Robert Esnault-Pelterie
Biography in context
Robert Albert Charles Esnault-Pelterie, pioneer of aeroplanes, engines, and rockets. He founded the Association des Industriels de la Locomotion Aérienne (Manufacturers Association of Aerial Locomotion) in 1908. His aircraft are numbered from 1907. He was generally working in or from Billancourt, France.
He was born on the 8th of November, 1881, in the 9th arrondissement of Paris, and died on the 6th of December, in Nice. He was as Aeronautical Engineer and an Inventor more generally.[1]
In 1904, Esnault-Pelterie built some unsuccessful versions of the Wright glider, including a vessel with ailerons.[2] Albert Francis Zahm (more charitable than Charles Harvard Gibbs-Smith) wrote that Esnault-Peletrie had a good design but should have purchased some of the key components from manufacturers who already specialized in making them.[3]
From 1907 to 1918, under designation REP, built at least 16 original designs including monoplanes, a floatplane, a parasol, and a fighter, some of which saw service in WWI. REP1 monoplane of 1907 with REP engine used wing warping. At Vickers request, sold REP license, 1911, to Vickers, which built eight REP monoplanes, 1911-1912. His firm was called Établissements Robert Esnault-Pelterie.
We have him as an Engineer addressed at rue de Silly 149, Boulogne-sur-Seine, département Seine, France.[4]
Get this patent in here: [1] aka [2] -- should be called Patent DE-1908-49251 or Patent DE-1911-49251
(We are missing a few pertinent Austrian patents here: basic ESNAULT-PELTERIE search. There are a few modest references to Belgian parental filings. Esnault-Pelterie was quite prolific. Filings in Spain seem to have greatly increased during his later productive years. These may not have been predominantly aeronautical. On the other hand, Patent ES-1907-40625 is absolutely aeronautical. There are others. We are working around various technical difficulties.)
Patent data followed by publication data
Patents whose inventor or applicant is Robert Esnault-Pelterie
- Patent ES-1907-40625 (English title: An extra-light combustion motor system applicable to aerostats, airplanes and other related uses)
- Patent GB-1908-28026 (English title: landing gear shocks)
- Patent GB-1908-28028
- Patent GB-1908-221 (English title: Improvements in aeroplanes, Supplementary to patent: Patent FR-1907-373763, Filing date: 1908-01-03)
- Patent GB-1910-12502 (Filing date: 1910-05-23)
- Patent GB-1910-18123 (Filing date: 1910-08-17)
- Patent FR-1906-366080 (English title: Extra-light combustion motor for various aircraft, Filing date: 1906-05-10)
- Patent FR-1906-372753 (English title: Airplane with two pairs of directable-directional wings, Filing date: 1906-12-19)
- Patent FR-1907-373763 (English title: Airplane with pliable balance wings and with rudders of steering and lift, Filing date: 1907-01-19)
- Patent FR-1907-373818 (English title: Airplane, overall design inclusive of all elements of lift and stability, Filing date: 1907-01-22)
- Patent DE-1907-228604 (English title: Apparatus for warping the wings of airplanes, Filing date: 1907-04-11)
- Patent DE-1907-216650 (English title: Monoplane with warpable wingpair, Supplementary to patent: Patent FR-1907-373818, Filing date: 1907-04-13)
- Patent FR-1907-366080.7788 (English title: Extra-light combustion motor for various aircraft, Supplementary to patent: Patent FR-1906-366080, Filing date: 1907-05-04)
- Patent FR-1907-373818.7789 (English title: Airplane, Supplementary to patent: Patent FR-1907-373818, Filing date: 1907-05-04)
- Patent FR-1907-380681 (English title: Automatic pliability system for airplane surfaces, both of lift and of direction, Filing date: 1907-05-22)
- Patent FR-1907-378277 (English title: System of auxiliary lift surfaces facilitating the raising of an airplane at reduced speed, Filing date: 1907-05-30)
- Patent FR-1907-366080.8650 (English title: Extra-light combustion motor for various aircraft, Supplementary to patent: Patent FR-1906-366080, Filing date: 1907-11-29)
