IL BACKGROUND OF THE INVENTION

1. Field of the Invention.

[001] The present disclosure relates to a safety shield for use in aircraft. More particularly, the present disclosure relates to a safety shield provided for nacelle of an aircraft.

2. Description of the Related Art.

[002] In recent years, a lot of accidental cases are reported with regards to bird aircraft strike hazards in which there is a collision between an airborne animal (like a bird or bat) or foreign particles and an aircraft which is a manmade vehicle. In event of a collision, it is likely that birds or foreign particles are sucked in the mechanical engine provided in nacelle of aircraft which ends up life of birds. Moreover, bird or foreign particles struck with a fan blade of mechanical engine and results in displacement of one blade on another for causing cascading failure. Any failure in engine leads to hazardous accidents which can cause loss of humans and properties.

[003] Several designs of various shield/deflector for shielding nacelle of aircrafts have been designed in the past. None of them, however, include a shield for protecting nacelle of aircraft which is simple in design and provided with ventilations, simplified manufacturing, installing and removing during maintenance. Moreover, the shield provides more stability and secureness. [004] Applicant believes that a related reference corresponds to US patent application 20100287908 filed by Cunningham Ray E. titled ‘Jet engine shield and debris deflector’ discloses a shield device which is aerodynamically shaped in the form of a frustro-conical cylinder and is configured with a series of openings or slots that allow sufficient air to be entrained into the jet engine intake. However, achieving a frustro-conical cylinder and configuring slots thereon is associated with a number of manufacturing complexities. Also, removal and fitment of such aerodynamically shaped shield device can be time consuming.

[001] Another US patent 6883751 filed by Boeing Co. titled ‘Apparatus and method for preventing foreign object damage to an aircraft’ discloses a deflecting member which is coupled to the aircraft between the landing gear and an inlet of the engine so that when the deflecting member is extended, it intersects with a portion of lines of sight between the landing gear and an inlet of the engine. However, providing such long deflecting member extending between gear to inlet of engine is not required as protection is moreover required in the engine area. Such long deflecting member utilizes more material and hampers overall cost.

[002] Other documents describing the closest subject matter provide for a number of more or less complicated features that fail to solve the problem in an efficient and economical way. None of these patents suggest the novel features of the present invention. III SUMMARY OF THE INVENTION

[003] In view of the above, it is an objective of the present invention to solve or at least reduce the problems discussed above. The present invention is a safety shield to be secured with nacelle of aircraft. Safety shield is shaped like nacelle such that nacelle is covered by use of safety shield. Shield frame of safety shield is provided with a plurality of openings of pre-defined size and shape and disposed at desired orientations. Openings facilitate ventilation to a mechanical engine provided in nacelle. Safety shield is connected to nacelle by clamping elements that securely clamps safety shield with nacelle. In operation, safety shield prevents collision of birds and foreign particles with fan blade of mechanical engine and thus saves life and failure of mechanical engine.

[004] It is one of the main objects of the present invention is to provide a safety shield for aircraft nacelle that is simple in design and hence easy to manufacture and provides adequate shielding for airborne animals and foreign particles.

[005] It is another object of this invention is to provide a safety shield for aircraft nacelle that is easy to install and remove for maintenance.

[006] It is another object of this invention is to provide a safety shield for aircraft nacelle that provides adequate ventilation to a mechanical engine provided in nacelle.

[007] It is another object of this invention is to provide a safety shield that is easy to be modified as per different shape and size of nacelle and that is easily retrofitted in existing nacelles or fitted in new nacelles and provides stability and secureness.

[008] Further objects of the invention will be brought out in the following part of the specification, wherein detailed description is for the purpose of fully disclosing the invention without placing limitations thereon.

IV. BRIEF DESCRIPTION OF THE DRAWINGS

[009] With the above and other related objects in view, the invention consists in the details of construction and combination of parts as will be more fully understood from the following description, when read in conjunction with the accompanying drawings in which:

Figure 1 represents a perspective view of a safety shield fitted on a nacelle of an aircraft, in accordance with one embodiment of the present invention.

Figure 2 is a front view of safety shield of Figure 1.

Figure 3 represents a cross-sectional view of safety shield of Figure 1 shielding a mechanical engine provided in nacelle.

Figure 4 represents a perspective view of safety shield fitted on nacelle of Figure 1.

