eBay: Non type specific.
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Snautzer01
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Blackburn Ripon N203 1ste prototype
R.A.F: BLACKBURN RIPON I 1ST PROTOTYPE ORIGINAL DOUGHTYS PHOTOGRAPH W/ STAMP | eBay
ORIGINAL DOUGHTYS PHOTOGRAPH W/ STAMP. BLACKBURN RIPON I 1ST PROTOTYPE.
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Good shots!
Blackburn Ripon N203 1ste prototype
This picture doesn't really give too much indication of how big these aircraft were. The only clue is the size of the rear seat's gun ring and its engine size. It had a fuselage length of 37 feet. It's a pity that the usual measuring stick that was placed in front of aircraft for official photographs is not visible.
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Snautzer01
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De Havilland DH.103 Hornet Sea Hornet PX301 QV-C. At Airworks, Hurn, (Bournemouth) which ran the civilian piloted Fleet Requirement Unit (FRU) for training RN radar operators.
WWII: DH103 HORNET F3 AT AIRWORKS HURN BOURNEMOUTH B&W PHOTOGRAPH | eBay
DH103 HORNET F3. AT AIRWORKS. HURN, BOURNEMOUTH. B&W PHOTOGRAPH.
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- #1,668
Snautzer01
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BLOCH 162 B5 BOMBER PARIS AIR SHOW 1938
BLOCH 162 B5 BOMBER PARIS AIR SHOW 1938 VINTAGE ORIGINAL PRESS PHOTO | eBay
Find many great new & used options and get the best deals for BLOCH 162 B5 BOMBER PARIS AIR SHOW 1938 VINTAGE ORIGINAL PRESS PHOTO at the best online prices at eBay! Free shipping for many products!
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Snautzer01
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HANDLEY PAGE MANX HO222
HANDLEY PAGE MANX TAIL-LESS AIRCRAFT ORIGINAL KEYSTONE PRESS PHOTO 1945 | eBay
OK condition, with wear.
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cammerjeff
Staff Sergeant
I always liked the looks of that plane, almost like a French B17. I don't know what the performance would have been though.
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Snautzer01
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BURMESE AIR FORCE AIRSPEED CONSUL ROCKET PROJECTILE
BURMESE AIR FORCE AIRSPEED CONSUL ROCKET PROJECTILE ORIGINAL MANUFACTURERS PHOTO | eBay
OK condition, with wear, wrinkling.
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- #1,675
Snautzer01
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Vultee 1A Captain Maya
Foto Spanien, Flugzeug Legion Condor, Capitan Haya, Flieger, Spanier, TOP | eBay
Entdecken Sie Foto Spanien, Flugzeug Legion Condor, Capitan Haya, Flieger, Spanier, TOP in der großen Auswahl bei eBay. Kostenlose Lieferung für viele Artikel!
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Nice shots!
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Snautzer01
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Focke-Wulf FW300 Focke-Wulf FW206 CIOS Report German Activities in the French Aircraft Industry.
quite far i think. Average pay per work hour 80,- Franks
so
fw206 cost 18400000
fw300 cost 12800000
------------------------+
31200000
quite far i think. Average pay per work hour 80,- Franks
so
fw206 cost 18400000
fw300 cost 12800000
------------------------+
31200000
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Snautzer01
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Focke-Achgelis Fa284
We had previously had unconfirmed information that the
Germans were developing a large helicopter for the purpose of
carrying heavy loads for short distances, i.e. transporting tanks
or heavy trucks over rivers, hoisting bridge girders into place
etc. The Fa 284 proves to be this type. The design work had been
going on at the Breguet Design Office at Montaudran Aerodrome near
Toulouse, but all the drawings were destroyed when the plant was
bombed, and the following details were supplied from memory by the
French personnel who were interviewed.
The Focke-Achgelis Firm supplied all general arrangement and
some detail drawings and Breguet were asked to design the fuselage
structure and rotor blades. A sketch of the aircraft is given at
pic. 4. It is typical of the Focke-Achgelis helicopters in that
it is of the side by side twin rotor type, the oppositely rotating
rotors each three-bladed and 18 metres (58.5 ft.) diameter, being
carried at each end of a transverse beam consisting of a centre
portion and inclined outriggers built up of tubular struts.
Each blade is built on a tubular steel spar with wooden ribs
and three ply covering. The spar is 8 cm. outside diameter with
a wall thickness of 6.5 mm and is cylindrical and of constant
gauge from the root to the station at 4*5 metres radius. From
this station to the tip it is swaged down until at the tip the
section is a parallel sided oval of 8 cm major axis, outside depth
3 cm and wall thickness 2.5mm. Over the section where the spar
is cylindrical the blades are rectangular of 77 cm chord, tapering
thereafter until at the tip the chord is 36 cm. The aerofoil
Sections are of the NACA 250 Series of 1# thickness/chord ratio.
The area of each blade is 5.4 sqr. metres so that the solidity is
.064-
The original aircraft was to have been powered by 2 BMT 801
engines rated at 1,600 horse power each, but at a later stage the
power was increased to 2,000 horse power. The engines are situated
towards the centre of the transverse beam and drive the rotors
through gears and shafting. A system of clutches is provided so
theither can drive one or both rotors, and the rotors can be
synchronised.
The outrigger beam constitutes the main structural member
and the fuselage is a simple framework attached to the beam and
carries only the usual tail surfaces and a cockpit for the crew
of two which la located behind the rotors. Except for the
cockpit and the tail surfaces the whole framework is left
uncovered. N° accommodation is provided in the fuselage for
freight or other load, but at the centre of the outriggers on
the forward face is a hook and cable incorporating a release
slip. These were to be used to attach heavy items such as tanks.
