Variable-thickness windshield

Patent metadata

Field	Value
Publication number	US-10023289-B2
Application number	US-201615044974-A
Country	US
Kind code	B2
Filing date	Feb 16, 2016
Priority date	Mar 10, 2015
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

According to one embodiment, a rotorcraft front windshield comprises an optically-transparent material having a non-uniform thickness profile such that the front windshield is a first thickness at a first position and a second thickness at a second position, the first thickness being different from the second thickness.

First claim

What is claimed is:

1. A rotorcraft, comprising:
a body;
a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source;
a hub;
a rotor blade coupled to the hub; and
a front windshield coupled to the body, the front windshield having a non-uniform thickness profile, wherein the front windshield comprises a plurality of thickness zones and a plurality of corners, and wherein:
a first thickness zone having a first thickness comprises an upper outboard corner of the front windshield, wherein the upper outboard corner includes, at least in part, an edge of the front windshield;
a second thickness zone having a second thickness comprises other corners of the front windshield, wherein the other corners include, at least in part, the edge of the front windshield, and the second thickness is smaller than the first thickness; and
a third thickness zone having a third thickness comprises a center portion of the front windshield, and the third thickness is smaller than the second thickness.

2. The rotorcraft of claim 1 , wherein the front windshield comprises a single, continuous, uninterrupted material for the plurality of thickness zones.

3. The rotorcraft of claim 1 , wherein the non-uniform thickness profile comprises gradual transition portions between each of the plurality of thickness zones, the gradual transition portions providing transitions between the plurality of thickness zones.

4. The rotorcraft of claim 1 , wherein the first thickness is at least twice as thick as the third thickness.

5. The rotorcraft of claim 1 , wherein the front windshield is fixably coupled to the body.

6. The rotorcraft of claim 1 , wherein the front windshield comprises an optically-transparent material.

7. The rotorcraft of claim 6 , wherein the optically-transparent material is polycarbonate.

8. A windshield, comprising:
an optically-transparent material having a non-uniform thickness profile and a plurality of thickness zones; and
a plurality of corners, wherein:
a first thickness zone having a first thickness comprises an upper outboard corner of the windshield, wherein the upper outboard corner includes, at least in part, an edge of the windshield;
a second thickness zone having a second thickness comprises other corners of the windshield, wherein the other corners include, at least in part, the edge of the windshield, and the second thickness is smaller than the first thickness; and
a third thickness zone having a third thickness comprises a center portion of the windshield, and the third thickness is smaller than the second thickness.

9. The windshield of claim 8 , wherein the optically-transparent material is a single, continuous, uninterrupted material for the plurality of thickness zones.

10. The windshield of claim 8 , wherein the non-uniform thickness profile comprises gradual transition portions between each of the plurality of thickness zones, the gradual transition portions providing transitions between the plurality of thickness zones.

11. The windshield of claim 8 , wherein the first thickness is at least twice as thick as the third thickness.

12. The windshield of claim 8 , wherein the optically-transparent material is polycarbonate.

13. The rotorcraft of claim 1 , wherein the plurality of thickness zones includes a fourth thickness zone having a fourth thickness that is less than each of the first thickness and the second thickness and is greater than the third thickness.

14. The rotorcraft of claim 13 , wherein the plurality of thickness zones includes a fifth thickness zone having a fifth thickness that is less than each of the first thickness, the second thickness, and the fourth thickness and is greater than the third thickness.

15. The rotorcraft of claim 14 , wherein the fourth thickness zone is, at least in part, between the second thickness zone and the fifth thickness zone.

16. The rotorcraft of claim 15 , wherein the fifth thickness zone is, at least in part, between the fourth thickness zone and the third thickness zone.

17. The windshield of claim 8 , wherein the plurality of thickness zones includes a fourth thickness zone having a fourth thickness that is less than each of the first thickness and the second thickness and is greater than the third thickness.

18. The windshield of claim 17 , wherein the plurality of thickness zones includes a fifth thickness zone having a fifth thickness that is less than each of the first thickness, the second thickness, and the fourth thickness and is greater than the third thickness.

19. The windshield of claim 18 , wherein the fourth thickness zone is, at least in part, between the second thickness zone and the fifth thickness zone.

20. The windshield of claim 19 , wherein the fifth thickness zone is, at least in part, between the fourth thickness zone and the third thickness zone.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Lu Zi
• Seifert Michael
• Rossini Marc-Andre

Classifications

• B64C1/1484 Primary

  Windows (B64C1/1492 takes precedence) · CPC title