Abstract: Sheet metal forming is one of the major process used in aeronautical industries, sheet metal forming includes stretch forming, rubber press forming. Press forming and hand forming for aeronautical applications. The practical difficulties faced and rectification carried using improved tooling techniques to achieve the required contour tolerance on the parts are enumerated. The study also provides the general input/ frame work to achieve the required tolerance for other sheet metal parts used in Light Combat Aircraft with Deep Contours.
DESCRIPTION
TECHNICAL FIELD
The invention describes the methodology for Forming Deep Contour Sheet metal Parts with Stage plates.
BACKGROUND OF INVENTION
One of the categories of sheet metal parts in Light Combat Aircraft are deep and sharp contours which has to be fabricated using High Pressure Hydraulic Press with single stage tool. The Common problem faced was cracks during forming and thinning of parts. Conventional method of Press forming had problems as below,
a) Wrinkles and overlap of material was observed during press forming, which was very difficult to overcome and resulted in rejection of the parts.
b) Since the part had deep contour involved hand forming which resulted in compromise in quality and time consumption
SUMMARY OF INVENTION
Process of High Pressure Hydraulic Press Forming was optimized by using stage plates and press forming in stages which resulted in quality parts.
PROCESS DETAIL DESCRIPTION
Methodology for forming with stage plates as follows:
a) Press forming the part with stage plates reduces the amount of wrinkles as the stage plate acts as bearing contact surface during pressing in soft condition of raw material.
b) Press forming will be done in stages with the stage plate, as the material is deformed in stages wrinkles and material thinning problems can be eliminated
c) Intermediate dressing will avoid the wrinkle formation
d) Remove extra material with 10 mm extra all round and repress the part after solutionize and trim the final trim the part profile
e) Final part will inspected to confirm the requirements of the drawings.
DRAWINGS
Fig.l: Typical part with complex contour Fig.2: Forming tool with component
CLAIMS
We claim the Methodology followed to form deep contour Sheet Metal parts in Light Combat Aircraft
| # | Name | Date |
|---|---|---|
| 1 | 50-CHE-2015 CLAIMS 05-01-2015.pdf | 2015-01-05 |
| 1 | 50-CHE-2015 FORM-5 05-01-2015.pdf | 2015-01-05 |
| 2 | 50-CHE-2015 ABSTRACT 05-01-2015.pdf | 2015-01-05 |
| 2 | 50-CHE-2015 FORM-3 05-01-2015.pdf | 2015-01-05 |
| 3 | 50-CHE-2015 CORRESPONDENCE OTHERS 05-01-2015.pdf | 2015-01-05 |
| 3 | 50-CHE-2015 FORM-2 05-01-2015.pdf | 2015-01-05 |
| 4 | 50-CHE-2015 DESCRIPTION (COMPLETE) 05-01-2015.pdf | 2015-01-05 |
| 4 | 50-CHE-2015 FORM-1 05-01-2015.pdf | 2015-01-05 |
| 5 | 50-CHE-2015 DRAWINGS 05-01-2015.pdf | 2015-01-05 |
| 6 | 50-CHE-2015 DESCRIPTION (COMPLETE) 05-01-2015.pdf | 2015-01-05 |
| 6 | 50-CHE-2015 FORM-1 05-01-2015.pdf | 2015-01-05 |
| 7 | 50-CHE-2015 CORRESPONDENCE OTHERS 05-01-2015.pdf | 2015-01-05 |
| 7 | 50-CHE-2015 FORM-2 05-01-2015.pdf | 2015-01-05 |
| 8 | 50-CHE-2015 ABSTRACT 05-01-2015.pdf | 2015-01-05 |
| 8 | 50-CHE-2015 FORM-3 05-01-2015.pdf | 2015-01-05 |
| 9 | 50-CHE-2015 CLAIMS 05-01-2015.pdf | 2015-01-05 |
| 9 | 50-CHE-2015 FORM-5 05-01-2015.pdf | 2015-01-05 |