- Patent GB-1907-28034 (English title: Improvements in Aeroplanes, with an emphasis on steering, Supplementary to patent: Patent FR-1906-372753, Filing date: 1907-12-19)
- Patent FR-1907-Robert Esnault-Pelterie26December1907 (Filing date: 1907-12-26)
- Patent FR-1907-373818.8693 (English title: Airplane, Supplementary to patent: Patent FR-1907-373818, Filing date: 1907-12-26)
- Patent FR-1908-373818.8769 (English title: Airplane wing warping and stability, Supplementary to patent: Patent FR-1907-373818, Filing date: 1908-01-10)
- Patent US-1914-1115795 (Filing date: 1908-01-16)
- Patent FR-1908-373818.9113 (English title: Airplane wings and frame, Supplementary to patent: Patent FR-1907-373818, Filing date: 1908-03-24)
- Patent GB-1908-8643 (English title: Wing spar, Supplementary to patent: Patent FR-1907-373818.7789, Filing date: 1908-04-18)
- Patent GB-1908-10528 (English title: automatic wing-warping, Supplementary to patent: Patent FR-1907-380681, Filing date: 1908-05-14)
- Patent US-1912-1024928 (Filing date: 1908-05-19)
- Patent FR-1908-373818.9591 (English title: Aeroplane hydropneumatic shock-absorbers along with more on wings and frame, Supplementary to patent: Patent FR-1907-373818, Filing date: 1908-05-25)
- Patent GB-1908-15637 (English title: Improvements in variably controlled monoplane wing warping having to do with lift per se, Supplementary to patent: Patent FR-1908-392672, Filing date: 1908-07-16)
- Patent FR-1908-392672 (English title: Warping airplane wings of variable-controllable lift power, Filing date: 1908-07-16)
- Patent FR-1908-394139 (English title: Mode of starting combustion engines with kerosene or other low-volatility fuels, Filing date: 1908-08-06)
- Patent FR-1908-393995 (English title: System for starting airplane or automobile engines, Filing date: 1908-09-05)
- Patent AT-1911-49251 (English title: Airplane, Filing date: 1908-10-16)
- Patent FR-1908-392672.10000 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1908-10-27)
- Patent FR-1908-373818.10055 (English title: Wing, Supplementary to patent: Patent FR-1907-373818, Filing date: 1908-11-10)
- Patent FR-1908-372753.10059 (English title: Airplane with two pairs of directable-directional wings, Supplementary to patent: Patent FR-1906-372753, Filing date: 1908-11-11)
- Patent GB-1908-28027 (English title: Improvements to airplane steering, Supplementary to patent: Patent FR-1907-Robert Esnault-Pelterie26December1907, Filing date: 1908-12-23)
- Patent DE-1908-222674 (English title: Airplane with warpable wing, Filing date: 1908-12-24)
- Patent DE-1908-226597 (English title: Control system for airplanes, Supplementary to patent: Patent FR-1907-373818.8693, Filing date: 1908-12-24)
- Patent FR-1909-398917 (English title: Manner(and probably apparatus) of the suspension of the cockpit in dirigibles, Filing date: 1909-01-28)
- Patent FR-1909-392672.10853 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-04-20)
- Patent FR-1909-402280 (English title: Propulsive blade with automatically-orientating wings (responsive therein to aircraft speed), Supplementary to patent: Patent BE-1908-May 22 Robert Esnault-Pelterie, Filing date: 1909-04-21)
- Patent GB-1909-10098 (English title: Variable-pitch propeller, Supplementary to patent: Patent BE-1908-May 22 Robert Esnault-Pelterie, Filing date: 1909-04-28)
- Patent FR-1909-392672.10957 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-05-06)
- Patent FR-1909-392672.11077 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-06-01)
- Patent FR-1909-403951 (English title: method of manufacturing "resistant" propellers particularly for propelling airplanes, Filing date: 1909-06-11)
- Patent FR-1909-373818.11185 (English title: Airplane, that is, a very light sufficiently rigid transversal beam, Supplementary to patent: Patent FR-1907-373818, Filing date: 1909-07-01)
- Patent FR-1909-392672.11199 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-07-02)
- Patent US-1912-1024929 (English title: Aeroplane, Filing date: 1909-07-14)
- Patent FR-1909-392672.11397 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-07-16)
- Patent FR-1909-392672.11398 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-07-22)
