HORUS - The Modular Aircrew Helmet System

Abstract

Systems and methods are disclosed herein for a Horus flight helmet is for pilots to be used in general, transport and long-range aviation. The invention includes an impact resistant helmet; the invention has high noise reduction system and helps to hear the clear message even in high noise environment. The visor come in as MBU-20/P Oxygen Mask trim in different colors. By keeping in mind, the safety of the pilots we have used energy-absorbing, pressure molded, low density, expanded-polystyrene, had been increased in thickness, secure fixing of helmet on the head of the pilot is provided, comfortable wearing due to the helmet's smaller size and better alignment.

Claims

I: A new modular aircrew helmet system comprising: Helmet shell; Helmet retention system; Helmet visors; Helmet pads and liners; Helmet gaskets and Helmet other components and features.

II: The Flight Helmet Shell as per claim I, is manufactured with: aviation-grade epoxy resin Carbon/Kevlar prepreg; reinforced with Zylon PBO aramid fabric inserts; Helmet Shell target weight 300 gr+/50 gr; Ready to Fly helmet target weight 850 gr+/50 gr and Helmet shell meets or exceeds MIL-DTL-87174/A, MIL-DTL-87174/A and EN996 impact protection.

III: A Helmet retention system as per claim I, comprised of Kevlar fire retardant webbing type chin retention system with side steel plates which is matched with a quick-release self-extinguishing micrometric adjustment buckle.

IV: A single helmet visor system manufactured using: a 2.0 mm Lexan; Polycarbonate with anti-scratch/antifog coating; a locking visor system, plus a quick-release down position locking safety system, is provided; the Visors are available in standard 70% dark finishing, clear, high contrast, iridium colors; and no tools needed to remove and replace the visor system or to add the visor cover assy.

V: A helmet pads and liner system according to claim I; A Fire retardant treated MTP foam core in different thicknesses with coolmax padded fabric; A liner is provided to adjust the helmet to the different head sizes, enhancing comfort; A Kevlar fire retardant thread is used in all liner stitching; A 3D mesh is placed in the helmet ventilation areas to increase airflow ventilation.

VI: A helmet with helmet gasket and other components as per claim I, including: components made with self-extinguishing plastic; Visor plates screws are made of 7075 CNC machined aluminum with anodized finish; Communication setup made in accordance with the customer and radio setup: Mil use setup 5-8 ohm/Civil use up to 300 ohm; Integrated speaker volume control; Integrated CEP system; Compatible with MBU-12/MBU20 oxygen Mask; Removable Maxillo Facial protection; Removable Visor cover with NVG quick release plate; Quick-release NVG plate for F4949 NGV and Integrated action cameras attaching points with removable lightweight.

Description

DETAILED DESCRIPTION OF DRAWINGS

[0028] FIG. 1 depicts a right perspective view of the present invention.

[0029] FIG. 2 depicts a right perspective view of the present invention.

[0030] FIG. 3 depicts the assembly in its opened form as per preferred embodiments of the invention.

[0031] FIG. 4 depicts the assembly back perspective view as per preferred embodiments of the invention.

[0032] FIG. 5 depicts the assembly communication system in open form as per preferred embodiments of the invention.

[0033] FIG. 6 depicts the assembly communication system in closed form as per preffered embodiments of the invention.

DETAILED DESCRIPTION

[0034] Detailed descriptions of the preferred embodiment are provided herein. It is to be understood, however, that the present invention may be embodied in various forms. Therefore, specific details disclosed herein are not to be interpreted as limiting, but rather as a basis for the claims and as a representative basis for teaching one skilled in the art to employ the present invention in virtually any appropriately detailed system, structure or manner.

[0035] The current invention in its preferred embodiment discloses an efficient system of Aircrew Flight Helmet System which is available in different configurations to suit a full range of mission needs

[0036] To develop the design of the helmet of the pilot helmet that would ensure reliable fastening and fixing a helmet in the pilot's mind, ease of use at various evolutions aircraft mounted thereon different equipment. In this case the helmet should have a minimum size, the minimum weight and high strength.

