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The Beardmore 160 hp is a British six-cylinder, water-cooled aero engine that first ran in 1916. It was built by Arrol-Johnston and Crossley Motors for
Beardmore_160_hp
The Beardmore 120 hp was a British six-cylinder, water-cooled aero engine that first ran in 1914, it was built by William Beardmore and Company as a licensed-built
Beardmore_120_hp
Topics referred to by the same term
Beardmore, 1st Baron Invernairn, a Scottish industrialist William Beardmore and Company, the engineering company of the above Beardmore Beardmore 160
Beardmore
British engineering and shipbuilding company
Sopwith Pup Wight Seaplane Beardmore 120 hp Beardmore 160 hp Beardmore Adriatic Beardmore Atlantic Beardmore Cyclone Beardmore Tornado R24r R27 R32 (airship)
William_Beardmore_and_Company
such as the Beardmore 120 hp and 160 hp. Frank Halford: Responsible for proposing modifications to the engines originally taken from Beardmore designs. Brevet
Beardmore_Halford_Pullinger
Russian airplane series
1915; fitted with four RBVZ-6 engines of 150 hp each. Type V No 182; fitted with four Beardmore 160 hp engines. Aircraft later rebuilt as a G-1. Ilya
Sikorsky_Ilya_Muromets
50 hp rotary Source: Lumsden Beardmore 120 hp Beardmore 160 hp Beardmore Simoon Beardmore Cyclone Beardmore Tornado Beardmore Typhoon Galloway Adriatic Galloway
List_of_aircraft_engines
British fighter bomber aircraft
G.102 with a 160 hp Beardmore engine. Maximum speed of the 160 hp aircraft was 108 mph (174 km/h) at sea level, falling to 100 mph (160 km/h) at 10,000 ft;
Martinsyde_G.100
well as the service's last pusher type. The M.F.6 was powered by a Beardmore 160 hp engine, imported from the United Kingdom. Concurrently with the construction
Marinens Flyvebaatfabrikk M.F.6
Marinens_Flyvebaatfabrikk_M.F.6
WW1 era inline-6 aircraft engine
to the original design, resulting in the Beardmore 160 hp. Frank Halford (the ‘H’ in B.H.P.) joined Beardmore in 1916 as a liaison officer from the Aeronautical
Galloway_Adriatic
1916 utility aircraft by Armstrong Whitworth
F.K.3, with a larger fuselage and wings, and was powered by a 160 hp (110 kW) Beardmore water-cooled engine. The undercarriage used oleo shock absorbers
Armstrong_Whitworth_F.K.8
British Admiralty Air Department patrol aircraft
Supermarine Channel. The Channel I was powered with a 160 horsepower (120 kW) Beardmore 160 hp engines, and the Channel II was fitted with a 240 horsepower
AD_Flying_Boat
1910s British piston aircraft engine
Committee for Aeronautics the Saracen faced stiff competition from the Beardmore 160 hp and Hispano-Suiza 8 and did not attract any orders. Only prototypes
Sunbeam_Cossack
966 lb (892 kg) Gross weight: 2,740 lb (1,243 kg) Powerplant: 1 × Beardmore 160 hp , 160 hp (119 kW) Performance Maximum speed: 110 mph (176 km/h, 96 kn)
Austin_Kestrel
Aircraft engine operating on the Diesel principle
single cylinder four-stroke for 215 hp (160 kW) per liter, scalable from 300 to 600 kW (400 to 800 hp) and up to 1.5 hp/lb. (2.5 kW/kg) power density with
Aircraft_diesel_engine
1929 British aero engine
"aircraft mechanic" in the Royal Flying Corps; his first job was fitting Beardmore 160 hp engines to airframes. After World War I he worked for a motor racing
Rolls-Royce_R
WW1 era inline-6 aircraft engine