- Patent GB-1910-18604 (Filing date: 1909-08-09)
- Patent FR-1910-405849 (English title: Improved wing structure, Filing date: 1909-08-09)
- Patent FR-1909-392672.11399 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1909-08-11)
- Patent FR-1909-405849.11380 (English title: Improved wing structure, Supplementary to patent: Patent FR-1910-405849, Filing date: 1909-08-17)
- Patent GB-1909-23309 (Filing date: 1909-10-12)
- Patent US-1912-1040533 (Filing date: 1909-10-19)
- Patent FR-1910-366080.12217 (English title: Extra-light combustion motor for various aircraft, Supplementary to patent: Patent FR-1906-366080, Filing date: 1910-01-28)
- Patent FR-1910-414125 (English title: Flexible system of mounting monoplane wings, in the interests of rendering automatique stability, Filing date: 1910-03-25)
- Patent GB-1910-9495 (English title: Improvements in Aeroplanes, Supplementary to patent: Patent FR-1909-392672.10853, Filing date: 1910-04-19)
- Patent GB-1910-10575 (Supplementary to patent: Patent FR-1909-392672.10957 • Patent GB-1908-15637 • Patent FR-1908-392672, Filing date: 1910-04-29)
- Patent FR-1910-373818.12619 (English title: Airplane, that is, a new rudder and the means of its control, Supplementary to patent: Patent FR-1907-373818, Filing date: 1910-05-17)
- Patent FR-1910-392672.12882 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1910-07-07)
- Patent FR-1910-418064 (English title: Landing gear of skis (as in modern helicopters) and of wheels, for airplanes, Filing date: 1910-07-08)
- Patent DE-1910-249760 (English title: Airplane chassis, Supplementary to patent: Patent FR-1910-418064, Filing date: 1910-07-13)
- Patent GB-1911-19349 (Filing date: 1910-08-17)
- Patent FR-1911-419438 (English title: Landing system for airplanes, featuring a certain "elasticity" in the course of braking, Filing date: 1910-08-17)
- Patent FR-1911-420981 (English title: System of construction of both monoplane and biplane chassis, etc., Filing date: 1910-09-30)
- Patent FR-1910-366080.13355 (English title: Extra-light combustion motor for various aircraft, Supplementary to patent: Patent FR-1906-366080, Filing date: 1910-10-27)
- Patent FR-1911-421962 (English title: System of levers or exhaust flywheels for the edification of student airplane pilots, Filing date: 1910-10-28)
- Patent FR-1910-366080.13630 (English title: Extra-light combustion motor for various aircraft, Supplementary to patent: Patent FR-1906-366080, Filing date: 1910-12-10)
- Patent FR-1911-424505 (English title: Wing support system allowing the same fuselage to be applied to either a monoplane or a biplane, Filing date: 1910-12-31)
- Patent FR-1911-373818.13004 (English title: Airplane, likely wings and frame, Supplementary to patent: Patent FR-1907-373818)
- Patent FR-1911-373818.13968 (English title: Airplane, that is, overall specifics of wing and otherwise airplane construction, Supplementary to patent: Patent FR-1907-373818, Filing date: 1911-01-11)
- Patent FR-1911-392672.13796 (English title: Warping airplane wings of variable-controllable lift power, Supplementary to patent: Patent FR-1908-392672, Filing date: 1911-02-01)
- Patent FR-1911-425728 (English title: Application of the gyroscope to the automatic control of transversal and longitudinal airplane stability, Filing date: 1911-02-08)
- Patent FR-1911-419438.13906 (English title: Landing system for airplanes, featuring a certain "elasticity" in the course of braking, Supplementary to patent: Patent FR-1911-419438, Filing date: 1911-03-06)
- Patent GB-1911-6750 (Filing date: 1911-03-17)
- Patent FR-1911-373818.14381 (English title: Airplane, that is, further elaboration of frame, featuring cables, Supplementary to patent: Patent FR-1907-373818, Filing date: 1911-05-19)
- Patent FR-1912-444280 (English title: system of hydro-pneumatic suspension for automobiles and other vehicles, Filing date: 1911-08-02)
- Patent GB-1911-18129 (Filing date: 1911-08-10)
- Patent GB-1911-18133 (Filing date: 1911-08-10)
- Patent GB-1911-18145 (Filing date: 1911-08-10)
- Patent FR-1912-434150 (English title: Manner of attaching canvas on airplane wings, Filing date: 1911-09-12)
