At present, various aircraft are arranged in the world, as aircraft, helicopter, spacecraft, dirigible or the like, but aircraft, airship all can not provide static lift, the stream pressure that needs to rely on constantly motion to produce produces lift, need the landing of suitable exacting terms ability, the complicated operation difficulty, consumes energy is serious, seriously polluted, load carrying ability is all very little, and is very uneconomical, though the lift that the enough air bags of dirigible energy provide flies, but the air bag of dirigible is soft, not firm, closed performance is poor, and cost is high, the usage condition harshness, to cargo hold and main cabin the very big influence of formation is set, the landing of dirigible and the ability that adapts to flight are also had very big influence, can't resemble and take off apace and under complex conditions, fly the aircraft.

Summary of the invention

The purpose of this utility model is to overcome the weak point that exists in the above-mentioned technology, and a kind of compact conformation, reasonable in design is provided, and lift is strong, and delivery power is big, but vertical takeoff and landing, the lift compartment-type aircraft of hovering.

In order to achieve the above object, the technical solution adopted in the utility model is: have horizontal baffle that the aircraft body is divided into upper and lower cabin in the aircraft body, polylith is being arranged perpendicular to horizontal baffle in the cabin down, to descend the cabin to be divided into a plurality of cuddies, be respectively equipped with the power operation chamber in rearward end position, last cabin and middle part, following cabin.

The utility model has the advantages that:

(1) compact conformation, reasonable in design can use any energy;

(2) the utility model aircraft aloft in-flight, can regulate separation along with the difference of situation, the different situations that run into during according to flight, as random air-flow, anomalous weather, lack of fuel or the like, the lift variation that separation is produced by operating control, reach and regulate the aircraft balance, increase lift, the purpose of aloft hovering or the like;

(3) landing of the utility model aircraft the time, can regulate the lift of separation, the lift that allows separation provide adapts to the weight of aircraft, cooperates the power of aircraft, reaches the effect of short distance or vertical takeoff and landing.

Description of drawings

Fig. 1 is the utility model structural representation;

The specific embodiment

Below in conjunction with accompanying drawing embodiment of the present utility model is described in further detail.

As shown in Figure 1, there is horizontal baffle 2 that aircraft body 1 is divided into upper and lower cabin 3,4 in the utility model aircraft body 1, polylith is being arranged perpendicular to horizontal baffle 5 in the cabin 4 down, to descend cabin 4 to be divided into a plurality of cuddies, be respectively equipped with power operation chamber 6 at position, 3 rear end, last cabin and 4 middle parts, following cabin.

The utility model is provided with the separation that lift can be provided for aircraft in aircraft inside, by the device that separation is handled, in separation, add lighter-than-air gas such as hydrogen, helium, or the air in the heating separation, with the air of discharging in the separation, make vacuum or the like method, allow separation produce the such lift of meteorologic balloon, for whole aircraft provides lift.The number of separation and lift size can be regulated, and can increase along with the requirement of different aircraft, to reach the purpose of infinitely increasing load carrying ability.When aircraft does not need such big lift, can use these alternate holds personnel and goods.If speed there is the aircraft of requirement, can when design, reduce the quantity of separation, allow separation being equal in weight or only offsetting the part load carrying ability because of the lift that hydrogen, helium or hot gas produced that adds and aircraft self, and the more lift that aircraft needs, during then by aircraft flight because of speed on the wing or the lift that produces on the rotor provide.Less or the aircraft that reduced of this separation, volume is little, and speed is fast, and flare maneuver is flexible.If it is low and to the demanding aircraft of load carrying ability to rate request, can when design, increase the quantity of separation, perhaps increase the hydrogen, helium, the hot gas that add in the separation, increase the lift that separation provided, allow the lift of whole aircraft all provide by separation, and the power of aircraft only is used to provide the power of flight, handles the attitude of flight.

Claims

1. lift compartment-type aircraft, comprise dividing plate, it is characterized in that: have horizontal baffle (2) that aircraft body (1) is divided into upper and lower cabin (3), (4) in the aircraft body (1), polylith is being arranged perpendicular to horizontal baffle (5) in the cabin (4) down, to descend cabin (4) to be divided into a plurality of cuddies, be respectively equipped with power operation chamber (6) at position, rear end, last cabin (3) and middle part, following cabin (4).