10 lb/h) Power-to-weight ratio: 0.38 kW/kg (0.23 hp/lb) Comparable engines Austro-Daimler 6 Beardmore 160 hp Mercedes D.III SPA 6A Related lists List of aircraft
RBVZ-6
British WWI aircraft engine
company, William Beardmore & Co. In contemporary publications the type was often referred to as the Beardmore, or BHP, Atlantic or 500 hp. In the United
Galloway_Atlantic
1920s British diesel aircraft engine
The Beardmore Tornado is an eight-cylinder inline diesel aircraft engine built in 1927 by William Beardmore and Company of Glasgow, Scotland, and used
Beardmore_Tornado
British bomber used during the First World War
reconnaissance missions. The DH.4 was to have been powered by the new 160 hp (119 kW) Beardmore Halford Pullinger (BHP) engine, but problems with that resulted
Airco_DH.4
British fighter/reconnaissance biplane
ready and it was fitted with a 160 hp (120 kW) Beardmore engine instead. The aircraft was underpowered with the Beardmore engine and suffered reliability
Vickers_F.B.14
From 1913, the 90 and 120 hp models were produced under license in Scotland by William Beardmore and Company. The Beardmore 120 hp went on to power many British
Austro-Daimler_6
Version of the AD Flying Boat
understand the sea and its ways”. The Channel's engine was a 160 horsepower (120 kW) Beardmore 160 hp, separated from the wing structure and fixed at the top
Supermarine_Channel
takeoff weight: 7,250 lb (3,289 kg) Powerplant: 2 × Beardmore 160 hp 6-cyl. in-line piston engines, 160 hp (120 kW) each Propellers: 2-bladed wooden fixed
Central_Centaur_IIA
cabin to seat four passengers. The aircraft was powered by a 160 hp (120 kW) Beardmore engine. The pilot sat in an open cockpit offset to port. The prototype
Avro_547
Type of fighter aircraft
model, the F.E.2b, again powered by a Beardmore, initially of 120 hp, although later F.E.2bs received the 160 hp (119 kW) model. The air brake of the "a"
Royal_Aircraft_Factory_F.E.2
1920s British amphibious fighter aircraft
Sea King was a single seater biplane powered by a pusher 160 horsepower (120 kW) Beardmore engine. It first flew in early 1920 and was exhibited by Supermarine
Supermarine_Sea_King
second prototype, designated DH.3A, was built with more powerful 160 hp (120 kW) Beardmore engines, and the War Office placed a production order for 50.
Airco_DH.3
British single-engined flying boat trainer
biplane, with unequal span two-bay wings and powered by a 160 hp (119 kW) Beardmore 160 hp engine mounted between the wings driving a four-bladed propeller
Norman_Thompson_N.T.2B
French WW1 fighter and reconnaissance aircraft
made to those built by Beardmore. It could be fitted with either a 100 hp (75 kW) Clerget, 130 hp (97 kW) Clerget 9B engine or 110 hp (82 kW) Le Rhône 9J
Nieuport_12
bomber with the more powerful engine (either a 150 hp (112 kW) RAF 4a or 160 hp (119 kW) Beardmore). Over a quarter of the aircraft built were used in
Royal_Aircraft_Factory_R.E.7
Single-engined biplane seaplane
The first of the three Sporting Types, (Shrimp), was powered by a Beardmore 160 hp (119 kW) engine. Registered G-EAPZ, it was first flown on 10 December
Short_Sporting_Type
1920s British aircraft piston engine
The Beardmore Cyclone was an aero engine produced by William Beardmore & Co with the aim of producing an engine generating a high power output at low revolutions
Beardmore_Cyclone
Monoplane fighter
completed, its intended engine, the 800 hp (597 kW) Hispano-Suiza 12Ycrs, was not ready so it flew with a 600 hp (447 kW) Hispano-Suiza 12Xcrs driving a