- Patent FR-1911-446282 (English title: Automatic airplane longitudinal stability system, Filing date: 1911-09-27)
- Patent FR-1912-446282.16689 (English title: Automatic airplane longitudinal stability system, Supplementary to patent: Patent FR-1911-446282, Filing date: 1912-01-15)
- Patent FR-1912-434150.16010 (English title: 1st certificate of addition to the patent taken on September 12th, 1911, for the manner of fixing of the fabric on the wings of an aeroplane, Supplementary to patent: Patent FR-1912-434150, Filing date: 1912-05-31)
- Patent FR-1912-444860 (English title: New manner of aeroplane wing construction, Filing date: 1912-06-11)
- Patent FR-1912-419438.16150 (English title: Landing system for airplanes, featuring a certain "elasticity" in the course of braking, more on frame flexibility, Supplementary to patent: Patent FR-1911-419438, Filing date: 1912-06-29)
- Patent FR-1912-446603 (English title: Aircraft with speed variable by way of relative inclination of wings and tail apparatus, Filing date: 1912-07-27)
- Patent FR-1912-447384 (English title: Mixed landing gear for hydroplanes, Filing date: 1912-08-19)
- Patent FR-1913-447384.16395 (Supplementary to patent: Patent FR-1912-447384, Filing date: 1912-08-24)
- Patent GB-1912-20927 (English title: Airplane stability, Supplementary to patent: Patent FR-1911-446282, Filing date: 1912-09-13)
- Patent GB-1912-21001 (English title: Airplane stabilizer, Supplementary to patent: Patent FR-1912-446282.16689 • Patent FR-1911-446282 • Patent GB-1912-20927, Filing date: 1912-09-14)
- Patent FR-1913-448556 (English title: Chassis of sea-"landing", or amerrissage, Filing date: 1912-09-20)
- Patent FR-1913-449503 (English title: Airplane landing gear system featuring skis, as opposed to wheels, Supplementary to patent: Patent FR-1907-373818 • Patent FR-1907-373818.8693, Filing date: 1912-09-25)
- Patent FR-1913-457105.19531 (English title: Armored fuselage system for military (heavier-than-air) aircraft, Supplementary to patent: Patent FR-1913-457105, Filing date: 1913-04-24)
- Patent FR-1913-457105 (English title: System of armored fuselage for military airplanes, Filing date: 1913-04-24)
- Patent FR-1913-473934 (English title: Airplane with automatic longitudinal equilibrium, Filing date: 1913-10-23)
- Patent FR-1913-473934.19539 (English title: Airplane with automatic longitudinal equilibrium, Supplementary to patent: Patent FR-1913-473934, Filing date: 1913-11-27)
- Patent FR-1914-457105.19754 (English title: System of plated fuselage for military aircraft (heavier-than-air), Supplementary to patent: Patent FR-1913-457105, Filing date: 1914-03-25)
- Patent FR-1914-476875 (English title: Refinement in shock absorber apparatus for airplane landing, Filing date: 1914-05-13)
Publications by or about Robert Esnault-Pelterie
- REP, 1905, Expériences d'aviation exécutées en 1904, en vérification de celles des frères Wright (Simple title: Aviation experiments carried out in 1904, in verification of those of the Wright brothers, Journal: L'Aérophile)
- REP, 1907, Aeroplane e motore Esnault-Pelterie (Simple title: Airplanes and motor Esnault-Pelterie, Journal: Boll. Soc. Aer. Ital.)
- Publication 2769, 1907, Chronology of principal events (Simple title: Chronology of principal events, Journal: Amer. Mag. Aeronautics)
- Besançon, 1907, Portraits d'aviateurs contemporains. Robert Esnault-Pelterie (Simple title: Portraits of contemporary aeronaut Robert Esnault-Pelterie, Journal: L'Aérophile)
- Publication 335, 1907, L'aeroplano e il motore Esnault-Pelterie (Simple title: The airplane and the Esnault-Pelterie engine, Journal: Boll. Soc. Aer. Ital.)
- REP, 1907, L'aéroplane et le moteur extra-léger Esnault-Pelterie (1) (Simple title: The airplane and the extra-light engine Esnault-Pelterie, Journal: L'Aérophile)
- REP, 1907, L'aéroplane et le moteur extra-léger Robert Esnault-Pelterie (2) (Simple title: The airplane and the extra-light Robert Esnault-Pelterie engine, Journal: L'Aérophile)
- REP, 1907, Le moteur R. E. P. sept cylindres (Simple title: The engine R. E. P. seven cylinders, Journal: La Rev. Aviat.)