Figure 5 represents an exploded view of safety shield of Figure 1. Figure 6 represents a front view of safety shield of Figure 1.

V. DETAILED DESCRIPTION OF THE EMBODIMENTS OF THE INVENTION

[010] Referring now to the drawings (FIGS. 1 to 6), where the present invention is generally referred to with numeral 10, it can be observed that a safety shield, in accordance with one embodiment, is provided that includes a shield frame 20 and clamping elements 30.

[011] Shield frame 20 is fitted on a nacelle 21 of an aircraft 22. Shield frame 20 is basically a frame with a plurality of openings 21. Size of openings 20a is such that openings 20a provide sufficient ventilation to dissipate heat of a mechanical engine 23 fitted in nacelle 21. Shape of openings 20a can be any desired shape or can be various combinations of shapes. Size and shape of shield frame 20 is complementary to size and shape of nacelle opening such that shield frame 20 can be easily fitted and removed from nacelle 21.

[012] Clamping elements 30 is used to clamp shield frame 20 to nacelle 21. Clamping elements 30 can be bolts or riveted of fasten with screws and the like. In another embodiment, clamping elements 30 can be integral with shield frame 20, for instance, clamping elements 30 can be of size such that clamping elements 30 can be press fitted with nacelle 21. Additionally, adhesives can be used for securing clamping elements 30. Clamping elements 30 are not limited to ones mention herein the present disclosure and any other clamping elements 30 that can easily secure and remove shield 20 from nacelle 21 are within the scope of the present disclosure. [013] In one embodiment, safety shield 10 is made of high quality, heat resistant metal. However, any like suitable material with heat resistant capacity is within the scope of the present disclosure.

[005] In operation, when shield 20 is fitted and secured to nacelle 21 and aircraft is take-off conditions or in-flight conditions, shield 20 provides adequate ventilation to mechanical engine 23 owing to openings 20a provided. Further, during take-off, mechanical engine 23 experiences high speed rotation because of which while flying of aircraft at lower altitude airborne animals are likely to be sucked and/or collide with fan blades 23a of mechanical engine 23 and end-up their lives. Also, fan blades 23a experiences displacement of one blade on another which results in cascading failure. Also, any foreign object when struck results in such cascading failure. Such failure can also occur when aircraft 22 is flying at a higher altitude after take-off. As, shield 20 is secured to nacelle 21 such occurrence of collision/accidents and events is prevented and saves upon life of airborne animals as well as human life travelling in aircraft and also prevents destruction of property. In one embodiment, the shield 20 contains an inner ring and an outer ring. The inner ring may be provided as wider than the outer ring.

[014] Thus, safety shield 10 is simple in design because it is not conventional shield of intricate aerodynamically shape with grooves formed on intricate aerodynamic surface which are difficult to configure. Owing to simple aerodynamic design safety shield 10 is easy to manufacture and also provide adequate shielding for airborne animals for protecting their lives and foreign particles. Safety shield 10 is easy to install and remove for maintenance from nacelle 21. Safety shield 10 provides adequate ventilation to a mechanical engine provided in nacelle 21. Safety shield 10 is easy to be modified as per different shape and size of nacelle 21 and that is easily retrofitted in existing nacelles 21 or fitted in new nacelles. Safety shield 10 thus protects human life and airborne animal life and protects property destruction.

[015] The foregoing description conveys the best understanding of the objectives and advantages of the present invention. Different embodiments may be made of the inventive concept of this invention. It is to be understood that all matter disclosed herein is to be interpreted merely as illustrative, and not in a limiting sense.

VI. INDUSTRIAL APPLICABILITY

[016] The safety shield for an aircraft nacelle has several embodiments for industrial applicability. In one implementation, the shield is installed into commercial aircraft which may fly at heights where encountering flying wildlife is common. The shield will then prevent the flying wildlife from entering the nacelle which prevents engine failure and preserves the life of flying wildlife. Furthermore, in another implementation, the shield is implemented into private aircraft. Pilots may then fit the shield into the existing aircraft in order to achieve the aforementioned benefits. The safety shield is shaped for a nacelle such that the nacelle is covered by use of safety shield. Additionally, the shield frame of the safety shield is provided with a plurality of openings of a pre-defined size and shape which are disposed at desired orientations. Furthermore, the openings facilitate ventilation to a mechanical engine provided within the nacelle. The safety shield is connected to the nacelle by clamping elements that securely clamps the safety shield with the nacelle.