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Best Fitted Cylinder Concept For Neutralizing The Contoured Form Tool For Lug Finalizing And For Optimum Usage Of Material

Abstract: The method involves taking set of points from the contour surface and fit a cylinder by repeated iteration and use the fitted cylinder axis as reference for design of the form Tool and other related master Tool and lug hole finalizing for further use on Assembly.

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Patent Information

Application #
Filing Date
05 January 2015
Publication Number
28/2016
Publication Type
INA
Invention Field
COMPUTER SCIENCE
Status
Email
Parent Application
Patent Number
Legal Status
Grant Date
2023-12-09
Renewal Date

Applicants

HINDUSTAN AERONAUTICS LIMITED
MANAGER (TOOLING), LCA TEJAS DIVISION, POST BOX NO. 3791, MARATHAHALLI POST, BANGALORE - 560 037

Inventors

1. MOHAN KUMAR. M
LCA TEJAS DIVISION, HAL BANGALORE - 37
2. C. CHITTAPPA
LCA TEJAS DIVISION, HAL BANGALORE - 37
3. M.C. SURESHA
LCA TEJAS DIVISION, HAL BANGALORE - 37

Specification

Description

Technical Field

The present development is related'with Military Aviation Industry more particular to structural assembly of Tejas (LCA) Aircraft.

Background of Invention

For any Tool design of contoured parts require neutralizing of the profile,
Conventional method of neutralizing is done for economical usage of raw material and not for manufacturing simplicity.

To make the design for manufacturing simplicity as well as manufacturing simplicity, the neutralizing by best fitted cylinder can be best suited.

a. For any tool Design of contoured parts require neutralizing of the profile,Conventional method of neutralizing is done for economical usage of raw material and not for manufacturing simplicity.

b. Lug holes are required for contour sheet metal part (doors and covers) for forming reference and for subsequent usage of the formed part on Assembly.

More than 90 % of the sheet metal form blocks are machined on 3 Axis machine. (With ball nose cutter).
On three axis machine, lug holes drilled on the form block will be normal to the base (Bed) and not necessarily normal to the contour and thereby the hole become elliptical and reference for further usage will not be feasible.

To make the design for manufacturing simplicity, lug hole finalising as well as economical usage, the neutralizing by best fitted cylinder can be best suited for the design of the form block (sheet metal )/Layup tool(for composite parts) and subsequent usage oh Assembly and design of Master model for making drill template for panel.

Summary of invention

A cylinder is best fitted on to the contour surface and the fitted cylinder axis is taken as reference for further 1. design of form block, 2. lug hole finalizing, 3. master model design and 4. Calculation of development length for the contour parts (allied benefit) using the neutral axis.

Process details description

1. The panel on the Aircraft look like this.

2. Take a set of 5 to 6 sections and create a set of points on to the section curve.

3. A cylinder is fitted.

4. Repeat the step 1 and step 2 and get a iterated fitted cylinder

5. Using the Axis of the cylinder and fitment of axis system make the form block design. The lug created by this method will normal to the base and normal to contour as well.

6. The model made out of this method can be further used for making the master with simplified angles which will have optimum machining requirement with minimum material usage.

CLAIMS

We claim that :-

1. Simplifying the angle and improve the manufacturing and thereby improving the quality. -

2. Economical usage of Costly imported Raw materials.

3. Lug holes used in detail parts can be taken further as reference to Assembly Locations.

Documents

Application Documents

# Name Date
1 51-CHE-2015 FORM-5 05-01-2015.pdf 2015-01-05
1 51-CHE-2015-IntimationOfGrant09-12-2023.pdf 2023-12-09
2 51-CHE-2015 FORM-3 05-01-2015.pdf 2015-01-05
2 51-CHE-2015-PatentCertificate09-12-2023.pdf 2023-12-09
3 51-CHE-2015-REPLY FROM DEFENCE.pdf 2022-11-30
3 51-CHE-2015 FORM-2 05-01-2015.pdf 2015-01-05
4 51-CHE-2015-Defence-25-08-2022.pdf 2022-08-25
4 51-CHE-2015 FORM-1 05-01-2015.pdf 2015-01-05
5 51-CHE-2015-Amended Pages Of Specification_FER Reply_25-07-2022.pdf 2022-07-25
5 51-CHE-2015 DESCRIPTION (COMPLETE) 05-01-2015.pdf 2015-01-05
6 51-CHE-2015-Authorization Certificate_FER Reply_25-07-2022.pdf 2022-07-25
6 51-CHE-2015 CORRESPONDENCE OTHERS 05-01-2015.pdf 2015-01-05
7 51-CHE-2015-Cancelled pages_FER Reply_25-07-2022.pdf 2022-07-25
7 51-CHE-2015 CLAIMS 05-01-2015.pdf 2015-01-05
8 51-CHE-2015-Correspondence_FER Reply_25-07-2022.pdf 2022-07-25
8 51-CHE-2015 ABSTRACT 05-01-2015.pdf 2015-01-05
9 51-CHE-2015-Drawings_FER Reply_25-07-2022.pdf 2022-07-25
9 Form18_Normal Request_19-12-2018.pdf 2018-12-19
10 51-CHE-2015-Form5_FER Reply_25-07-2022.pdf 2022-07-25
10 Correspondence by Applicant_Form18_19-12-2018.pdf 2018-12-19
11 51-CHE-2015-FER.pdf 2022-01-27
12 51-CHE-2015-Form5_FER Reply_25-07-2022.pdf 2022-07-25
12 Correspondence by Applicant_Form18_19-12-2018.pdf 2018-12-19
13 51-CHE-2015-Drawings_FER Reply_25-07-2022.pdf 2022-07-25
13 Form18_Normal Request_19-12-2018.pdf 2018-12-19
14 51-CHE-2015 ABSTRACT 05-01-2015.pdf 2015-01-05
14 51-CHE-2015-Correspondence_FER Reply_25-07-2022.pdf 2022-07-25
15 51-CHE-2015 CLAIMS 05-01-2015.pdf 2015-01-05
15 51-CHE-2015-Cancelled pages_FER Reply_25-07-2022.pdf 2022-07-25
16 51-CHE-2015 CORRESPONDENCE OTHERS 05-01-2015.pdf 2015-01-05
16 51-CHE-2015-Authorization Certificate_FER Reply_25-07-2022.pdf 2022-07-25
17 51-CHE-2015 DESCRIPTION (COMPLETE) 05-01-2015.pdf 2015-01-05
17 51-CHE-2015-Amended Pages Of Specification_FER Reply_25-07-2022.pdf 2022-07-25
18 51-CHE-2015 FORM-1 05-01-2015.pdf 2015-01-05
18 51-CHE-2015-Defence-25-08-2022.pdf 2022-08-25
19 51-CHE-2015-REPLY FROM DEFENCE.pdf 2022-11-30
19 51-CHE-2015 FORM-2 05-01-2015.pdf 2015-01-05
20 51-CHE-2015-PatentCertificate09-12-2023.pdf 2023-12-09
20 51-CHE-2015 FORM-3 05-01-2015.pdf 2015-01-05
21 51-CHE-2015-IntimationOfGrant09-12-2023.pdf 2023-12-09
21 51-CHE-2015 FORM-5 05-01-2015.pdf 2015-01-05

Search Strategy

1 searchstrategyE_25-01-2022.pdf

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