- REP, 1907, L'aéroplane Esnault-Pelterie. Le moteur (Simple title: The Esnault-Pelterie airplane. Engine, Journal: La Conq. l'Air)
- Publication 1046, 1908, Aviazione. Wright, Farman, Blériot, Bonnet-Labranche, Santos-Dumont etc (Simple title: Aviation. Wright, Farman, Blériot, Bonnet-Labranche, Santos-Dumont, Koechlin-Pischof, Antoinette, Herring, Esnault-Pelterie, Meschuer, British military airplane, another English airplane, Zipfel, Equeauy's flying Peau Machina, Chappel, Gastambide- Mengin, French military airplane, Journal: Boll. Soc. Aer. Ital.)
- Publication 1046, 1908, Aviazione. Wright, Farman, Blériot, Bonnet-Labranche, Santos-Dumont etc (Simple title: Aviation. Wright, Farman, Blériot, Bonnet-Labranche, Santos-Dumont, Koechlin-Pischof, Antoinette, Herring, Esnault-Pelterie, Meschuer, British military airplane, another English airplane, Zipfel, Equeauy's flying Peau Machina, Chappel, Gastambide- Mengin, French military airplane, Journal: Boll. Soc. Aer. Ital.)
- REP, 1908, Les projets de M. R. Esnault-Pelterie (Simple title: The projects of Mr. R. Esnault-Pelterie, Journal: La Rev. Aviat.)
- Bradley and Perry, 1909, Power generation and transmission in aeroplanes (Simple title: Power generation and transmission in aeroplanes, Journal: Eng. Mag.)
- Faroux, 1909, En el Gran Palacio (Simple title: In the Grand Palaias, Journal: Revista de Locomoción Aérea)
- Esnault-Pelterie, 1910, Letter from Esnault-Pelterie explaining his point of view on the Wright question (Simple title: Letter from Esnault-Pelterie explaining his point of view on the Wright question, Journal: Aircraft)
- Esnault-Pelterie, 1910, Photograph and biography of R. Esnault-Pelterie (Simple title: Photograph and biography of R. Esnault-Pelterie, Journal: Aircraft)
- Esnault-Pelterie, 1912, Aëroplane chassis (Simple title: Aëroplane chassis, Journal: Aeronautics)
Other standard format data
Names | Robert Esnault-Pelterie |
---|---|
Birth date | 1881-11-08 |
Death date | 1957-12-06 |
Countries | FR, US, GB, DE, AT, ES |
Locations | Billancourt, département Seine, France; Boulogne-sur-Seine, département Seine, France |
Occupations | Engineer, Aeronautical Engineer, Inventor |
Tech areas | Airplane, Monoplane, Biplane, Hydroplane, Propellers, Wings, Wing warping, Lift, Construction, Design, Aerodynamics, Flapping, Propulsion, Propellers, Ignition, Rudder, Chassis, Fuselage, Stability, Cables, Aileron, Shock-absorbers, patins, Amerrissage, Landing, Automatic stability, pump, Pistons |
Affiliations | Association des Industriels de la Locomotion Aérienne, Établissements Robert Esnault-Pelterie |
Wikidata id |
References
- ↑ Robert Esnault-Pelterie on French Wikipedia
- ↑ Gibbs-Smith, Aviation, 1970, p. 108. "Inspired by Archdeacon to emulate the Wrights, an able engineer named Robert Esnault-Pelterie also built and tested in May 1904 what he falsely claimed was an exact copy ('absolument semblable') of the 1902 Wright glider, except for details; he found it was unsatisfactory and decided to improve it. He clearly could not make the warping work properly, and—like the other Europeans—did not understand the significance of Chanute's description of the simultaneous use of warping and rudder. Esnault-Pelterie then asserted that warping was structurally dangerous. In October 1904 he tested a rebuilt version using—for the first time in history—ailerons, or rather primitive elevons, instead of the warping and front elevator (Pl. XXII): this machine, despite its ingenuity, was a crude affair and a failure, and Esnault-Pelterie—like his friends—would not take the trouble to experiment, modify and improve. The deplorable influence of Esnault-Pelterie on French aviation did not take effect until 1905, when his lecture was given, and publicized later in the year."
