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Bonding Fixture For Double Convex Aircraft Window.

Abstract: Bonding Fixture for Double Convex Aircraft Window is made up of Upper Plate (2), Lower Plate (1), Ring (3) and Commercially available Toggle clamp. Upper plate (2) and Lower Plate (1) are fixed with dowel bolts (7). The Fixture, is used to facilitate bonding operation of first lens (4) and second lens (5) of Double Convex Aircraft Window. At the start of bonding operation first lens (4) is to be placed on plate assembly (1 & 2), after application of adhesive on first lens (4) second lens (5) is kept on first lens (4) at applied adhesive peripheral area (6). The ring (3) is placed on the second lens (5) and fixed in position with commercially available toggle-clamp suitably. Hence the Bonding operation is completed. This invention reduces the lead time of bonding process of lenses and increases the positional accuracy. To be published along with Figure-4

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Notices, Deadlines & Correspondence

Patent Information

Application #
Filing Date
25 September 2023
Publication Number
15/2025
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

HINDUSTAN AERONAUTICS LIMITED
HINDUSTAN AERONAUTICS LIMITED, TRANSPORT AIRCRAFT DIVISION CHAKERI POST OFFICE -HARJINDER NAGAR KANPUR U.P INDIA-208008

Inventors

1. ANURAG
200, KHAIN, KARCHHANA, PRYAGRAJ, U.P-212307, INDIA
2. SANDEEP KUMAR
B-117, EAST GOKAL PUR, AMAR COLONY, NORTH EAST DELHI, DELHI-110094, INDIA

Specification

Documents

Application Documents

# Name Date
1 202311064103-Other Patent Document-250923.pdf 2023-09-26
2 202311064103-Form-5-250923.pdf 2023-09-26
3 202311064103-Form-3-250923.pdf 2023-09-26
4 202311064103-Form-2-250923.pdf 2023-09-26
5 202311064103-Form-18-250923.pdf 2023-09-26
6 202311064103-Form-1-250923.pdf 2023-09-26