GB360951A - Improvements in engine mountings for aircraft - Google Patents
Improvements in engine mountings for aircraftInfo
- Publication number
- GB360951A GB360951A GB23958/30A GB2395830A GB360951A GB 360951 A GB360951 A GB 360951A GB 23958/30 A GB23958/30 A GB 23958/30A GB 2395830 A GB2395830 A GB 2395830A GB 360951 A GB360951 A GB 360951A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- ribs
- points
- leading edge
- main spar
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/04—Aircraft characterised by the type or position of power plant of piston type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
360,951. Propelling aeroplanes. BAYERISCHE FLUGZEUGWERKE AKT.- GES. and MESSERSCHMITT, W., 118A, Haunstetterstrasse, both in Augsburg, Germany. Aug. 11, 1930, No. 23958. [A Specification was laid open to inspection under Sect. 91 of the Acts, Aug. 12, 1930.] [Class 4.] In aeroplanes in which one or more engines are secured to the wing at least two of the enginebearing points are secured to or mounted on the ribs of the wing, the remaining bearing points, if any, being mounted on the cross spar or spars. Figs. 1 and 2 show an engine nacelle 7 mounted in the trailing edge of the wing by means of lugs 11 .. 14 on bearing plates 15, 16, 19, 20 on the ribs 8, 9 and also on the rear main spar. Fig. 5 shows a wing in which the ribs 31 .. 34 converge to the edges of the wing and in which the points of support are shown at 36 in the leading edge and 35 in the trailing edge of the wing, the main spar 27 being shown. Fig. 7 shows a wing in which the supports are .disposed at 43, 44 in the leading edge on parallel ribs 45, 46 and on the main spar 27 at 42 and if necessary at 47, 48. In Fig. 9 the ribs 56, 57 at the leading edge are triangulated with enginesupporting points at 58, 59 and in addition parallel ribs 60, 61, 62 are provided with bearing points 63, 64.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23958/30A GB360951A (en) | 1930-08-11 | 1930-08-11 | Improvements in engine mountings for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23958/30A GB360951A (en) | 1930-08-11 | 1930-08-11 | Improvements in engine mountings for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB360951A true GB360951A (en) | 1931-11-11 |
Family
ID=10204087
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23958/30A Expired GB360951A (en) | 1930-08-11 | 1930-08-11 | Improvements in engine mountings for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB360951A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2465581A (en) * | 1945-08-07 | 1949-03-29 | Ferrel Ind Inc | Airplane construction |
| FR3037521A1 (en) * | 2015-06-16 | 2016-12-23 | Airbus Operations Sas | TOOL FOR POWERING A CONNECTING ELEMENT AND METHOD FOR ATTACHING AN AIRCRAFT ENGINE USING THE SAME |
-
1930
- 1930-08-11 GB GB23958/30A patent/GB360951A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2465581A (en) * | 1945-08-07 | 1949-03-29 | Ferrel Ind Inc | Airplane construction |
| FR3037521A1 (en) * | 2015-06-16 | 2016-12-23 | Airbus Operations Sas | TOOL FOR POWERING A CONNECTING ELEMENT AND METHOD FOR ATTACHING AN AIRCRAFT ENGINE USING THE SAME |
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