Discharge plate;

[END]

Description:

The muffler assemblies are installed around the aircraft forming a shield. See u.s nonprovisional application 15783601.

The muffler assemblies contain hole(s) for mounting the muffler assemblies to the aircraft via the latching mechanism of the ejection assembly. Therefore the ejection assembly serves as a mounting assembly. And ejection assembly.

The nipple is threaded over the shaft to install. The nipple is inserted into the hole of the muffler assembly to assemble or mount to the aircraft.

To install the muffler assemblies to the aircraft, the muffler assemblies are placed around the nipples of the ejection bars. The mechanic forces pressure against the ejection springs, depressing them towards the aircraft, and another engages electricity to cause the nipple latches to lock inside of the installation holes. The locking completes the installation and spring pressure is retained.

The spring surrounds the shaft of the ejection assembly and coils away from the direction of the aircraft. Immediately after is located the ejection plate which is a disk plate to force spring pressure against the muffler assembly. Away from the aircraft. The disklike structure of the plate surrounds the hollow shaft. The spring end of the contacting disk plate is flat. The structure of the disk plate transitions in shape to progress to be smaller in dimensions at the nipple end or side of the ejection shaft assembly. Thus the nipple when threaded over the end of the shaft will lock and retain the spring and pressure plate surrounding the hollow shaft.

The hollow shaft contains a stream of wires and a wiring harness. The nipple, with hollow male thread, contains a wiring harness.

The wiring harnesses are plugged together to complete the circuit of the latch function of the latching mechanism contained in the nipple assembly. Then the nipple is screwed over the threaded portion of the hollow shaft. The nipple contains sideward holes for the latching parts. The nipple is inserted inside of the holes of the muffler assemblies. The second mechanic engages the circuit to cause the latching pieces to come outward from inside of the nipple to both lock into the muffler assemblies, holding it secure, and doing this also holds open a normally closed circuit internal the muffler assemblies.

The normally closed circuit will ignite the flare packs after the latches are retracted by the pilot. This is timed, computer controlled.

To install the ejection assemblies:

1. The hollow shaft with inside circuit is attached to the aircraft;

2. The pressure spring is placed surrounding the shaft;

3. The disk plate is placed around the endward of the shaft, slightly depressing, with flat area contacting the spring; 4. The wiring harness of the inside of the hollow shaft is connected to the wiring harness of the nipple;

Now, the nipple male hollow thread can be screwed over the female hollow thread of the shaft;

5. The nipple has a hexagonal nut fitting shape at its end, but before the thread. The socket is placed around the entire nipple, locking around the nut portion of its body, to be twisted and torqued to fasten the nipple to the shaft;

6. Now the installation is complete. The spring system is locked around the shaft by the nipple. The circuit is connected by the wire connection.

Therefore the muffler assemblies can be installed around the nipples and the latching, circuit holding pieces of the nipple assembly can hold the muffler assemblies on, and hold the circuit open.

Ariel visual:

The pull switch causes the helicopter to discharge its shield when engaged by the Marshall with precision force. The two pieces will be forced outward from the aircraft and fall as the latch is released. The latch release will cause the circuit to close. The closed circuit will begin the timer. The end of the timer will spark ignition. Ignition to flare packs. The flaring will be done. Throughout the show multiple flare drops vary consistent with paragraph 6.

An Ariel visual is arranged with a plurality of aircraft having said flaring muffler assemblies. This includes one helicopter and 5 outer jet planes.

Planes: A jet plane is described having two jet sources.

A rear oriented jet force is engageable for forward jet flight.

A front orient jet force is engageable for rear jet flight.

Both jet forces are dual engageable for opposing forces to cause a plane to remain still in flight, moving neither forward nor in reverse respective the cosmetic orientation of the aircraft.

This incorporates a computer controlled system regulating equilibrium between the opposing jet forces.

The jets contain muffler assemblies which are likewise dischargeable from the aircraft via a control switch or responsive component.

The following final section describes the performance of multiple arranged aircraft, flare show.

Ariel visual:

Each aircraft is equipped with muffler assemblies packed with said ignition materials wherein the combination of engineered packing, unique to each aircraft, in combination with its assigned, designated, path of flight, produces a combinational, specific, flare show.