[0037] The present invention is an Aircrew Flight Helmet System is available in different configurations to suit a full range of mission needs. The lightweight flight helmet shell is constructed from Carbon Kevlar Epoxy Matrix, reducing head-borne weight while maintaining reliable strength and durability. This technologically advanced system provides pilots with a decisive edge in combat and in every day flights by reducing fatigue, so they may perform more High-G missions per day without compromising awareness and performance.

[0038] The invention as per its additional embodiments The HORUS Flight Helmet Shell is made of aviation-grade prepreg Kevlar and Carbon fiber with Zylon PBO aramidic fiber inserts in the stressed areas to maximize the impact and the perforation resistance. The helmet shell is vacuum bagged and heat-treated using the autoclave cycle to enhance the product strength and reduce the final shell weight.

[0039] The HORUS Flight Helmet Crash protection element is made of high-density polystyrene EPS with excellent impact absorption properties. The comfort lining is made with MTP foam covered with padded coolmax soft fabric in two different thicknesses, coupled with a 3D mesh fabric area to promote and enhance airflow ventilation. The complete liner and internal paddings could be easily removed, washed, reinstalled, or replaced with no tools.

[0040] The Retention System as per its preferred embodiments is The HORUS Flight Helmet Retention System consists of a padded high strength, a fire-resistant Kevlar chinstrap paired with side steel plates, and a self-extinguishing quick release micrometric adjustment buckle easily removable for helmet maintenance and buckle replacement.

[0041] The Polycarbonate Visors as per its further embodiment is the HORUS Flight Helmet Visor is a 2.0 mm thick polycarbonate with anti-scratch/antifog treatment. A visor vertical position end of travel adjustment is provided. There is no visual distortions, excellent material light transmittance, prismatic powers, and refractive resolution. Visors are available in standard 70% dark contrast, natural clear, and high contrast. The Iridium visor treatment is available in various colors. By special request, the antilaser treatment is available. No tools are needed to remove and replace the visor assy and the visor cover.

[0042] The Removable Visor Cover as per its further embodiments is manufactured with aviation-grade prepreg epoxy resin carbonKevlar, easy to install with no tools, is designed to protect the visor from scratches. It can be paired with an ANVIS mounting quick release plate. The quick-release plate can also be used to install an NGV system or an action recording camera.

[0043] The Horus Ventilation System as per its additional embodiments has been designed to enhance the pilot's performance, to allow perfection of proprietary ventilation system.

[0044] The system, combined with the 3D Mesh fabric in the helmet liner, mitigate the heat and the moisture accumulation inside the helmet shell, avoiding the sweat and heat that impairs the pilot performance under G-loads.

[0045] The Present invention is an Aircrew Flight helmet system for pilots to use in combat and in every day flights which will help them reduce fatigue, which results in better performance. The Flight Helmet is an exclusive active ventilation system combined with the soft Coolmax internal helmet liner enables the pilot to regulate the temperature inside the flight helmet during cold or hot weather, minimizing moisture retention inside the flight helmet. Several key features are in the helmet such as; Customizable Visor, Optimal Respiratory Integration, Visor Cover and NVG kit, Configurable Communication System. It is also equipped with the most modern materials, solutions, production process to enhance the weight, the ergonomy and the noise reduction.

[0046] While a specific embodiment has been shown and described, many variations are possible. With time, additional features may be employed. The particular shape or configuration of the platform or the interior configuration may be changed to suit the system or equipment with which it is used.

[0047] Having described the invention in detail, those skilled in the art will appreciate that modifications may be made to the invention without departing from its spirit. Therefore, it is not intended that the scope of the invention be limited to the specific embodiment illustrated and described. Rather, it is intended that the scope of this invention be determined by the appended claims and their equivalents.

[0048] The Abstract of the Disclosure is provided to allow the reader to quickly ascertain the nature of the technical disclosure. It is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims. In addition, in the foregoing Detailed Description, it can be seen that various features are grouped together in various embodiments for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed embodiments require more features than are expressly recited in each claim. Rather, as the following claims reflect, inventive subject matter lies in less than all features of a single disclosed embodiment. Thus, the following claims are hereby incorporated into the Detailed Description, with each claim standing on its own as a separately claimed subject matter.