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Mark Nankivil said:Greetings All -
From the Vought Archives, V507-22. The drawing in the report did not have the top view
Enjoy the Day! Mark
Look at reply #13 of this Subject Mark.
Mark Nankivil said:Greetings All -
From the Vought Archives, V507-22. The drawing in the report did not have the top view
Enjoy the Day! Mark
circle-5 said:Here's an aircraft carrier spotting model from Vought. I don't know what type it represents, but maybe one of you graphics wizards can unfold the wings, stabs and radome which might help visualize the overall shape.
I'm impressed by the wing fold being so close to the root, which makes the airframe fit in a very compact area.
Many thanks to whomever can figure this one out.
Tailspin Turtle said:Here's how I think the folding works. The wing sweep pivot is in the part of the wing that folds up. To unfold, the wing is first unswept, i.e. it swings up vertically. That moves the semicircle that is hanging down in the swept and folded position so the wing can be unfolded. When the wing is swept back in flight, that semicircle slides into a cavity in the fixed inboard section of the wing.
Source: https://www.asme.org/getmedia/2d64abc8-3fa3-4d29-92d4-40db4777e8b2/238-Grumman-Wildcat-Sto-Wing-Wing-folding-Mechanism.aspxMany laborious hours were spent over sketches and with models trying to figure out a way to twist the wings to a vertical position and then fold them back along the fuselage. Finally, Roy Grumman, a fine engineer, found the steps. He saw in all probability that the solution revolved around a pivot. So he took a soap eraser, such as those used in drafting, and used that to represent the fuselage of the plane. Then he took two paper clips for the wings and bent out the short end of each of the clips so that it was normal or perpendicular to the body of the clip. Then he began sticking these short ends into the eraser until he found the proper angle and position at which the clip, when twisted to a vertical position, would also fold back snugly against the eraser. Eureka! It was as simple as that. Once the principle of the “STO-Wing” (as it came to be called) was established, all that remained was some hard engineering work by Grumman’s fine team of engineers to make the mechanism strong and fail-safe.
The STO-Wing was applied to the Wildcat, the Hellcat and the TBF Avenger. The Grumman folding wing is still in use today, notably on the larger carrier-based aircraft built by Grumman
Box 38
1 Agreement of Understanding between LTV Aerospace 1966 for its LTV Vought Aeronautics Division and Lockheed Aircraft Corporation for its Division Lockheed- California Co.
V507 “Rough Order of Magnitude” 1968
Method of Determining Prices for Varying Lot Quantities nd
Departmental Correspondence 1968
Three photographs of Avions Marcel Dassault 1967
Aviation Magazine nd
2 VFX Pricing, V-507B Configuration 1968
Departmental Correspondence 1968
3 Space/Aeronautics, Article: Tactical Air Superiority 1968
Handwritten notes belonging to Clark on the Config VFX 1968
Report: Avionics, Armament & Engine Tradeoffs nd
Special Agreement between Dassault International and 1968
LTV Aerospace Corporation
Report: VFX Wing Package proposal CALAC vs VAD nd
Report: LTVAC-Dassault Agreements 1968
Lockheed/LTV/Univac Management Meeting 1968
4 VFX Mockup and Display Area 1968
5 Report No. 2-50000/8R-1A, Vought Model V-507 nd
Conference with Professor Courtland 1968
6 VSX Selling Prices - Telephone Discussion 1969
Technical Debriefing of VFX 1969
CVA 59 A/C Elevator Compatibility Study
Box 39
1 Vought Projects Fixed Wing VFX nd
2 Pentagon FX Presentation 1968
NASA debriefing comments relative to the VFX-1 1970
Powerplant Analysis
Highlights of Dassault - LTA Agreement on 1970
Co-operation re: Interchange, Tactical Aircraft
Know-how - VFX Program
Correspondence 1968
Memorandum 1968, 70
PaulMM (Overscan) said:Where's the crate Richard
Hope that is resting on your desktop!Ran across this little jewel of a find recently. V-505 model.