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Design specifications for rear springs for a Bentley Chassis.


Identifier  ExFiles\Box 100\1\  scan0177
Date  27th June 1938
  
446

DESIGN FOR SPRINGS

Reference Rolls-Royce letter Roy {Mr H. Royce - Buyer} /HW.1., dated 27.6.38., for 2. Rear Springs for Bentley Chassis similar to F.B.3851., but having the following characteristics:-

Load................... = 1000 lbs.
Width of Plates.......... = 2".
Span................... = 50.0".
Loaded Camber............ = Nil. i.e.Spring flat.
Free Camber.............. = 7.0".
Deflection due to Load. = 7.0". positive.
Main Plate thickness. = .26".

For particulars of design see table below.

=================================================================
Plate | Thickness | Length | Ex. Dist. | Remarks
Nos. | Inches. | Inches | Inches. |
=================================================================
1. | .26 | 50 + 2 eyes. | Nil | Rolled eyes to be the same as FB.3851., but with riveted lubricators. M.P.ground, other plates concave buffed. All plates to be polished & plated. Clip positions:- Front end - 9.3/4" & 19.0". Rear end - 11.0" & 19.3/4". ex Centre bolt.
2. | .25 | 48.6. | .7. |
3.x | .24 | 42.3/8. | 9/16. |
4. | .23 | 36.0. | 1/2. |
5. | .23 | 30.0. | 1/2. |
6.x | .22 | 24.1/8. | 9/16. |
7. | .22 | 17.1/2. | 3/8. |
8. | .21 | 11.0. | 1/4. |
-----------------------------------------------------------------
TOTAL.| 1.86. | ---- | ---- | ---------
=================================================================

NOTE. Range of stress to the Loaded position = 37.8 Tons per Sq. inch.
" " " " " Max. Bump " = 59.5 Tons per Sq. inch.

HWs!
T.F & J.B.Ltd.
29.6.38.
Filed to TB I . 30.6.38
  
  
From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).


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