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              An
               American engine for the Vickers Gunbus in 1915 
             
            
            
             
               
             
            
            
             At
              the outset of World War 1 the only aircraft designed for fighting in 
             the air was the Vickers Gunbus (later FB5).  Initial orders for 
             the aircraft had come from the Navy but much of the production was 
             handed over (transferred) to the Army for the RFC. 
            
             In
              the search for improved performance an engine designed by American 
             aviation pioneer and engine designer Mr John W Smith, the 
             Smith Static Motor, was trialled for the Vickers aircraft.  Mr 
             Smith moved to England in 1915 and set up the British Static Motor Company 
             in Birmingham in partnership with Mr Charles Schofield. He 
             brought with him from Chicago an experienced engine mechanic Mr 
             Ralph Watson. 
            
               
              © J Soderberg 
            
             Smith
              Static Motor (on test stand) 
            
             During
              1915 the engine was demonstrated to the Admiralty and the War Office 
             and was installed that summer on two Vickers FB5 aircraft (serial 
             no.s 1534 & 1535) for the Admiralty, the first of which was 
             delivered to RNAS Eastchurch (Isle of Sheppey) on 7 August 1915. The 
             Smith engine was relatively light and claimed to deliver 140 hp. 
            
             Watson
              wrote to his wife on 8 August 1915 the day after No.1534s delivery: 
            
             "Just
              arrived in Birmingham from London, it takes a little over 2 hours to 
             make the trip. I will be here for about a week I think unless they 
             have trouble with the motor down at the flying field. I was out to 
             the field [Joyce Green, Vickers test flight] yesterday 
             and saw them off for the other flying field belonging to the Navy [RNAS
              Eastchurch]. And they want to play with it themselves for a 
             few days and make a few more tests. I was up the other day Friday it 
             was [30 July] with Mr. Barnwell the pilot [Vickers Chief 
             test pilot Harold Barnwell], he is one of the very best 
             there is over here so I am told and he knows how to fly all right. We 
             were only up at 1200 to 1500 feet, took a trip over a little Suburb 
             of London out there, and up and down over the Thames river and I felt 
             much safer in it than in an auto doing 60 mile per. hr. and we were 
             going better than 80 M.P.H." 
            
               
            
               ©
              J Soderberg 
            
             Vickers
              FB5 aircraft 1534 
            
             Clearly
              more work was required to get the engine right.  JW Smith wrote 
             to Watson (probably at RNAS Eastchurch) on 7 Dec 1915: 
            
             
              "I
               sent along a valve unit, which consists of valve cage, exhaust and 
              intake valve so you could take out one of the old valves and put in 
              the new one. 
             
              The
               old valves that are in the motor come from the States, and I thought 
              it would be well to keep one of these valves to show to anyone when I 
              wished to convince that after the motor had made 200 hours run the 
              valve was practically as good as new. 
             
              The
               new Carburettor works perfectly on both high and low.  
             
              The
               new sight feed [clear pipe for viewing the flow] works nicely 
              for any amount of oil that I want to use it on, and you had better 
              put in this new sight feed, and let it run a good bifuel stream to 
              the extent of 1 1/4 gal. to 1 1/2 gal. per hour which means a pretty 
              thick stream as the oil is heavy and moves slow. 
             
              I
               gave the motor an hours run to-day to limber it up, and ground the 
              valves. If it has the punch to-morrow I will call up the Officials 
              for a test." 
              
            
             The
              then RFC HQ Chief of Staff Lt Col. Brooke-Popham mentioned 
             the engine in a January 1916 report of his visit to Home 
             Establishment as follows: 
            
             
              The
               Smith Radial engine was tested on Tuesday [18 Jan 1916]. It 
              ran for an hour giving 140 hp. and then broke a valve rocker. Its 
              weight is only 180 lbs. and if it can be got right it would seem that 
              it would be a very useful engine. 
              
            
             The
              same report notes however the imminent arrival of a squadron of 
             FE2bs with 240 hp Rolls-Royce engines, another pusher aircraft that 
             effectively took over from the Vickers FB5 and 9, and saw out the war 
             as a night bomber. 
            
             Watson
              writing to a friend at the Standard Steel Car Company in the US in 
             March 1916 commented on engines: 
            
             
              If
               you are getting into this game you will find that it must be a motor 
              of the radial type and no doubt air cooled as that eliminates more 
              weight than anything else and pounds per HP will always be the 
              determining factor in aeroplane work. Besides the radial type lends 
              itself to plane construction on mounting. It takes one man about 4 
              days to dismount a Sunbeam motor from a fuselage. I have taken one of 
              Smiths motors (off) in 20 minutes. 
              