Loire-Nieuport_161
Rigid training airships in the UK
first and last of the four ships. The other two were built by William Beardmore and Company and Armstrong-Whitworth. While the 23 class airships were
23-class_airship
Diesel electric streamliner
Publishing: 632–635. April 27, 1935. McCutchson, K. D. (2022, March 11). Beardmore . Enginehistory.org. Retrieved March 17, 2023, from https://www.enginehistory
Comet_(train)
British WW1 biplane fighter aircraft
Le Rhône 9J, 110 hp Gnome Monosoupape 9B-2, 100 hp Gnome Monosoupape 9N, 160 hp The F.1 was the main production version. It was armed with twin synchronised
Sopwith_Camel
French series of aircraft engines
Not accepted by French military aviation authorities. Le Rhône 18E (1913) 160 hp (120 kW) two-row rotary displacing 21.8 litres, consisting of two nine-cylinder
Le_Rhône
Military transport aircraft
climb: 1,300 ft/min (6.6 m/s) Wing loading: 32 lb/sq ft (160 kg/m2) Power/mass: 10.5 lb/hp (4.8 kg/hp) C-117Ds flying over MCAS Iwakuni 1981. One of these
Douglas_R4D-8
French pre-WW1 racing aircraft
started constructing his first aircraft, a small monoplane powered by a 20 hp (15 kW) Darracq engine and succeeded in making some brief straight-line flights
Nieuport_II
British fighter (1924 - 1934)
Reserve Flying School at Renfrew operated by William Beardmore and Company, with the Beardmore-owned aircraft being powered by Jupiter VI engines, while
Bristol_Jupiter_Fighter
Locomotive powered by a diesel engine
manufacturers in the 1930s, e.g. by William Beardmore and Company for the Canadian National Railways (the Beardmore Tornado engine was subsequently used in
Diesel_locomotive
733 kg) Gross weight: 5,100 lb (2,313 kg) Powerplant: 2 × Beardmore water-cooled inline , 120 hp (90 kW) each Performance Maximum speed: 87 mph (140 km/h
Bristol_T.T.A.
Classes of British self-powered diesel trains
Railway (LMS) commissioned a four-car DEMU in 1928, using a 500 hp (370 kW) Beardmore engine; this was similar to that used on the airship R101, placed
British railcars and diesel multiple units
British_railcars_and_diesel_multiple_units
French WW1 bomber aircraft
tailplane including a heart shaped elevators. It was powered by a 220 hp (160 kW) Renault 12F V-12 engine. with Hazet modular radiators mounted on each
Nieuport_15
Hypertension occurring during pregnancy
for Healthcare Research and Quality (AHRQ). doi:10.23970/ahrqepccer263. Beardmore KS, Morris JM, Gallery ED (January 2002). "Excretion of antihypertensive
Pre-eclampsia
1929 Italian prototype heavy bomber
meaningful meeting and conversation with his inspiration, Count Caproni. Beardmore Inflexible NACA 1930, p. 1. Orbis 1985, p. 1054. NACA 1930, pp. 1-2. NACA
Caproni_Ca.90
were delivered with 100 hp (75 kW) Scania-Vabis engines, which proved too weak and was replaced with 160 hp (120 kW) Beardmore or Sunbeam engines. For
Marinens Flyvebaatfabrikk M.F.8
Marinens_Flyvebaatfabrikk_M.F.8
French sesquiplane fighter
aircraft, powered by a 500 hp (370 kW) Hispano-Suiza 12Hb. Nieuport-Delage NiD.621 Twin-float fighter-trainer, powered by a 500 hp (370 kW) Hispano-Suiza
Nieuport-Delage_NiD_62
Defunct French aircraft manufacturer
production after the Russian Revolution had ended. In Scotland, William Beardmore and Company built the Nieuport 12 under licence, while gradually incorporating
Nieuport
Family of French naval dive-bombers
