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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).
Bump test results for four special type Firth leaf springs.

Identifier  ExFiles\Box 119\2\  scan0223
Date  26th November 1924
  
BUMP TEST.

RE. 40/50 FRONT SPRINGS.

TEST OF FOUR SPECIAL TYPE FIRTH SPRINGS (F11980/1[?]) 1100 & 1150LBS.

CONDITIONS: 2" CAMS SET AT 180°. DRUMS MAKE 105 R.P.M. TYRES AT 65 LBS/SQ"
LOAD ON FRONT OF CHASSIS = 1000LBS.

| SPRING DETAILS. | FRACTURE | POSITION OF LEAF | POSITION OF FRACTURE FROM CENTRE BOLT | APPROXIMATE RUNNING TIME | THICKNESS OF LEAF | BRINELL AT FRACTURE |
|---|---|---|---|---|---|---|
| Nº 019. NEAR SIDE 1100LBS. FLEXION: COMPRESSION = 2.0"; REBOUND = 2.5" | A | BOTTOM. | 2" TO REAR. | 22-44 | .182" | 363 |
| | B | NEXT TO BOTTOM. | 3.5" TO REAR. | 27-44 | .205" | 388 |
| | C | BOTTOM. | 1.5" TO FRONT. | 30-54 | .182" | 363 |
| | D | 2ND (FROM TOP) | 4.25" TO REAR | 30-54 | .245" | 375 |
| | E | 3RD (FROM TOP) | 2" TO REAR | 30-54 | .247" | 388 |
| | F | TOP. | 5.25" TO REAR. | 30-54 | .290" | 363 |
|---|---|---|---|---|---|---|
| Nº 020. OFF SIDE 1150LBS. FLEXION: COMPRESSION = 1.9"; REBOUND = 2.5" | G | TOP | 2" TO REAR | 45-42 | .281" | 352 |
| | H | 5TH (FROM TOP) | 1" TO REAR | 45-42 | .237" | 341 |
| | J | BOTTOM | 1.5" TO REAR | 45-42 | .208" | 363 |
|---|---|---|---|---|---|---|
| Nº 022. NEAR SIDE 1100 LBS. FLEXION: COMPRESSION = 1.6"; REBOUND = 2.4" | K | 4TH (FROM TOP) | 7" TO REAR | 36-0 | .232" | 388 |
| | L | 5TH (FROM TOP) | 7.5" TO FRONT | 42-30 | .240" | 388 |
|---|---|---|---|---|---|---|
| Nº 023. OFF SIDE 1150LBS. FLEXION: COMPRESSION = 1.5"; REBOUND = 2.5" | M | TOP. | 2" TO REAR | 32-57 | .282" | 363 |
| | N | BOTTOM. | 1.25" TO REAR | 32-57 | .210" | 352 |
  
  


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