            
             Flt
              Cdr? W A Bristow writing to J W Smith in October 1916 from 
             the Admiralty Air Department was enthusiastic about the engines performance: 
            
             
              Working
               out your figures after the test today I find the engine gave 131.3 
              BHP at 1,275 and the petrol consumption was .67 pts per BHP hour. 
             
              This
               seems to be very good and the engine certainly ran better than ever. 
              It will be as well I think to lock the carburettor in the position we 
              ran it in today as I should like it to go into the air just as it was. 
             
              With
               regard to request for suggestions as to improvements I am afraid it 
              is difficult to suggest anything really worth talking about. The 
              position of the carburettor might be changed &ldots; 
             
              But
               as to the design and make of the engine there is nothing I can 
              suggest as an improvement. As you know I have flown with the engine 
              about a thousand miles and I certainly feel safer with it than almost 
              any other engine I have been up with. 
             
              What
               I like about it is the ease of control and absence of vibration over 
              a wide range of speed and considering we have had to come down once 
              only and that not through any particular fault in the engine. It 
              speaks pretty well for it. Would it be possible to make a large 
              engine say 200/220 HP. You might think it over and let Commander 
              Briggs know. 
              
            
             
                
             
            
             
              ©
               J Soderberg 
             
            
             
              Smiths
               workshop in Birmingham 
             
            
             J
              W Smith sold his share of the business (UK patent rights) to Mr 
             Heenan of Heenan & Froude Ltd in early 1916 but stayed on 
             under contract in UK to help the business at the Admiraltys 
             request. The Smith motor production was moved to Heenan & Froude 
             Ltd at Worcester (see www.miac.org.uk/heenan.htm 
             ) in April 1916 and the manufacturing suffered a number quality 
             problems leading eventually to the engines rejection by the Air 
             Board. The company had an initial order for 250 engines. 
            
             There
              had been plans to fit a 140 HP Smith Static Motor in a prototype 
             seaplane PV4 designed by the Admiraltys Port Victoria 
             Marine Experimental Aircraft Depot in 1916. The engine was not 
             delivered so a Clerget was tried in June 1917 but this proved too 
             long in body (compared to the Smith) to rig the machine for 
             longitudinal control across the speed range. A prototype for another 
             Admiralty designed float plane the AD Naviplane No. 9095 was 
             built in 1916 by Supermarine initially with a 150 HP Smith Static, 
             but this proved underpowered and the engine was replaced by a Bentley 
             Rotary 1 in 1917 which also failed to deliver the required 
             performance. The design was abandoned. The Blackburn TB twin 
             engine seaplane had been another possible user of the Smith 140 
             HP engine but smaller engines had to be fitted and again it proved 
             under powered. 
            
             A
              new company, Smiths Static Motor Company, was 
             registered in November 1916, essentially holding the UK patent rights 
             for the Smith motor.  Heenan with Schofield and others were 
             Directors of the new company.  J W Smith had then returned to 
             the US because of his wifes ill health (she was a survivor of 
             the sinking of the RMS Lusitania and continued to be in poor health). 
            
             Watson
              continued to work for Smiths Motors and went to France as part 
             of efforts to promote the engine to the French Air Service. By 
             October 1917 a 190 HP engine was available and being offered as a 
             test engine to the French. Watson had been asked by J W Smith to file 
             patents for the engines in France with a view to licensed production. 
             Watson reported that negotiations with the French were hampered by 
             the lack of clarity as to who was running the company in UK.  
             Schofield had visited Paris in November and fallen seriously ill and 
             proposals were not progressed. This seems to mark the end of the line 
             for the Smiths engine. 
            
             The
              British Ministry of Munitions had taken a decision in 1917 to 
             concentrate engine manufacturing efforts on six aero engines two of 
             which, the Clerget and Bentley Rotary 1 (BR1), were in the same 
             category as the Smith Static. It would seem that the Smith 
             companys efforts were consequently directed toward the French market. 
            
             After
              WW1 the French company Darracq which had built FB5s under licence 
             from Vickers acquired Heenan & Froude Ltd. The latter continued 
             in existence after the Darracq amalgamation with Sunbeam Talbot, as 
             STD, and was sold off as a going concern after STDs bankruptcy 
             in 1935. 
            
             Sources: 
            
             R
              O Watson private papers 
            
             National
              Archives (UK) Air 1/992/204/5/1214 report by Brooke-Popham 
            
             Brooklands
              Museum Trust Archives (delivery of aircraft No. 1534 to Eastchurch) 
            
             Photographs
              copyright J Soderberg 
            
             
              Copyright
               © 2013 www.airwar1.org.uk 
             
            
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