to develop a faster version, by substituting an 860 hp (640 kW) Hispano-Suiza 12Y-31 for the 690 hp (510 kW) Hispano-Suiza 12Xcrs engine of the LN.401
Loire-Nieuport_LN.401
British fighter aircraft used in World War One
Type 9 R.2A, to be powered by the 120 hp Beardmore engine and the similar Type 9A R.2B, powered by the 150 hp Hispano-Suiza. Both designs had the fuselage
Bristol_F.2_Fighter
Series of 1920s French racing monoplanes
Wright-Hispano H-3 water-cooled upright V-8, 300 kW (400 hp) Performance Maximum speed: 300 km/h (190 mph, 160 kn) or more Range: 400 km (250 mi, 220 nmi) Aircraft
Nieuport-Delage_Sesquiplan
Prototype with a 160 kW (220 hp) Wright J-5C radial engine, one built later converted to a 641. NiD 641 Production aircraft with a 180 kW (240 hp) Lorraine 7M
Nieuport-Delage_NiD_640
1927 fighter aircraft family
Hispano-Suiza 12Hb liquid-cooled V-12 engine, 373 kW (500 hp) Performance Maximum speed: 260 km/h (160 mph, 140 kn) at 1,800 m (5,900 ft) Range: 400 km (250 mi
Nieuport-Delage_NiD_52
1920s British piston aircraft engine
The Siddeley Tiger marked the end of the aero engine line started by Beardmore and Siddeley-Deasy. The name was later re-used for an Armstrong Siddeley
Siddeley_Tiger
French WW1/post-WW1/interwar fighter aircraft
pre-production batch was ordered on 21 August 1918. It was powered by a 220 kW (300 hp) Hispano-Suiza 8Fb piston engine and performed well in test, but could not
Nieuport-Delage_NiD_29
(2,970 lb) Powerplant: 1 × Hispano-Suiza 8Ab , 130 kW (180 hp) Performance Maximum speed: 160 km/h (100 mph, 87 kn) Range: 350 km (220 mi, 190 nmi) Service
Nieuport-Delage_NiD_38
French WW1 reconnaissance aircraft
fitted with a 180 hp (130 kW) Lorraine-Dietrich 8A engine, another with a 150 hp (110 kW) Hispano-Suiza engine, and a third with a 220 hp (160 kW) Hispano-Suiza
Nieuport_14
French WW1 fighter aircraft
landing – this was corrected by using heavier bracing wire. The Nieuport 28's 160 hp Gnome 9N rotary engine and fuel system proved to be unreliable and prone
Nieuport_28
Both wings were fabric covered. The Nie 31 was powered by a 130 kW (180 hp) Le Rhone 9R nine-cylinder rotary engine, smoothly and completely cowled.
Nieuport_31
French WW1 Nieuport fighter aircraft
examples) Netherlands Luchtvaartafdeling - operated 5 Nieuport 21s as 80 HP Nieuports. Portugal Portuguese Air Force Romania Romanian Air Corps Russian
Nieuport_21
Fighter aircraft built in France
monoplane fighter with 370 kW (500 hp) Hispano-Suiza 12Hb (one built) NiD 42S shoulder-wing monoplane racer with 450 kW (600 hp) Hispano-Suiza 12Hb (two built)
Nieuport-Delage_NiD_42
upright water cooled V-8, 220 kW (300 hp) Propellers: 2-bladed fixed pitch Performance Maximum speed: 250 km/h (160 mph, 130 kn) at 7,000 m (23,000 ft)
Nieuport-Delage_NiD_37
baggage space behind them. The steel structure also mounted an 89 kW (120 hp) Lorraine 5Pc five-cylinder radial engine in uncowled pusher configuration
Nieuport-Delage_NiD_940
French WW1 sesquiplane fighter aircraft used by the RNAS
rotaries, they were fitted with the 130 hp (97 kW) Clerget 9B rotary instead of the 25 kg (55 lb) lighter 120 hp (89 kW) Le Rhône 9J used in most of the
Nieuport_17bis
French WW1 fighter aircraft
and better balance. It was fitted with the 110 hp (82 kW) Le Rhône 9J engine and later examples used 120 hp (89 kW) motors. The upper wings of the Nieuport
Nieuport_17
