ENERGY ABSORBING EARCUP APPARATUS AND METHOD OF MAKING SAME
20210099788 ยท 2021-04-01
Inventors
Cpc classification
B64D11/0015
PERFORMING OPERATIONS; TRANSPORTING
H04R2420/07
ELECTRICITY
G10K11/17873
PHYSICS
H04R1/1091
ELECTRICITY
H04R2460/11
ELECTRICITY
H04R2201/107
ELECTRICITY
G10K2210/1081
PHYSICS
International classification
H04R1/10
ELECTRICITY
B64D11/00
PERFORMING OPERATIONS; TRANSPORTING
G10K11/178
PHYSICS
Abstract
An energy absorbing earcup apparatus for use in an aviation helmet and a method of making same is disclosed. The apparatus can include an earcup body adapted for positioning on a human ear and containing a speaker adapted to emit sound, and a noise attenuating cushioning member surrounding the earcup body. The apparatus can provide active noise reduction. A vent a vent can be formed in the earcup body to provide ventilation for the speaker, and an opening can be formed in the cushioning member that is in communication with the vent.
Claims
1. An energy absorbing earcup apparatus for use in an aviation helmet comprising: (a) a foam housing having a front side and a back side opposite the front side; (b) a speaker adapted to emit sound positioned within an opening formed in the front side of the housing; and (c) a noise attenuating backing member attached to the back side of the housing.
2. The apparatus according to claim 1, wherein the speaker comprises an electroacoustic transducer operatively connected to an active noise reduction circuit, and the apparatus provides active noise reduction.
3. The apparatus according to claim 1, wherein the housing comprises a closed cell foam.
4. The apparatus according to claim 1, wherein the housing comprises at least one material selected from the group consisting of polyethylene, polyurethane, neoprene, ethylene propylene diene monomer rubber, and polyvinyl chloride and nitrile-butadiene rubber.
5. The apparatus according to claim 1, further comprising a seal member positioned over the speaker.
6. The apparatus according to claim 1, further comprising a fabric covering positioned over the housing.
7. The apparatus according to claim 1, wherein the backing member is comprised of plastic.
8. An energy absorbing earcup apparatus for use in an aviation helmet comprising: (a) an earcup body adapted for positioning on a human ear and containing a speaker adapted to emit sound; and (b) a noise attenuating cushioning member surrounding the earcup body.
9. The apparatus according to claim 8, wherein the apparatus is adapted to provide active noise reduction.
10. The apparatus according to claim 8, wherein the speaker comprises an electroacoustic transducer operatively connected to an active noise reduction circuit,
11. The apparatus according to claim 8, further comprising an active noise reduction microphone positioned in the cushioning member.
12. The apparatus according to claim 8, wherein the cushioning member comprises a closed cell foam.
13. The apparatus according to claim 8, wherein the cushioning member comprises at least one material selected from the group consisting of polyethylene, polyurethane, neoprene, ethylene propylene diene monomer rubber, and polyvinyl chloride and nitrile-butadiene rubber.
14. The apparatus according to claim 8, wherein a vent is formed in the earcup body, wherein the vent provides ventilation for the speaker.
15. The apparatus according to claim 12, wherein an opening is formed in the cushioning member in communication with the vent in the earcup body.
16. The apparatus according to claim 8, further comprising an attachment member positioned on the cushioning member adapted for attaching the apparatus to an aviation helmet.
17. The apparatus according to claim 14, wherein the attachment member comprises a plurality of hook fasteners.
18. An aviation helmet apparatus comprising: (a) a helmet having an interior surface and an exterior surface, the interior surface contacting a user's head when wearing the helmet; (b) an energy absorbing earcup apparatus comprising an earcup body containing a speaker adapted to provide active noise reduction, a noise attenuating foam member surrounding the earcup body and a first attachment member positioned on the cushioning member; and (c) a second attachment member positioned on the interior surface of the helmet adapted for complementary releasable engagement with the first attachment member, the first attachment member engaged to the second attachment member whereby the earcup apparatus is releasably attached to the helmet.