The undercarriage consist of a wheel under each engine
mounting and a tail wheel.
The Montaudran staff stated that the aircraft as originally
designed was to weigh 12.5 metric tons, lifting a load of 2 tons,
but that later the operating weight was increased to 16 tons, the
load then being increased to 5 tons, , This change was made at the
time the horse power of the engines was increased.
On the return of the Team to Paris a visit was paid to the
Breguet offices, 24 rue Georges Bizet, in company with Captain
Garry, the French Air Ministry project Officer on rotating wing
aircraft.
Monsieur Louis Breguet was interviewed and substantially
confirmed the information which was obtained at Montaudran.
No drawings were available, but the following weight analysis
was obtained, which indicates that the design weight is still
12 metric tons, but that the maximum operating weight is 16 tons.
Weight Breakdown, Fa 284
Weight, empty 8106 kilograms
removable equipment 70 kilograms
Fuel (for one hour) 640 kilograms
Oil 70 kilograms
Crew, two 200 kilograms
Normal freight load 2914 kilograms
Normal weight 12000 kilograms
Maximum freight load 6914 kilograms
Operating weight 16000 kilograms
CIOS Report German Activities in the French Aircraft Industry.
We had previously had unconfirmed information that the
Germans were developing a large helicopter for the purpose of
carrying heavy loads for short distances, i.e. transporting tanks
or heavy trucks over rivers, hoisting bridge girders into place
etc. The Fa 284 proves to be this type. The design work had been
going on at the Breguet Design Office at Montaudran Aerodrome near
Toulouse, but all the drawings were destroyed when the plant was
bombed, and the following details were supplied from memory by the
French personnel who were interviewed.
The Focke-Achgelis Firm supplied all general arrangement and
some detail drawings and Breguet were asked to design the fuselage
structure and rotor blades. A sketch of the aircraft is given at
pic. 4. It is typical of the Focke-Achgelis helicopters in that
it is of the side by side twin rotor type, the oppositely rotating
rotors each three-bladed and 18 metres (58.5 ft.) diameter, being
carried at each end of a transverse beam consisting of a centre
portion and inclined outriggers built up of tubular struts.
Each blade is built on a tubular steel spar with wooden ribs
and three ply covering. The spar is 8 cm. outside diameter with
a wall thickness of 6.5 mm and is cylindrical and of constant
gauge from the root to the station at 4*5 metres radius. From
this station to the tip it is swaged down until at the tip the
section is a parallel sided oval of 8 cm major axis, outside depth
3 cm and wall thickness 2.5mm. Over the section where the spar
is cylindrical the blades are rectangular of 77 cm chord, tapering
thereafter until at the tip the chord is 36 cm. The aerofoil
Sections are of the NACA 250 Series of 1# thickness/chord ratio.
The area of each blade is 5.4 sqr. metres so that the solidity is
.064-
The original aircraft was to have been powered by 2 BMT 801
engines rated at 1,600 horse power each, but at a later stage the
power was increased to 2,000 horse power. The engines are situated
towards the centre of the transverse beam and drive the rotors
through gears and shafting. A system of clutches is provided so
theither can drive one or both rotors, and the rotors can be
synchronised.
The outrigger beam constitutes the main structural member
and the fuselage is a simple framework attached to the beam and
carries only the usual tail surfaces and a cockpit for the crew
of two which la located behind the rotors. Except for the
cockpit and the tail surfaces the whole framework is left
uncovered. N° accommodation is provided in the fuselage for
freight or other load, but at the centre of the outriggers on
the forward face is a hook and cable incorporating a release
slip. These were to be used to attach heavy items such as tanks.
The undercarriage consist of a wheel under each engine
mounting and a tail wheel.
The Montaudran staff stated that the aircraft as originally
designed was to weigh 12.5 metric tons, lifting a load of 2 tons,
but that later the operating weight was increased to 16 tons, the
load then being increased to 5 tons, , This change was made at the
time the horse power of the engines was increased.
On the return of the Team to Paris a visit was paid to the
Breguet offices, 24 rue Georges Bizet, in company with Captain
Garry, the French Air Ministry project Officer on rotating wing
aircraft.
Monsieur Louis Breguet was interviewed and substantially
confirmed the information which was obtained at Montaudran.
No drawings were available, but the following weight analysis
was obtained, which indicates that the design weight is still
12 metric tons, but that the maximum operating weight is 16 tons.
Weight Breakdown, Fa 284
| Fuselage | 436 kilograms. | |
| Main undercarriage | 421 | |
| Tail wheel | 157 | |
| Tail unit | 110 | |
| Controls | 140 | |
| Rotor blades | 720 | |
| Rotor hubs | 1500 | |
| Main transverse beam | 10j6 | |
| Engines | 24^0 | |
| Engine mountings and | ||
| cowlings | 153 | |
| Gear boxes, clutches | ||
| and transmission | 710 | |
| Engine accessories | 18 | |
| Fuel tanks and systems | 235 | |
| Fixed equipment | 190 | |
| Weight, empty | 8106 |
Weight, empty 8106 kilograms
removable equipment 70 kilograms
Fuel (for one hour) 640 kilograms
Oil 70 kilograms
Crew, two 200 kilograms
Normal freight load 2914 kilograms
Normal weight 12000 kilograms
Maximum freight load 6914 kilograms
Operating weight 16000 kilograms
CIOS Report German Activities in the French Aircraft Industry.
- Thread starter
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Snautzer01
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- Mar 26, 2007
P-43 Lancer
WWII 1942 USAAF 1st Fighter Group March Field, CA photo crashed P-43 airplane | eBay
When relative to the photo I have one of pages along with the cropped info referring to the photo. This is not included with the photo, just for reference. Next photos are in June 1-10 1942 Iceland, then England.
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