To begin. The jets encircle the helicopter in fashion.

They pause as described, sitting stationary surround the helicopter in their center.

Thus, the ceremony begins. The central aircraft remains still, perpetual, in its epicenter coordinate of formation.

The paused jets disconnect their rearward opposing forces and expand in circular formation with the origin flare from the central helicopter trailing behind them. The initial muffler assembly flare style of the first helicopter drop signaling all the others to start the show, will follow the circling jets as they depart and begin flying away from the central chopper. The helicopter remains in its original coordinate position throughout the show timely releasing its set of flare drops. The planes as described, venture outward and away from the center helicopter is visual appeal, manuever synchronized timely formation dropping timed, coordinate fire show drops as they go path.

They (jet planes) gradually motion upward in angular direction of flight, and continue until complete sky bound is achieved while releasing their flare shields. The release of the muffler shields, with flare explosions, causes loud sound.

As paragraph 6, multiple specifically designed drops of multiple rounds of flare are dropped. The sudden initial release of the muffler assemblies from all aircrafts causes an appealing sound increment. The firecrackers too cause noise.

The ritual is done near a shore over a body of water, during the late portions of the end of the sunset. The ashes will fall into the ocean as the crowd observes from land. A vast arraignment and display of sound and lighting is disbound from jet to jet. Description of Drawings:

Figure 1 illustrates the dual jet configuration for the stillplanes.

Figure 2 illustrates the muffler assembly and ejection system.

Figure 3 illustrates installation or an assembly of the ejection system parts.

Figure 4 illustrates installation or an assembly of the muffler assembly to the ejection system.

Figure 5 illustrates a simplified form of what is the basics of the performance ritual, in terms of Ariel team, formation, manuever, and flight path.

Specification:

Multiple muffler assemblies are mounted to the aircraft and are dischargeable from a pull switch located in the cockpit. The muffler assemblies comprises two parts, independently installed on the craft, each assembly(component) containing an arrangement of mufflers that are mounted around the body of the helicopter, surround its body and portion of propeller, thus dampening or removing projected sound while the assemblies remain so attached to the chopper. The planes have them too . pull switch causes electromechanical discharge and ejection of the mounted muffler assemblies. See referenced priority application 15783601 for muffler assemblies. Discharging the assemblies causes a performance style boom of increased roaring sound release.

Flaring:

The muffler assemblies are packed with flaring.

Various types of Chinese traditional lighting configurations are incorporable.

Swirls, combinations of color, boom styles, geometric configurations, and lighting transitional flaring are combined.

The loaded flaring packs of ammunition or ignition material are configured to, when the muffler assemblies are discharged, timely become engaged via an ignition circuit that is normally open in the muffler assembly but becomes otherwise closed pursuant to discharge, causing flare. The ignition circuit is computer controlled for timing. The computer will go with the flaring. All of the vehicles participating in this said ritual contain multiple loads or rounds of flaring independent of the initial or main round consistent with the muffler assemblies. In this ritual, the ships will be controlled by the pilots to sequentially and configurably release multiple waves rounds or repetitions of different drops of firework release sets, throughout the course of the maneuvered performance. Each particular individual flare drop has a different packing style than the others, to intricate performance and entertainment appeal as of variable intricacy. As each aircraft progresses its path as has been well rehearsed, the different flare drop sets change or vary pursuant to the combined Ariel paths of flight, and how the well designed combinations of, different packs of fireworkings will amuse the audience.

The following text will describe the muffler assy, system.

Muffler assembly discharge system:

Pieces:

Aircraft vessel;

Muffler assembly left;

Muffler assembly right;

( see u.s 15783601)

Ejection mechanism(s); [END]

Muffler assembly comprises:

Solid assemblies containing multiple mufflers;

Flare packs;

Mounting hole(s) for ejection mechanism(s);

Ignition circuit for flare packs;

[END]

Ejection mechanism(s) of the aircraft vessel com

Hollow shaft with hollow male thread ending;

Nipple assembly with female thread ending and internal electromechanical latch mechanism;

Shaft wiring harness;

Ejection spring;