- ↑ Zahm, 1911, Aerial Navigation, p. 304. "Though the 'R. E. P. aëroplane, as it was commonly called, did not achieve great distinction at first, due, perhaps, to the inventor's being over original, and making all its parts himself, instead of buying some high-class engine and propeller, as other successful aëroplanists had done, still his machine was greatly admired by technicians for its excellent finish and the fastidious, thorough and patient manner in which its young inventor labored to make it perfect, both in design and construction."
- ↑ Patent GB-1912-20927
Sources
- Gunston, 1993, p109, 316
- Gunston, 2005, p150, 483
- SD240
- 1919AYB358, 360
- Wikipedia article about Esnault-Pelterie
More patents by REP, from DPMA
- DPMA -- the German patent office which has records from several countries
- there does exist some << < > >> navigation to get to later pages, which is used in the browser window away from the pdf, after the pdf is closed.
- Search query: ((PA=(Esnault (L) Pelterie)) OR (IN=(Esnault (L) Pelterie))) Status: 24.03.2017
serial number Publication number Applicant/Owner PDF URL Sequence listings URL Searchable text URL
- 1 AT000000102992B -- DPMA's site gives back a "java.lang.NullPointerException" when trying to load this one. So we don't have a year.
- 2 AT000000102163B -- Austrian patent 102163 from 1924-25 by REP, first page shown only
- 3 AT000000049251B -- Austrian Patentschrift Nr 49251. from Kais. Konigl. Patentamt. Given 10 Aug 1911 I believe, but might be 1914. Klasse 77d. Only cover sheet is shown.
- 4 AT000000047810B ESNAULT-PELTERIE ROBERT, FR
- 5 AT000000045367B ESNAULT-PELTERIE ROBERT
- 6 AT000000037181B -- Austrian patent 37181 granted 10 May 1909, REP listed in Boulogne-sur-Seine, title Einrichtung an Flugmaschinen, "Angemeldet am 22 Aug 1907", "Beginn der Patentdauer 15 Dec 1908, klasse 77d, first page shown only
- 7 CA000000417116A SPLADIS SOC POUR L APPLIC D IN -- no link
- 8 CH000000137497A ESNAULT PELTERIE ROBERT ALBERT, FR -- Conferation Suisee Clas 62 No. 137497 published 16 avril 1930. Demande deposee 9 juin 1927. Brevet enregistre 15 janvier 130. Priority: GB 4 fev 1927. Robert Albert Charles Esnault-Pelterie, Paris. Title not clear but maybe: Prcede et appareil pour l'essai des materiaux. 7 figures referred to.
- 9 CH000000137496A ESNAULT PELTERIE ROBERT ALBERT, FR -- another from 1930
- 10 CH000000109170A ESNAULT PELTERIE ROBERT, FR
- 11 CH000000094537A ESNAULT PELTERIE ROBERT, FR
- 12 CH000000094293A ESNAULT PELTERIE ROBERT, FR
- 13 CH000000093670A ESNAULT PELTERIE ROBERT, FR
- 14 CH000000093079A ESNAULT PELTERIE ROBERT, FR
- 15 CH000000092794A ESNAULT PELTERIE ROBERT, FR
- 16 CH000000092472A ESNAULT PELTERIE ROBERT, FR
- 17 CH000000092228A ESNAULT PELTERIE ROBERT, FR
- 18 DE000001027031B SPLADIS SOC POUR L APPLIC D IN [3] [4]
- 19 DE000001027031A SPLADIS SOC POUR L APPLIC D IN [5] [6]
- 20 DE000000524139A [7] [8]
- 21 DE000000496783A [9] [10]
- 22 DE000000469191A [11] [12]
- 23 DE000000415491A [13] [14]
- 24 DE000000399264A [15] [16]
- 25 DE000000384737A [17] [18]
- 26 DE000000352698A [19] [20]
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- 32 FR000001098756A
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- 37 FR000000903741A ROBERT ESNAULT PELTERIE ETS
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- 59 [https://depatisnet.dpma.de/DepatisNet/depatisnet?window=1&space=main&content=treffer&action=pdf&docid=FR000000529858A FR000000529858A
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- 72 FR000000501838A
- 73 FR000000500632A ROBERT ESNAULT PELTERIE, FR
- 74 FR000000495270A ROBERT ESNAULT PELTERIE, FR
- 75 FR000000491144A
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