French WW1 fighter aircraft
Nieuport 16, which was a strengthened Nieuport 11 airframe powered by a 110 hp (82 kW) Le Rhône 9J rotary engine. Visible differences included a larger aperture
Nieuport_11
and a deep, straight edged rudder. The NiD 43 was powered by a 373 kW (500 hp) Hispano-Suiza 12Hb water cooled upright V-12 engine in the nose, which drove
Nieuport-Delage_NiD_43
French fighter aircraft
upright V-12 water-cooled engines, with a 298 kW (400 hp) 12Jb in the first prototype and a 373 kW (500 hp) 12Hb in the second, the NiD 48bis. Aft of the engine
Nieuport-Delage_NiD_48
High wing, eight seat, single engine airliner
Its first flight, made early in 1930 by Lasne, was powered by a 430 kW (580 hp) Renault 12Ki V-12 engine, identifiable by a short, upright exhaust stub,
Nieuport-Delage_NiD_540
piston engine, 32 hp (24 kW) Propellers: 2-bladed fixed-pitch propeller Performance Maximum speed: 70 mph (110 km/h, 61 kn) Range: 100 mi (160 km, 87 nmi) Aircraft
Bristol_Brownie
engines, and Sinnott, Aircraft Design, pp. 165–71. HP.66 would have had Hercules 100 engines, HP.69 turbo-supercharged Hercules. According to Buttler
List of Air Ministry specifications
List_of_Air_Ministry_specifications
400 kg (3,100 lb) Powerplant: 1 × Armstrong Siddeley Lynx IVC , 150 kW (200 hp) Performance Maximum speed: 175 km/h (110 mph, 96 kn) Range: 375 km (234 mi
Nieuport-Delage_NiD_39
French WW1 fighter aircraft
made in December 1917, or early January 1918 while powered by a 110 kW (150 hp) Gnome Monosoupape 9N rotary engine, the same engine used in the Nieuport
Nieuport_Madon
TSR-2 UK Jet Reconnaissance bomber 1964 Prototype 2 Beardmore W.B.1 UK Bomber 1917 Prototype 1 Beardmore W.B.VI UK Torpedo bomber n/a cancelled project 0
List_of_bomber_aircraft
Gray, 1970, p.493 Wixey 1990, p. 135. Wixey 1990, p. 147. Wixey 1990, pp. 160–161. Wixey 1990, pp. 167–174. Wixey 1990, p. 107. Wixey 1990, pp. 190–193
List of flying boats and floatplanes
List_of_flying_boats_and_floatplanes
French single-seat parasol monoplane fighter aircraft
specification for an all-metal, single-seat fighter to be powered by a 650 hp (485 kW) engine and required to reach a speed of 350 km/h (217 mph) and a
Nieuport-Delage_NiD-120
two 10.60 m (34.8 ft) long all-metal floats and powered by two 310 kW (420 hp) Gnome & Rhône 9A Jupiter radial engines. The 4 crew members were to have
Nieuport-Delage_NiD_50_HB.4
French WW1 fighter aircraft
advanced trainers, and the 130 hp (97 kW) Le Rhône 9JB Rotary engine was often replaced by lower powered engines, such as the 80 hp (60 kW) Le Rhône 9C. Operational
Nieuport_27
French pre-WW1 racing and reconnaissance aircraft
by the air forces of several countries. It was initially powered by a 50 hp (37 kW) Gnome Omega rotary engine, which was later replaced by more powerful
Nieuport_IV
weight: 2,580 kg (5,680 lb) Powerplant: 1 × Sunbeam Matabele , 260 kW (350 hp) Performance Maximum speed: 172 km/h (108 mph, 94 kn) Range: 420 km (260 mi
Nieuport-Delage_NiD_30
British aerospace and engineering company (1915–1977)
16-cylinder 1,500 hp (1,100 kW) Fairey Monarch – 2 x 12 cylinders (two engines with one propshaft passing through the other) 2,250 hp. The P-24 flew in
Fairey_Aviation_Company
French WW1 reconnaissance aircraft
weight: 795 kg (1,750 lb) Powerplant: 1 × Gnome rotary engine , 60 kW (80 hp) Performance Maximum speed: 105 km/h (65 mph, 56 kn) Taylor 1989, p.696 The
