Aircraft braking system

An aircraft braking system including a port formed in a side of an airplane. The port has an openable door disposed therein. The openable door is in operative communication with a computerized hydraulic system of the airplane whereby the openable door will open once the airplane begins a turn and will not close until the turn is complete.

BACKGROUND OF THE INVENTION

The present invention relates to an aircraft braking system and more particularly pertains to reducing g-force pull on a pilot of an airplane to allow for greater maneuverability.

The use of braking systems for airplanes is known in the prior art. More specifically, braking systems for airplanes heretofore devised and utilized for the purpose of reducing the speed of an airplane during flight are known to consist basically of familiar, expected and obvious structural configurations, notwithstanding the myriad of designs encompassed by the crowded prior art which have been developed for the fulfillment of countless objectives and requirements.

While these devices fulfill their respective, particular objective and requirements, these patents do not describe an aircraft braking system for reducing g-force pull on a pilot of an airplane to allow for greater maneuverability.

In this respect, the aircraft braking system according to the present invention substantially departs from the conventional concepts and designs of the prior art, and in doing so provides an apparatus primarily developed for the purpose of reducing g-force pull on a pilot of an airplane to allow for greater maneuverability.

Therefore, it can be appreciated that there exists a continuing need for new and improved aircraft braking system which can be used for reducing g-force pull on a pilot of an airplane to allow for greater maneuverability. In this regard, the present invention substantially fulfills this need.

SUMMARY OF THE INVENTION

In the view of the foregoing disadvantages inherent in the known types of braking systems for airplanes now present in the prior art, the present invention provides an improved aircraft braking system. As such, the general purpose of the present invention, which will be described subsequently in greater detail, is to provide a new and improved aircraft braking system and method which has all the advantages of the prior art and none of the disadvantages.

To attain this, the present invention essentially comprises a port formed in a side of an airplane. The port has an openable door disposed therein. The openable door is in operative communication with a computerized hydraulic system of the airplane whereby the openable door will open once the airplane begins a turn and will not close until the turn is complete.

It is therefore an object of the present invention to provide a new and improved aircraft braking system which has all the advantages of the prior art braking systems for airplanes and none of the disadvantages.

It is another object of the present invention to provide a new and improved aircraft braking system which may be easily and efficiently manufactured and marketed.

It is a further object of the present invention to provide a new and improved aircraft braking system which is of durable and reliable construction.

An even further object of the present invention is to provide a new and improved aircraft braking system which is susceptible of a low cost of manufacture with regard to both materials and labor, and which accordingly is then susceptible of low prices of sale to the consuming public, thereby making such an aircraft braking system economically available to the buying public.

Even still another object of the present invention is to provide a new and improved aircraft braking system for reducing g-force pull on a pilot of an airplane to allow for greater maneuverability.

Lastly, it is an object of the present invention to provide a new and improved aircraft braking system including a port formed in a side of an airplane. The port has an openable door disposed therein. The openable door is in operative communication with a computerized hydraulic system of the airplane whereby the openable door will open once the airplane begins a turn and will not close until the turn is complete.

The same reference numerals refer to the same parts through the various figures.

DESCRIPTION OF THE PREFERRED EMBODIMENT

With reference now to the drawings, and in particular, to FIG. 1 thereof, the preferred embodiment of the new and improved aircraft braking system embodying the principles and concepts of the present invention and generally designated by the reference number 10 will be described.

Specifically, it will be noted in the various Figures that the device relates to a aircraft braking system for reducing g-force pull on a pilot of an airplane to allow for greater maneuverability. In its broadest context, the device consists of. Such components are individually configured and correlated with respect to each other so as to attain the desired objective.

The present invention is essentially comprised of a port 12 formed in a side of an airplane 13 . The port 12 is positioned below the cockpit of the airplane 13 so as to be centrally located with respect to the airplane 13 . The port 12 has an openable door 14 disposed therein. The openable door 14 is in operative communication with a computerized hydraulic system of the airplane 13 whereby the openable door 14 will open once the airplane 13 begins a turn and will not close until the turn is complete. With the openable door 14 in the open orientation, the degree of g-force will be significantly reduced thereby allowing for the turn to be accomplished in an easier manner. The openable door 14 will open between 0 degrees and 90 degrees.