19. The apparatus according to claim 18, wherein the first attachment member comprises a plurality of hook fasteners, and the second attachment member comprises a plurality of loop fasteners.
20. The apparatus according to claim 18, wherein a vent is formed in the earcup body to provide ventilation for the speaker, and an opening is formed in the foam member that is in communication with the vent.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
[0053] An energy absorbing earcup apparatus according to a preferred embodiment of the invention is illustrated in
[0054] The apparatus 10 can include a speaker 20 positioned within an opening 15 in the foam housing 14, as shown in
[0055] An ear seal member 16 is positioned over the speaker 20 and attached to the housing 14, as shown in
[0056] In a method of using the apparatus 10 according to a preferred embodiment of the invention, the earcup assembly 10 is used in a helicopter and/or fixed-wing aircrew helmet. The earcup assembly 10 can be used in military, government and/or civilian helicopters and fixed-wing aircraft. Another embodiment of the invention comprises a helmet, such as a helicopter or fixed-wing aircrew helmet, comprising the apparatus 10.
[0057] An earcup apparatus according to another preferred embodiment of the invention is illustrated in
[0058] According to an embodiment of the invention, the earcup apparatus 100 can be made using a conventional aviation headset. According to the method, a conventional aviation headset 150, such as the communication headset sold by Bose Corporation as the BOSE A20 Aviation Headset is provided. U.S. Pat. No. 8,675,885 is incorporated herein by reference. The headset 150 has an Active Noise Reduction (ANR) circuit and includes wireless communication technology (Bluetooth), volume control, and cell phone integration. The headset 150 is dissembled to remove the boom microphone 152 and the over the head headband 154, leaving Left and Right earcups 160 connected by the crossover cable 140 of the headset 150.
[0059] An additional air vent 120 is formed in the lower portion of each earcup 160, as shown in
[0060] The cushioning members 114 comprise surrounds that can be precision machined or injection molded and are made of a cushioning material. The cushioning surrounds 114 are shaped and sized to receive and conform to the earcups 160. The cushioning surrounds 114 are preferably made of an impact absorbing closed cell foam material. The cushioning surrounds 114 can be made of polyethylene foam, polyurethane foam, neoprene, ethylene propylene diene monomer rubber (EPDM), and/or polyvinyl chloride and nitrile-butadiene rubber (PVC/NBR). An opening 124 is formed in each surround 114, as shown in
[0061] The ANR microphone 156 is removed from each earcup 160 and the wiring harness is extended to allow relocation and integration into each surround 120. The wiring from the ANR microphone 156 can be positioned through the opening 124 of either surround 120, and the ANR microphone 156 can be positioned in the front of the foam surround 124, as shown in
[0062] A layer of Velcro fasteners 116 is applied to the outer surface of each earcup 160. The Velcro fasteners 116 allow direct attachment to the inside of the aviation helmet 180, as shown in
[0063] Each earcup 160 is positioned into one of the foam surrounds 120, as shown in
[0064] The battery pack/control module 158 of the headset 150 is removed from the headset 150 and reattached to the earcup assemblies 110. The battery pack/control module 158 provides an electrical interface for the earcups 160. A modified main cable 148 connects the earcup assemblies 110 to the aircraft intercommunication system via plug 146. A voice communication microphone 130 can be mounted to the aircraft helmet 180 and connected to the earcup assemblies 110 via the battery pack/control module 158 and cable 140.
[0065] The earcup apparatus 100 can be attached to the interior of the helmet 180 by engaging the hook fasteners 116 on the earcup assemblies 110 with complementary loop fasteners positioned on the interior of the helmet 180.
[0066] An energy absorbing earcup apparatus and methods of making and using same are described above. Various changes can be made to the invention without departing from its scope. The above description of preferred embodiments and best mode of the invention are provided for the purpose of illustration only and not limitation.