Nieuport_VI
1928 disappearance of New Zealand aviation pioneers
Australia to New Zealand in a four-seater, 450 hp open-sea reconnaissance machine made by William Beardmore and Company". It was estimated about £8,500 would
Moncrieff and Hood disappearance
Moncrieff_and_Hood_disappearance
respectively powered by a Lorraine 12 Rcr, 1,500 kW (2,000 hp) and a Renault 12 Ncr, 1,500 kW (2,000 hp) liquid-cooled V-12 engines, and with dimensions similar
Nieuport-Delage_NiD_450
French WW1 aircraft
Powerplant: 1 × le Rhône 9C 9-cylinder air-cooled rotary piston engine, 60 kW (80 hp) Propellers: 2-bladed fixed-pitch Régy 155 or Chauviere 2219 propeller, 2
Nieuport_10
Former Royal Air Force station in Kent, England
Combat Aircraft (Salamander ed.). Hamlyn. p. 56. ISBN 0-600-33144-X. 160 hp BHP (Beardmore-Halford-Pullinger) engine, Lee, David W. (2010). Action Stations
RAF_Lympne
three-seat light aircraft Beagle Basset light twin-engine utility aircraft Beardmore Wee Bee ultralight Bede BD-1 two-seat prototype design Bede BD-4 four-seat
List_of_civil_aircraft
Locomotive wheel arrangement
last six in 1948. There was also a Class XE that was built by William Beardmore & Company and Vulcan Foundry. Wartime designs included the Class AWD and
2-8-2
French fighter prototype
387 lb) Powerplant: 1 × Le Rhône 9Ja 9-cylinder rotary engine, 82 kW (110 hp) Propellers: 2-bladed fixed-pitch wooden Lavasseur 484 Performance Maximum
Nieuport_Triplane
French single-seater fighter
Powerplant: 1 × Le Rhône 9R 9-cyl. air-cooled rotary piston engine, 130 kW (180 hp) Performance Maximum speed: 193 km/h (120 mph, 104 kn) Cruise speed: 150 km/h
Nieuport-Delage_NiD_32
French WW1 fighter aircraft
the faired wood externally sprung tailskid used on previous types. A 130 hp (97 kW) Le Rhône rotary engine was fitted in a spun aluminium cowl similar
Nieuport_24
French WW1 fighter aircraft
developed in 1916, with a strengthened airframe powered by a more powerful 110 hp (82 kW) Le Rhône 9J rotary engine. Visible differences included a headrest
Nieuport_16
1978, pp. 25–27 Thetford, 1978, pp. 326–327 Thetford, 1978, pp. 39–43, 159–160 Thetford, 1978, pp. 121–122 Thetford, 1978, pp. 401–402 Thetford, 1978, pp
List of aircraft of the Royal Air Force
List_of_aircraft_of_the_Royal_Air_Force
French trimotor monoplane
sides and underside but with curved upper decking. The NiD 740's central 95 hp (71 kW) Salmson 7Ac seven-cylinder radial engine was uncowled in the nose
Nieuport-Delage_NiD_740
British rigid airship in service 1929-1930
the engine would not be developed in time and it was decided to fit the Beardmore Tornado diesel engine that was being developed for the Air Ministry for
R100
Aircraft powered by three piston engines
US 1913 Beardmore Inflexible UK 1928 Beechcraft Model 18 Tiara engine testbed US 1966 Bellanca 28-92 US 1937 Bernard 60 France 1929 Bernard 160 France
Trimotor
pp. 349–363 Chant, 1999, p.43 Jackson 1968, pp. 128–134 Jackson 1968, pp. 160–169 Jackson 1968, pp. 150–159 Jackson 1968, pp. 439–451 Jackson 1968, pp
List of carrier-based aircraft
List_of_carrier-based_aircraft
French monoplane designed for policing
controlled through hand-operated differential brakes. Two of the three 220 kW (300 hp) nine-cylinder radial Lorraine 9Na Algol engines were mounted under the wings
Nieuport-Delage_NiD_590
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP
BEARDMORE 160-HP