Plane Saddle for a Safety Airplane

**NEW PRODUCT FOR LICENSING, MANUFACTURING, and/or INVESTORS**

New Product:

PLANE SADDLE FOR A SAFETY AIRPLANE

U.S. Patent : # 5,568,903

Inventors: Jesus S. Pena, Julia M. Williams, and Joe L. Williams

As attorney for the inventor of an innovative Plane Saddle for a Safety Airplane we are currently seeking manufacturing companies to license, purchase patent rights or enter into a royalty agreement for this timely invention.

This unique device allows the pilot in the cockpit to release the saddle portion (containing the passengers and crew) of the airplane from the carrier portion (wings and engines) in a time of emergency during flight, such as plunging to earth and crashing. When the saddle portion is deployed, four parachutes gently lower it to the ground, avoiding disaster. In addition, a pair of stabilizing reverse thrust engines are mounted on opposite sides of the fuselage of the saddle portion, so as to accelerate release of the saddle portion from the carrier portion.

Objects of the present invention:

to provide a plane saddle for a safety airplane that contains a saddle portion having the cabin and cockpit therein, which will separate from the carrier portion having the wings and engines when there is a problem during flight
to provide a plane saddle for a safety airplane whereby when danger is perceived, the pilot in the cockpit can release the saddle portion from the carrier portion and deploy four parachutes, to gently lower the saddle portion to the ground
to provide a safety device for airplanes that is simple and easy to use and economical in cost to manufacture

Now for the first time the unique Plane Saddle for a Safety Airplane is available to companies worldwide. Of major importance is the low manufacturing cost of the Plane Saddle for a Safety Airplane as compared to other such devices.

LIST OF REFERENCE NUMERALS
10 safety airplane	48 horizontal stabilizer of 28
12 carrier portion of 10	50 elevator on 48
14 saddle portion of 10	52 rail on 24
16 retaining assembly	54 sleeve on 32
18 releasing structure	56 locking facility
20 gently lowering paraphernalia	58 socket in 52
22 ground	60 aperture in 54
24 lower fuselage of 12	62 harness in 32
26 nose core of 24	64 pin
28 wing on 24	66 solenoid in 62
30 engine on 28	68 emergency actuating switch in 36 to 66
32 upper fuselage of 14	70 stabilizing reverse thrust engine of 18 on 32
34 cabin in 32	72 first storage compartment in 32
36 cockpit in 32	74 second storage compartment in 32
38 tail assembly on 32	76 extraction parachute in 72, 74
40 aileron on 28	78 third storage compartment in 32
42 flap on 28	80 fourth storage compartment in 32
44 vertical tail fin of 28	82 recovery parachute in 78, 80
46 fudder on 44	intentionally not used

If you are interested in licensing, purchasing the rights to the above invention or entering into a royalty agreement please contact the office of Michael I. Kroll as follows:

Michael I. Kroll
171 Stillwell Lane
Syosset, New York 11791
Tel. #: 800-367-7774
Tel. #: 516-367-7777
Fax #: 800-367-7704
Fax #: 516-692-2787
E-Mail patent@invention.net

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